Sample 4 FAT Report Rev 0

RPP-RPT-49670, Rev. 0 

Washington River Protection Solutions 242-A 

Evaporator KI Exhaust Ventilation Systems 

Factory Acceptance Test Report 

W.T. Domigan 

Washington River Protection Solutions 

Richland, WA 99352 

U.S. Department of Energy Contract DE-AC27,O8RVI 4800 

EDT/ECN: V 1 UC: 

Cost Center: N/A Charge Code: N/A 

B&R Code: N/A Total Pages: 3-7 &o 

Key Words: 242-A, Ki Exhauster, Factory Acceptance Test, ASME AG-i 

Abstract: The 242-A KL Exhaust Ventilation System was designed, fabricated, and tested by Premier 

Technology, Inc. out of Blackfoot, I1). This report documents the testing approach, acceptance criteria, 

testing results, and completion of testing for the equipment provided to WRPS. 

TRADEMARK DISCLAIMER. Reference herein to any specific commercial product, process, or service by trade name, 

trademark, manufacturer, or otherwise, does not necessarily constitute or imply its endorsement, recommendation, or 

favoring by the United States Government or any agency thereof or its contractors or subcontractors. 

SEP 01 2 

OAT: tAC 

1; 1 I Loo11 

Release-Approval Date Release Stamp 

Approved For Public Release 

STA. D 

A-6002-767 (REV 2)

Note: 

Premier Technology, Inc. 

Factory Acceptance Test Report 

242-A Evaporator HVAC K1 Exhaust Ventilation System Upgrade 

RPP-RPT-49670 Rev 0 

Factory Acceptance Testing (FAT) was initiated by Premier Technology, Inc. (Premier) using revision 5 of 

the Factory Acceptance Plan which had been approved with comments by Washington River Protection 

Solutions (WRPS) authorizing Premier to proceed with specific sections of the FAT. As such, certain 

sections of the FAT were signed off using revision 5 of the FAT Plan. These sections can be found in 

Attachment B of this report. 

Premier revised the FAT Plan and submitted rev 6 which addressed the majority of the outstanding 

WRPS comments, however not all of them, such that WRPS approved rev 6 of the FAT Plan with 

comments and authorized Premier to proceed with additional sections of the FAT. As such, certain 

sections of the FAT were signed off using revision 6 of the FAT Plan. These sections can be found in 

Attachment A of this report. 

Lastly, Premier again revised the FAT Plan and submitted rev 7 which fully and satisfactorily 

incorporated all outstanding WRPS comments such that WRPS approved rev 7 of the FAT Plan and fully 

authorized Premier to proceed with all remaining sections of the FAT. It is this revision that makes up 

the main body of this report and the appropriate references to either revision 5 or 6 in attachments B or 

A, respectively, are made therein.

A Premiar T'echnaowg, ISC. 

1 858 W, Bridge Streest 

BlackfOotZD, 83221 

(208) 785-2274 

www.ptius.niet 

Washington River Protection Solutions 242-A Evaporator K1 

Exhaust Ventilation Systems Factory Acceptance Test 

Approvals Nm:Signature: Date: 

Preparer 

Technical J 

~ - c1illi 

Quality Assurance ~A~ 

Revision 7 

CONTROLLED

(~?IEMIE -P 

PRxEER TECHNOLOGY, INC. Project No. 006765.0.000 

-242-A Evaporato Ki Exhaust Contract 40167 

\~k~ ag e hno ; I c.V entilation S stem No. 


1FACTORY ACCEPTANCE TEST PLAN S p e No0. R.PSev 0 06 

Table of Contents 

1.Purpose and Scope;............................................. ....... .......... 

1. pups ....................................... 

. ......................... 

~.......................... ............... 

1 oiscope e............................... ...................... 

1.5 .............................................. 

1. efernScoe .......................... ......... ...... ...... ........ ........... 

IA. IformtIo.....................................................................---.... -*...4* 

1 .1 Tef ras d.............iti 

.. n......................................4 

..... 

2. TstPesone........................... ........................ 6 

2.4 

2.1 

Genelitu......................................................... 

Tes Exde ntions .................. : . ............................... I.................... . . . . . 7 

.6 rmRso A e. . . ... ................................. 

........................................... 7 

* 2.71 Syise ..... I................................................ 

2.8 an RCUD~S uspnsiD Tst................................. 

o Tet 

2.9 TesPeonneihl .............. ........................................ 

8 

.4 Preuinend info ations.................................................................. 

3.1 Prsonel sfety.............................. ..................... 9 

.2 

.6 

es Eipen ........................................................ 

Aar m es pons... ........................................................................................ 

. 

1 

.1 

4.1.Test.Spe..fic.p....o........i................................ 

I..................1 7 

.2 Spsei1 Stools, Equ...pment........d..Suppli............ .. . . . . . . ............ ........ 

.8 Susensionof.T.t..n..........et......................... .............. 

6.9 TesnusidelifFA............................ 

6. ~................. 

........................... 

................... 

1 

.2 Vaers/Da-aper -................. Te.........*... ...................... 3 

6.3 Pessure.rop........................ Damers - 

....................... 14 

4.2 entandSi~ pecal ools, lies.................................... 

E uip 

6.4 DanpersSeat&.........C 

Sch du v .... 

:...................................................................A.. 

1. Pemn O ide e ology,.......................... 

.....

PREMIER TECHNOLOGY, INC. 1'rojectNo. 006765.0.000 

VWS - 242-A Evaporator KI Exhaust Contract 40167 

Ventilation System 

No. 

FACTORY ACCEPTANCE TEST PLAN Spec No. Re 0 


6.5 FilterTran -PessureBoundaryLekage ........................I.....I 

....................................... 17 

6.6 Instrumentation and power wiring - Continuity and megger testing.........................................is 

6.7 Pre-Filter Diffetial Pressure indicators - Verify Differential Pressure Indicator Function............. 19 

6.8 Local I' Stage BEPA Section Pressure Indicators - Verify Differential Pressure Indicator Function ... 20 

-6.10 

6.9 Loal "~Stge EP Sctin resure idcatr- Verify Differential Pressure Indicator Function ... 21 

Exhaust Stack Sample Pitot Tube and Transport Lines - Leak test & Pitot Tube Alignment............. 22 

6.11 Mass Flow Controller Record Sampler and Vacuum Pump .................................................. 22 

6.12 Mass Flow Controller CAM and Vacuum Pump ......... ... I...............................................2 

6.13 Vacum Pump -Verify Purmp operation .......................................................... ......... 24 

6.14 Continuous Air Monitoring -Verify CAM Alarm and Interlock Set point .......~........I...............24 

6.15 Sampler line Vacuum. Indicator - Functional Test (P1-1)................................................... 25 

6.16 Sampler Line Vacuum Indicator -Functional Test (P1.1l-2)...........I....................................... 25 

6.17 CAM Operation - Verify'No Electromagnetic Radation Interference ............ ......................... 25 

6.18 Sampling system instrumentation and wiring - Continuity and megger testing............................. 25 

6.19 Sample Cabinet cooling fan -Functional test ................................................................. 26 

620 Verabar Flow Sensor - Verify Exhiauster Flow Indication ................................................... 26- 

6.21 Sampling Manifold - Qualification of Filter Sampling System .............................................. 27 

6.22 Fan and Motor .- Vibration (Drive motor rotating elements) & Sound ...................................... 28 

6.23 Intake Plemn & Expansion Joints - Pressure, Decay Test & Bubble Leak Test............................ 

7 Procedure.......................................................... 

..................................... 

29 

29 

7.1 Valves/Dampers - Visual inspections ............... t........................ ................................ 29 

7.2 Valve/Dampers - Verify Isolation Valve Position Indication and Function................................. 31 

7.3 Filter Train - Visual Inspection ........ 7 . ............ I......................................................... 33 

7.4 242-4 Evaporator KI Exhaust - Pressure Decay Test & Bubble Leak Test................................. 35 

7.5 Power Instriuent and Control Cabling -Proper voltage and phase sequence at equipment served....39 

7.6 Dampers - Damper Cycle Time and Operation ................................. I..................... ......... 40 

7.7 KI-S2M Motor and VFD - Proper voltage at equipment served .................................. . ........ 1.42 

7.8 KI-5-2 Fan and Motor -Vibration Test (Minimum System Loss)........................................... 46 

7.9 Kl-5-2 Fan and Motor - Sound Test........................................................................... 

7.0 Section 1 Valves/Dampers - System Pressure Boundary Leak Test......................................... 50 

7.1 1( -5-2 Fan and Motor - Vibration Test (Maximum System Loss) .......................................... 51 

7.12 K1-5-3M Motor and VFD - Proper voltage at equipment served ............................................ 53 

2 Premier Technology, Inc. 

006765.0.OOO-FAT-OO1-1 (Rev 7) 

49

PREMIER TECHNOLOGY, INC. Project No. 006765.0.000 

[U WEpS - 242-A Evaporator KI Exhaust Contract 40167 

\~wv'Thhfll~g4 ~Ventlation System No. 

& Te~clno 09y Inc.PPC-36062 

FACTORY ACCEPTANCE TEST PLAN Spec No. Rev 0 


7.13 KI1-5-3 Fan and Motor - Vibration Test (Minimum System Lass).......................................... 57 

6 

7.14 Kl1-5-3 Fan and Motor - Sound Tog..................I...................................................... 

7.15 Section 2 Valves/Dampers - System Pressure Boundary Leak Test.....*................................... 61 

7.16 Stack Joint -Bubble leak est.................................................... 

............................ 62 

7.17 KI-5-3 Fan and Motor - Vibration Test (Maximum System Loss)......................................... 63 L 

7.18 

7.19 

Filter Train A - Airflow Distribution (Full System).........................................................64A 

Filter Train B - Airflow Distibution (Full System)-...I...........I................................... 

...... 66 

7.20 

7.21 

7.22 

7.23 

Filter Train C -Airflow Distribution (Full Systemf)........................................................6 

Stack Sampling location -Angular or Cyclonic flow ...................................................... 

6 

Stack Sampling Location - Contaminant Concentration and Velocity Profiles ......................... 

.. 71 

Exhaust Stack Sarle; Line - Heat Trace Thermostat for CAM airborne Radiation Detector (GS)I....73 

8. -Completion ofFAT Test.............'.........1 ...........- ..................... I..................1 

9. Attachment List.................... ............................................................................ 

1. Purpose and Scope 

1.1 purpose 

This pro cedure was created for the purpose of performing Factory Acceptance Testing 

(FAT) of the 242-A Evaporator K1 Exhaust ventilation System provided by Premier 

Technology, Inc. for Washington River Protection Solutions (WRJ'S). 

The objective of this document is to provide a description of the processes that will be 

followed at the manufacturer's facility in order to performi t Factory Acceptance Testing 

of the 242-A Evaporator KI Exhaust Ventilation System in order to verify that the unit 

comp lies with the requirements of WRPS Specification RPP-SPEC-3 6062, Rev. 0 and the 

applicable flow down Specifications listed tberem". 

) 5M P49WD FA 

This Procedure will address all applicable components supplied by this order. These 

components are listed i section 6 and 7 of this FAT test The findings of each test shall be 

recorded in separate section of this document for each component. 

The testing will be performed at Premier Technology's facility. 


fM -M&(hSAP ~ (7r. ~ 

I 7 7L~ -- 

OO6765.O.00-FAT-O01-1 

84 

(Rev 7)

(i ET 


MIERT 

PREMIER TECHNOLOGY, INC. 

W.RPS - 242-A Evaporator KI Exhaust 

Project No. 

Contract 

006765.0.000 

40167 

'Fehooy n.Ventilation System No. 

FACTORY ACCEPTANCE TEST PLAN ISpec No. IPPSev -300 

7.24 Continuous Air Monitoring - Verify CAM bypass feature .................................................. 74 

7.25 Vacuum Pump - Verify Pump operation...................................................................... 76 

7.26 C AM Operation - Verify No Electromagnetic Radiation Interference ...................................... 77 

7.27 Sample Cabinet cooling fan - Functional test ....................... ......................................... 78 

7.28 Inlet Plenum & Expansion Joints - Pressure Decay Test & Bubble Leak Test ............................. 79 

7.29 Exhaust Stack Sample Pitot Tube and Transport Lines - Leak test & Pitot Tube Alignment............. 81 

7.30 Sampler line Vacuum Indicator - Functional Test (PI1) .................................................... 82 

3a Premier Technology, Inc. 006765.O.OOO-FAT-0O1-1 (Rev 7)

PREMIER TECHNOLOGY, INC. ProjectNo. 006765.0.000 

ER WRS 242-A Evaporator Ki Exhaust conwmct 

p"DEM 

(Z -Tlchnowg Inc. Ventilation Systm No. 40167 

1.2 Scope 


FACTORY ACCEPTANCE TEST PLAN Spec No RPPSPEC-36062 

Rev 0 

This procedure is to demonstrate that the 242-A Evaporator KI Exhaust Ventilation System 

preforms properly in accordance with the WRPS Specification RPP-SPEC-36062, Rev. 0, 

NEMA MG-i 2007, ASME AG-I, TFC-ENG-STD-07, and ANSIN13.1. 

1.3 Not in Scope 

"None" 

1.4 Assumptions 

Test configuration matches onsite conditions 'with the following exceptions: 

* Temporary wiring will be used between major components. (Permanent wire will be 

provided new and unused) 

* Facility Differential pressure will be simulated by throttling filter housing inlet. 

butterfly valves. 

6 VCS and MCS are not available, communication will be verified by continuity 

checks 

0 Temporary power will be used in place. of facility power. 

These assumptions have no impact on execution or results of the FAT. 

1.5 References 

1.5.1 -ASHR.AIE 52 2007 

1.5.2 IMEE 112 2004 

1.5.3 AMCA 500 1989 

1.5.4 ANSI N13.1 1999 

1.5.5 ASMEfiB31-1 2007 

1.5.6 AMCA 2041996 

1.5.7 ASME AG-i 2003 

1.5.8 40OCFR 60 

2. Information 

2.1 Terms and Definitions 

2.1.1 FAT Factory Acceptance Test 

4 Premier Technology, Inc. 006765.0.000-FAT-001-1 (Rev 7)

PREMIER TECHNOLOGY, INC. Project No. 00616&.0.000 

WRPS - 242-A Evaporator Ki Exhaust Contract 40167 

eMhoo~~Inc. Ventilation System 

FACTORY ACCEPTANCIE TMS PLAN Spec No. 0 


2.1.2. RPS Washington River Protection Solutions 

2.1.3 QA Quality Assurance 

2.1.4 NQA Nuclear Quality Assurance 

2.1.5 ASMB American Society Of Mechanical Engineers 

2.1.6 AMC Air Monitoring Corporation 

2.1.7 PPE personal Protective Equipment 

2.1.8 OAT operational acceptance test 

2.1.9 VCS Ventilation Control System 

2.1.10 SCF Standard Cubic Feet 

2.1.11 CAM Continuous Air Monitor 

2A1.12 VFD Variable Frequency'Drive 

2.1.13 SWC Snall Logic.Controller 

2.1.14 )MM, DigitalMultimeter 

2.1.15 P1)11 Pressure Differenitial1 Indicating Transmitter 

2.1.6 PID '"Proportional Integral Derivative 

2.1.17 H~MI. Human Machine Intrface 

2.1.18 PLC Programmable Logio Controller 

2.1.19 BUMP To briefly energize 

2.1.20 M&TE Measurment and Testing Equipment 

2.1.21 MCS Monitoring control. system 

2.1.22 AWG America Wire Gauge 

2.1.23 CAT Construction Acceptance Test 

2.1.24 ENSUR Confirm that an activity or condition has occurred in conformance with 

specified requirements, and take action to make it so if the condition is 

NOT found to be in conformanc-e. 

2.1.25 VERIFY Perfor-m a comparison with stated requirements. No manipulation of 

equipment of other subsequent actions by the checker are involved. 

Verifications normally require initials or signature. 

2.1.26 STEADY STATE OPERATION 

Fan running at equilibrium at a set flow rate and system warmed up. 

2.2 units 

2.2.1 % Percent 

2.2.2 F Fahrenheit 

2.2.3 Hp Horsepower 

2.2.4 A Amps 


006765.O.OOO-FAT-OO1-1 (Rev 7)

PREMIER TECHNOLOGY, INC. Project ~q 0 006765.0.000 

WRPS - 242-A Evaporator K1 Exhaust Contract 40167 


(E~EMIERNo 

Tecnkg Ventilation System N.~ ~ C66 

Tecnoogy Ic- FACTORY ACCEPTANCE TEST PLAN SpecNo. RP-SEC366 

2.2.5 VAC Volts Alternating Current 

2.2.6 dBA decibels (weighted on 'A' scale) 

2.2.7 psi Pounds per square inch 

2.2.8 in inch 

2.2.9 mm millimeter 

2.2.10 in Hg Inches of mercury 

2-2.11 AWG American Wire Gage 

2.2.12 IN~ W.G. Inches Water Gauge 

2.2.13 IN W.C. Inches Water Column 

2.2.14 SCFM Standard Cubic Feet per Minute 

2.2.15 rpm revolutions per minute 

2.3 Test Personnel 

The Following personnel are required to conduct the Factory Acceptance Testingfte22 

A Evaporator Ki Exhaust Ventilation SystemA 

2.3.1 Test Director 

The test director will be present for all testing. This individual will be the Project 

Manager for the project unless otherwise designated. 

2.3.2 Test Technicians 

Test Technicians will assist the Test Director in the preparation of hardware and 

equipment for the FAT tests. These individuals will be familiar with the equipment. 

being used. 

2.3.3 QA Personnel 

Quality Assurance personnel will be present for all listed functions of the testing. The 

QA designee will record the results and test data of the testing. 

2.4 General Information 

2.4.1 Editorial changes may be made to thids procedure as required to accommodate 

procedural/editorial deficiencies that do not affect technical content Redline changes 

shall be entered using red ik, initialed and dated by the Test Director. 

2.4.2 Testing performed in the fabrication shop shall comply with shop Lock and Tag 

policy requirements. Fabricator shall verify general requirements, roles, and 

responsibilities. 

*6 Premier Technology, In c. 006765.0.000-FAT-0O1-1 (Rev 7)

PREMIR TECHNOLOGY, INC. Project No. 006765.0.000 

(~ T f R WRPS - 242-A Eaporator KI Exhaust contract 406 

\&/olo yI±E Ventilation SEste 

FACTORY ACCEPTANCE, TEST PLAN spec No. RPPSev-3 


2 .4.3 Verifiation of each test shall be documented at the end of each test section by having 

the Test Director and the QA Personnel Sign and date the test section. 

2.5 Test Exceptions 

2.5.1 Test exceptions are used to document unexpected tes euttcnclpoeua 

deficiencies, and identify appropriate action. 

2.5.2 A description and a resolution for the test exceptions shall be documented in 

Attachment 1 FAT, Test Exception Record 

2.5.3 In the event of an equipment malfunction or other anomaly, the Test Director shall 

document the condition with a&Test Exception Record and assess the effect on 

equipment and direct either 

* Continuation of the test in. the same section. 

*proceeding to another attachrmbnt or section of the test. 

* Suspensibn of the test nd tstablishnidtit of a safe condition for equipment 

(See Section I!). 

2.5.4 Test exceptions and discrepancires that cannot be orreted in- accordance with this 

procedure will he documented and addressed on a non-conformnce report, per 

Premier Technology, Inc. NQA-l Quality Assurance Program. 

2.6 Alarm Response 

2.6.1 This procedure identifies all alarms expected as a result of testing, and provides 

instructions for responding to those alarms, During testing of Hfigh or Low set points, 

High and Low alams are also anticipated. 

2.6.2 Unexpected alarms received during testing shall be logged as test exceptions in 

Attachment 2, Test Exception Log and evaluated by the Test Director for effect on 

the test. 

2.6.3 All test exceptions, must be recorded in Attachment 2, FAT Test Exception Log,' and 

explained in detail in the Attachment 1, FAT Test Exception Record. 

2.6.4 Variation between EIM alarm terminology and alarm terminology provided in this 

FAT is not cause to stop testing. The variance shall be evaluated by the Test Director 

to confirm desired system response and documented on Attachment 3, FAT Test Log. 

2.7 System-Status 

2.7.1 Record all abnormalities in equipment configuration, comments, observations by 

participants, and all other data pertinent to the test in the Attachment 3 FAT Test 


006765.O.OO-FATOO01-1 (Rtev 7)


(P~ IE AI~ R WRPS - 242-A Evaporator K1 Exhaust Contract 40167 


' Teho gyi.Ventilation System .No. RI-PC30 

FACTORY ACCEPTANCE TEST PLAN Spec No. RuPSev 0 06 

Log. If applicable, initiate a test exception by identifying the condition in the 

Attachment 2, FAT Test Exception Log. 

27.8 Suspension of Test and Resuming Test 

2.8.1 The Test Director may, at his discretion, stop testing and place equipment in a safe 

condition. All suspension of testing due to exceptions shall be documented in the 

Attachmnent 3, FAT Test Log. 

2.8.2 If a section of the test is suspended for any reason prior to completing all steps, the 

Test Director shall establish initial conditions necessary to resume testing for that 

section. Previously completed sections need not be repeated unless directed by the 

Test Director to establish conditions required to resume the test. 

2.8.3 WEPS is to be advised of the condition(s) that resulted in the suspension of any test 

along with the expectd resplution. Prior to resuming any terminated test WR.PS is to 

be notified. 

2.8.4 Sections of this procedure may be performed out of sequence as lon g as components 

or-tests are NOT altered. Steps within ech section must be performed in order except 

section 7.1 which is pre-.requisite to 7.2 and 7.3 which is a pre-requisite to 7.4 and as 

indicated in sections 7.8-7.11, 7.13-7.17, and 7.18-7.22. these tests must be 

performed in order. 

2.9 Responsibilities 

2.9.lIThe Test Directr shall- 


* .Verify prerequisites are completed prior to start of testing. 

*Maintain control of the testing process and change record authorization for 

this procedure. 

a Ensure all required data is collected. 

* Ensure safe working conditions and practices. 

'Ensure compliance with test documents. 

*Ensure review and approval of all modifications to test procedures are 

* complete prior to return to testing. 

*Act as direct line of communication and centralized point of control during 

normal, abnormal, and casualty situations. 

*Conduct pre-test briefings as required. 

* Schedule and reschedule tests as required. 

*Conduct pre-test system walk-downs. 

*Review test documents to validate acceptance. 

006765.O.OO-FAT-OOI-l (Rev 7)

P MR TECHNOLOGY, INC. Project No. 006765.0.000 

WRPS - 242-A, Evaporator Ki Exhaust Contract 40167 


(~T~CI11OOg)~X1C entilation SYStem No 

FACTORY ACCEPTANCE TEST PLAN Spec NO. Rev.PR-306 

*Record equipment statuis and data in accordance with this procedure. 

*Review, approve and record data exceptions and their resolutions and other 

*notes as required on the applicable attachinents. 

*Prepare post-testing documents 

*verify component ID is correct for the component being tested. 

* verify comnpletion. of each test section. 

& Verify proper valve andAlectrical alignment before each test section. 

* Provide technical support during testing. 

a Review test documents to validate acceptance. 

* verif current version of software. 

0 Sign verification of data on calculation attachments. 

. Review-recorded data for completeness -and accuracy. 

Review and approve test exoepiQ~s. and tl~eir resolutions. 

*Review FAT for compltenss w' acqI;1OQW Y. 

2.9.2 QA Personnel shall: 

* Verify component ID is correct for thecomponent being tested. 

* Review procedure for accuracy and comnpleteness. 

. Review the PAT for accuracy and completeness. 

* Review and approve test exceptions and their resolutions. 

2.9.3 The Quality Control Inspector shall: 

a Witness testing. 

* Review recorded data for accuracy and completeness. 

-- Verify completion of each test section. 

*Verify completion of test exceptions and their resolutions. 

2.9.4 Test Technicians shall: 

0 Provide assistance during testing. 

* provide equipment for performance of this procedure. 

3I Precautions and Limitations 

3.1 Personnel Safety 

All persons within the test area shall wear the appropriate Personal Protective Equipment 

(PPE). At a minimum this shall include eye protection. Gloves should be worn where there 

is a likelihood of contactig sharp edges or when handling rigging equipment. 


006765.O.OWOFAT-OO1-l (Rev 7)

PREMIER TECHlNOLOGY, INC. Project No. 006766.0.000 


(~1 NA ER WRS - 242-A Evaporator Ki Exhaust Contract 40167 

TcnlgInc. Ventilation System No. 

FACTORY ACCEPTANCE TEST PLAN Spec N~o. RPPeC-306 

All persons within the test area are authorized to immediately halt testing should they 

observe an unsafe condition that could compromise the safety of themselves, other persons 

in the test area or the safety of the equipment Concerns should be addressed to the test 

director to ensure an orderly and controlled shutdown of the equipment being tested. 

NOTE: Energized circuits and leads are contained inside cabinets, Failure to comply with 

appropriate electrical PPE and safety procedures can cause serious personnel injury or death 

from electrocution. 

3.2 Equipment Safety 

3.2.1 A pre-test briefing should be conducted to identify unusual and for hazardous 

conditions 

3.2.2 Shop'safety rules should be stzictly adhered to during the performance of ths test 

3.2.3 Shop Lack and Tag requirements should be followed at all times during the 

performance of this test 

4. Prerequisites 

4.1 Test Specific pre-configurations 

4.1.1 Any settings, configurations, etc, which are required for specific tests (prior.to 

beginning the numbered test steps) shall be determined by the test director, who shall 

direct personnel to make any necessary configuration changes. Prerequisites listed. 

elsewhere in this test procedure but not required for a particular test do not have to be 

performed, at the discretion of the test director. This includes ensuring that all gaskets 

have been installed, holes have been sealed, and any valves have been properly positioned. 

4.1.2 Ensure that all apparatus on the 242-A Evaporator KI Exhaust Ventilation Systemn 

necessary for the performance of the Test Procedure have been installed and are fully 

operational. This includes ensuring that all gaskets have been installed, holes have 

been sealed and any valves have been properly positioned. 

4. 1.3 Ensure that the equipment to be tested is free of dirt, chips, scale or any other debris 

that would hinder testing. Cutting fluids and residual oils shall be removed from the 

surfaces of the housing and components. 

10 Premier Technology, Inc. 006765.O.00-FAT-0O1-1 (Rev 7)

I 6.1 


P E M T E C N O L G Y , I N C 

WRpS 

. 

- 242'-,A Evaporator Ki Exhaust Contract J' N 40167 0 7 . . 0 

Ventlation 'RstemnNo 

& echnology, Inc. P P. M-VC362 

FACTORY ACCwzTANCE TEST I LAN SWe N& Rv, 

PP LEMIER 

4.1.4 Test Procedure Review - The test director shaI enure that all Persons participating 

in testing as Test Technicians have reviewed and understood the requirements Of the 

test procedure and the equipment to be tested. 

4.1.5 The signature in Testing Outside of FAT serves as confirmation by Premier 

indicating that the subject documentation was reviewed, verified, complete, and 

accepted. 

4.2 Special Tools, Equipmentand Sutpplies 

& Compressed air source (0.25 00) 

9 covers to seal te~t boundaries 

* clock or tinmer capable of reading seconds, 

apressuro-indicatg device accurate to t 0.1 in:.wg [02(25 kPA (gage)]* 

*flow meter or totalizing gas volume meter accurate to 15%/ (conant-presSure 

method)* 

*temperafure-indicaiof device accurate to 6-05TF (0.25*C)o 

*bubble solution for detecting air leaks (bubble method) 

* optional portable electronic sound detection equipment (audible leak method)* 

" barometer* 

" Amp Meter* 

" Volt Metr* 

NOTE: *Calibration information required, 

5. Schedule 

The schedule is.deennned by the test director according to scheduling of subcontractors 

and pre-requisites to each specific test listed in section 7. 

6,. Testing Outside of FAT 

Testing that was accomplished or will be accomplished by vendors, contractors, and 

standard NQA-I manufacturing practices that can be used to validate any FAT are verified 

in this section. 

Electric D~rive Motor - Motor RuD Test 

MAT=I REFERENCE - line 1, 2, & 3 


006765.O.000-FAT-0O1-1 (Rev 7)

PRELMIER. TECHNOLOGY, INC. Project No. 006765.0.000 

(UP E M4IER WRPS - 242-A Evaporator KI Exhaust Contract 40167 

\ 4~cn~oy ic Ventilation System No. 

Techollgy, nc.RPP-SPEC-36062 

FACTORY ACCEPTANCE, TEST PLAN Spec No. Rev 0 


BACKGROUND - This test is to show that electric drive motors are in accordance with 

IEEE standard 112. 

COMPONENT BEING TESTED: 

* Kl-5-2-M 

* KI-5-3-M 

ACCEPTANCE CRITERIA: 

0 Motor is free of mechanical and electrical defects and is within mnanufacturers 

tolerance 

* Efficiency shall equal or exceed 94.1% 

* Locked motor current shall not exceed 543 A for 75 Hp motor at 460 VAC 

* Motor is certified to NEMA MG-1 

TEST PROCEDURE: 

6.1.1 RECORD motor efficiency from motor nameplate. 

6.1.2 RECORD motor locked rotor amps form motor nameplate. 

6.1.3 REVIEW manufacturer's certification documents in Attachment 6.1 (see Baldor 

Reliance Product Information Packet ECP843 16T-4 page 8 of 8 & Baldor 

Petroleum/Chemical Solutions Cataloged page 5 841XL Motor).4k 

Motr*. 

IKs-5-24W 

Nameplt Certification 

Effciecy ockd aps 

Efdcy LdamsEfficiency Locked amp'sIs 

95A 542 SA4Z- 

Intals 

Test IQA 

Director I nsixotor 

KI-5-3-M 954426 

6.1.4 CONFIRM the acceptance criteria have been met. I " 

6.1.5 Test Director VERIFY test is complete. 

Test Director Signature 


D ate 

006765.04000-FAT-O01-1 (Rev 7)

PREMIER TECHNOLOGY, INC. Projectflo. 006765.0.000 

(P ZI M I R WRP - 242-A Evaporator Ki Exhaust Contract 40167 * 

N'v~I~echnolog~ inc Ventilation System_____nPSE-66 

FACTORY ACCEPTANCE TEST PLAN SpecNo. R" 0 

6.1.6. QA Inspector VERUFY test is complete. 

QA Inspector Signature 

6.2 Valies/Dampers - Shell Leak Test 

MATRI REFER~ENCE - line 16 & 17 

Date 


BACKGROUND - This test is to show that valves meeting the ASME B3 1.1 requirements 

have no visual detectable leaks. 


*KI-HV-001 

9 ,-3V02 

KI-HV-003 

*KI-HV-00 

*KI-HV-017 

K 1l-HV-024 


*Visually detectable leakage through the pressure boundary is not acceptable. The 

pressure boundary includes, along with the body, bonnet, or Cover, all gasketed 

joints; however, leakage through the stem seals or stem packing shall not be cause 

for rejection. Stem seals or stem packing exempted from the shell test pressure 

leakage requirement shall be capable of retaining pressure up to the 38 0 C (I100 0 F) 

pressure rat ing without visible leakage. 

*Ultra High molecular Weight Polyethylene (UIIM PE) seats shall be tested in 

accordance with API 598 hydrostatic high-pressure closure test at 110% of the 

design differential pressure at the 100*F rating 

TEST PROCZDURE: 

6.21 REVWW manufacturer's certification documents located in Attachment 6.2 (see 

ABZ Valves & Controls Summary & Manufacture drawing 30" 402-205-Gear). 

6.2.2 -CONFIRM the acceptance criteria have been met by initialing data table. 

FIAT 6.2 ASME B31.1 Iiil 


006765.0.000-FAT-OO1-1 (Rev 7)


(i EM IER WRPS - 242-A Evaporator KI Exhaust Contract 40167 

\iw'Technology, '11c. Ventilation System No. 


FACTORY ACCEPTANCE TEST PLAN SpecNo. RPP.SPEC-36062 

Rev 

Valve List Satifed Unsatisied Test QA 

KCI-HV-001 K___________ 

ICI-HV-002 3 

K-IIV-003 

KI-HV-010 

X 

11 

'f 

K1-HIV-024,y 


Test Director Signature Date 

6.2.4 QA Inspector VERIFY test is complete. 

QA Inspector Signature Date 

6.3 Dampers - Pressare Drop 

MATRIX REFERENCE - line 18 

BACKGROUND - ASME AG-i, DA-51 10 Pressure drop data shall be based on tests 

performed in accordance with AMQA Standard 500. The AMCA Standard number used 

shall be stated with the pressure drop data., 


* Kl-MOV-001 

* KI-MOV-002 

0 KI-BDD-001 

* Kl-BDD-002 

e K1-)DMPR-001 

0 Kl-DMPR-002 

K ACCEPTANCE CRITERIA - Pressure drop wil be within 10% of value used to size the 

fan. Test data or manufacturer certification on damper style is acceptable.. 

-56u ie.-r Vrh'-'tI'. ;at AUIE?'QVu C -r 'FaJ'~ 



PiEMIER TECHNOLOGY, INC. ProjectNo. 006165.0.0007 

WRIS - 242-A Evaporator Ki Exhaust Cotr 40167 

\~ t mhooy n. -Ventilation System No.SEC366 



6.3.1 REvIEw manufacturer's certification documents located in Attachment 6.3 (see 

Quality verification Documentation page 3 and pressure drop chart) and fan sizing 

calculation. 

6.3.2 CONFIRM the acceptance criterion has bee met by initialing dataL table. 

FAT 6.3 ASME AG-1, DA-5110 Initials 

Test QA 

Damper list Satisfied Tisfed 7 kpao 

KI-MOV-001 IZ 

KI-MOV-001 Fk ' II .. 

KI-BDD-002 JL_ __ _ __ _ 

KI-DNM-401 y C f 

R1.DhM-002 y- M h 



*6.3.4 QA lnspector VERIFY test is complete. 


6.4 Dampers - Seat & Frame Leakage 

MATRIX REFEMENCE - line 20 & 21 

Date 

Date 

BACKGROUND - ASME AG-I, DA-5 130, Pressure plates shall be bolted to the inlet and 

outlet side of the damper. The chamber created shall be pressurized to the specified frame 

design pressure with the blades partially open. Testing industrial style dampers shall be in 

accordance with the bubble method. ASME AG-i, DA-5 140, Seat leakage testing shall be 

performed or verified after oycle time and cycle repetition testing and frame leakage testing. 


e KI-MOV-001 

* KI-MOV-002 

* Kl-BDD-0Ol** 


006765.0.0O0-FAT-O01-1 (Rev 7)


PREMIER TECHNOLOGY, INC. Prject No. 006765.0.000 

EM ER WRPS -242-A Evaporator KI Exhaust Contract 40167 

(D 

VentilationSystem ___o. ______ 

FACTORY ACCEPTANCE TEST PLAN Spec No. RPPSevO 60 

* Kl.BDD-002** 

* KI-DMPR-001 

*Kl-DMPR-002 

NOTE: "*Dampers that are only required to be cycle tested, frame bubble test will be 

conducted in 7. 10 and 7. 15 for customer information only. 


* The damper shall be bolted to a pressure chamber which is then pressurized to the 

specified blade design pressure. A bubble solution (a commercial test solution or a 

solution consisting of equal parts liquid detergent, glycerin, and water) shall be 

applied to the damper seat area to be tested. A few moments later, but before the 

soap solution can dry, check the wetted areas and mark places where bubbles are 

being generated. Unless otherwise specified, a leak indication is any bubble 1/6 in. 

(1.58 mmn) diameter that forms in I see, or a bubble 9/32 in. (7.14 mm) that forms in 

1 mmd. Movement of the blades and actuators and linkage shall be smooth and 

without hesitation, and limit switches operate in their intended position. 

* Meets Leakage Class IV (DA-I NOTE: (3) Leakage Class TV is for applications 

where leakage is of no consideration.) 


6.4.1 REVIEW manufacturer's certification documents located in Attachment 6.4 (see test 

report for each damper). 

6.4.2 CONFIRM th acceptance criteria have been met by initialing data table. 

FAT 6.4 ASMI AG-i, DA-5130 initials 

Dampr atifiedUnstisiedTest 

Lst 

Damer istSatslcd nsaisfedDirector 

QA 

Instiector 

K1-MOV-001 

I-MOV-0O2 VI OrZi~ 

KI-BDD-002~t2L 

______002 X_ _ _ _ _ I-If 


/ LJ~t 


16 Premier Technology, Inc. 006765.O.OO-FAT-001-I (Rev 7)

pRE2!mlIR TECHNOLOGY, INC. Project No. 006766.0-000 

(1~'T AM ER WRPS - 242-A Evaporator K1 Exhatust Contract 4016 

EMitg Inc. Vetilationi Systeim 

& nc.RPP-SPEC-36062 

Tecrjoog, 

No. 

FACTORy ACCE&PTANCE TEST PLAN Spec No. Rei 

6.4.4 QA In 3 to 7 VERIFY test is complete. 

.6.5 Filter Train -pressure 

MAT=I RnwmuNC - line 40 

Boundary Leakage 


BACKGROUND - BHEPA jilter' element holding frames at each filter position shall be 

press=redecay leak tested in accordance with the requirement of ASME N5 10, Section 7 

The filter trains shagl be pressure decay leak tested before test pro-fi1ter and HEPA filters are 

installed. Tetsal ecnuted to meet the riquiremetits of, ASM N51 0, Scin6 

COMPONENTBEIG TESTED: 

e Filter TrainlA 

& Filter Train B 

* Filter Train C 

ACCE'PTANC]& CRITERZIA -The leak rate shall not exceed 0.1% of the housing volume 

per hour at the system leak test pressure as defined in ASME AG-1 for leakage Class I 

(Table SA-B-13 10) 


6.5.j RVIEW xnanufactoreres certification documents located in Attachment 6.5 (see 

leak test report for each filter housing)- 

6.5.2 CONFIRM the accptance criterion has been Met by initialing data table.- 

FAT 6.5 AsmE N510 Initials 

Tod QA 

Filer rati istSaisfedUhsatisfied 

Filer rai stisedDiretor Lit 

1 

Filter Train A 

Filter Train B 

Filter Train C 

17 Premier Technology, Inc, 

006765..000FAT-001- (Rev 7)


PREMIER TECHNOLOGY, INC. ProjectNo. D06765.0.000* 

( KEMIN ER WRPS - 242-A Evaporator Kl Exhaust Crct~ 40167 

_ Tchnology Inc Ventilation System - NO. 

FACTORY ACCEPTANCE TEST PLAN Spec No. RPP-SPEC-3606Z 



/ 1 - 



QA Inspector Signature bate 

6.6 Instrumentation and power wiring - Continuity and megger testing 

MIATRIX REWEPXNCE - line 37 

BACKGROUND - This test is to show that all wiring is connected properly and meets 

industry standards. 

ACCEPTANCE CRITERIA - 

* Resistance shall be 5 1 ohm for continuity checks for wiring #14 AWG and larger 

and:S 3 ohms for wiring #16 AWG and smaller. 

* Resistance to ground shall be 50 mega ohm minimum. Conductors rated 2: 600 V 

used for services, feeders or branch circuits over 150 V to ground, Phase-to-Phase 

and Phase-to-Ground insulation resistance 200 mega ohms. (Voltage output of 

megger shall be 1000 V dc nominal). 


6.6.1 VERIFY continuity using Exhauster Electrical Assembly Traveler Attachment C - 

Continuity (see Attachmient 6.6). 

6.6.2 CONFIRM the acceptance criteria have been met 





18 Premier Technology, Inc. 006765.0.000-FAT-0O1-1 (Rev 7) 

4

P EMIERINo 


PREAM TECHNOLOGY, INC. Prjc~.0675000 1 


Inc. Ventilation SstemN. 

FACTORY ACCEPTANCE TEST PLAN SPec No. RI 

6.7 Pre-Filter Differential Pressure indicators - Verify' Differential Pressure 

Indicator Function 

MATRIX R~FER~ENCE - line 28 

BACKGROUND - Differential pressure is displayed and corresponding 4-20 mA signal is 

provided for operating range of -I to 9 inH2O. 


*PD1T-Kl -3 06 

*PDIT?-Kl -309 

*PDrr-K1-312 

ACCEPTANCE CRITERIA -Local 

output are within -1 to 9 inH2O. 


pressure indicationsi and corresponding 4 -20 mA 

6.7.1 VERIFY appropriate 4-20 mA using Ehauster Electrical Assembly Traveler 

Attachmnent b- Loop Check Table 1. (S69 -WA aMz',n ( .L-- 

6.7.2 CONFIRM the acceptance criterion has been met. 

6.7.3 PD]T-Kl-:306 Test DiretorZ. QA Inspector 

6.7A PDIT-Kl-309 Test DiretorX_-N. QA IispectorLkl 

6.7.5 PDLT-K1 -3 12 Test DirectorL?2. QA InSpetor~ k 


___ 

Li 1115I 

Tes;t irector Signature Date 

6.7.7 Q n tor VERIFY test is complete. 



Date 

006765.O.000-FAT-O01-1 (Rev 7)



E I R WRPS - 242-A Evaporator KI Exhaust Coutract 40167 

'A ciooy nVentilation System No. 

RPP-SPEC-36062 


6.8 Local I" Stage UEPA Section Pressure Indicators - Verify Differential 

Pressure Indicator Function 


BACKGROUND - Differential Pressure is displayed and corresponding 4-20 mA signal is 

provided for operating range of -1 to 9 inH 2O. 


* PDIT-K1-307 

e PDIT-KI-310 

* PDrT-Kl-')13 

ACCEPTANCE CRITERIA - Local pressure indications and corresponding 4 -20 niA 

output are withini 4to 9 ioIHaO. 


6.8.1 VERIFY appropriate 4-20 mA using Exhauster Electrical Assembly Traveler 

Attachment D - Loop Check Table 1 (see Attachment 6.7). 

6.8.2 CONFIRM the acceptance criterion has been met 

6.8.3 PDlT-Kl-')07. Test DirectorL ~ QA Inspeco 

6..4 PDT-l-10Tet 

irctr_& - QAInp c 

6 w. DTK 30Ts irco.~§ Q npco 

6.8.5 PDIT-Kl-313 Test Director..~. QA Inspector .lw... 





20 Premier Technology, Inc. 006765.0.000-FAT-O01-1 (Rev 7)


PREMIE TECHNOLOGY, INC. Project No. . 0066..0 

(~~1VIE~R WRPS - 242-A Evaporator Ki Exhaust Confrac 40167 

P~iTcnlg Rnc Ventilationl Stem NO. 

Rr?'.SPC36062 

FACTORY ACCEPTANCE MET PLAN LSpeeo. Re 0 

6.9 Local 2 nd Stage HEPA Section Pressure indicators - Verify Differential 

Pressure Indicator Function 


BaACKGROUND - Diffrrential Pressure is displayed and corresponding 4-20 MA signal is 

provided for operating range of -1 to 9 mnH 2O. 

COMPONENT B3EING TESTED: 

" PDIT-KI -308 

" PDIT-Kl-311 

" PDIT-Kl-314 

ACC1PTANCE CRMPRA - Localpressue indications anid orrspoding4 -20 mX 

output are within -I to 9 inH 2O. 


6.9.1 vsRIFY appropriate 4-20 mA using Exhauster Electrical AssemblY Traveler 

Attachment D - Loop Check Table I (see Attahment 6.7). 

6.9.2 CONF]IRM the acceptance criterion hats been met 

6.9.3 PDIT-Kl -308 Test Dietr~QA Inspector Ct:- 

6.9.4 PDIT-Kl-311 Test Direcorjn,. QA Inspetor.i G. 

6.9.5 PDIT-KI-314 Test Director_1L!%- QA Inspector 






Date 

Date 

006765.0.000-FAT-O01-1 (Rev 7)


PREMIER TECHNOLOGY, INC. Project No. 006'765.,000 

( E XIER WRPS - 24 2 -A Evapora t or Kl Exhaust Contract 406 

FACTORY ACCEPTANCE TEST PLAN ISpec No. I feo 

6.1OE xbaust Stack Sample Pitot Tube and Transport Lines - Leak test & Pitot 

Tube Alignment 

MATRIX RIF'ERENCE - line 46 

BACKGROUND - The stack sampling system shall be inspected for leaks at the time of 

installation in accordance with ANSI N13. 1, Section 6.9. PIC 3 stack allows for inspection 

as satisfactory method. Isolate and pressurize sample line to 5 psi. 


aExhiaust Stack sample pitot tube and transport lines 

ACCEPTANCE CRITERIA - No leaks detected using bubble testing on joints. 


6.10.1 REVIEW AMC Factory Acceptance test Report section 3.1 (e- *Tktt-6 .io 


6.10.3 Test Director VERITY test is complete. 


6.10.4 QA hInsector VERIFY test is complete. 1 


6.11 Mass Flow Controller, Record Sampler and Vacuum Pump 


BACKGROUND - RPP-SPEC-3 6062, Rev. 0, Section 3.3.4.2, # 10; Sample Flow 

Instrumentation: Each of the sample loops, including the record sampler loop and the CAM. 

sample loop shall include a mass flow controller Hastings model HFC-3 03, or Buyer 

approved equal. The flow controller shall send a 4-20 mA signal to the 242-A VCS and 

receive a 4-20 mA flew setpoint signal from the 242-A VCS. The sample flow will be held 

constant to accommodate the requirements of the collector or analyzer. 

COMPONENTS LIST: 

*22 Premier Technology, Inc. 006765.0.000-FAT-0O1-1 (Rev 7)

* 

PREMIER TECHNOLOGY, INC. Project No. 0067 5.0.0OO 

(~ W1 LIIR WRJ'S - 242-A Evaporator Ki Exhaust Contrat 40167 

VeEiltion te No. 


C 

RPP.SFEC-36062 

FACTORY ACCEPTAJNCE TEST PLAN spee Rev. 

*Mass Flow Controller Record Sampler and Vacuum Pump FCV-2. 

ACCEPTANCE CRITERIA -The flow read-out and totalizer function of the control valve 

will be within 10% of M&TE equipment (FAT only). Sample flow is constant as the 

exhauster flow is varied. Sample flow will be maintained at 85%. Record Sampler Flow 

Low Alarm at 85%/, indicator lights and strobe will activate. 

TEST PROCEDURR: 

* 1 6.11.1 REVIEW AMC Factory Acceptance Test Report section 4.2, 4.3, & 4.4 (NW sw e(wm 

6.11.2 CONflM the acceptance criterion has been met 

6.11.3 -Test Director VERIFY test is complete. 




6.12 Mass Flow Controller CAM and Vacuum PUMP 

mATRJX REFERENCE - line 48 

Date 

Date 

BACKGROUND- RPP-SPEC-36062, Rev. 0, Section 3.3.4.2, #10; Sample Flow 

bitrumentation: Each of the sample loops, including the record sampler loop and the CAM 

sample loop shall include a mass flow controller Hastings model HFC-303, or Buyer 

approved equal. The flow controller siall send a 4-20 mA signal to the 242-A VCS and 

receive a 42.20 mA flow set point signal from the 242-A VCS. The sample flow will be held 

constant to accommodate the requirements of the collector or analyzer. 

COMPONENTS BEING TESTED: 

*Mass Flow Controller Record Sampler and Vacuum Pump FCV-l 

ACCEPTANCE CRITERIA -The flow read -out and totalizer function of the control valve 

will be within 10%/ of M&TE equipment (FAT only). Sample flow is constant as the 

exhauster flow is varied. Sample flow will be maintained at 85%, CAM Flow Low Alarm 

activates at 85%, indicator lights and strobe will activate. 


006765.O.000-FAT-001-1 (Rev 7)


WRS-242-A Evaporator 1(1 Exhaust Czontract 

.~ehooy Inc. - Ventilation System No. 417 


FACTORY ACCEPTANCE TEST PLAN Spec No.IRe0 


6.12.1 REVIEW AMC Factory Acceptance Test Report section 4.2,4.3, & 4AW " -- O 

6.12.2 'CONFIRM the acceptance criteria have been met. 



6,12.4 QA Inspector VERIFY test is complete. 


6.13Vacnu m Pump - Verify Pump operation 

NOTE: see section 7.25 

6.14 Continuous Air Monitoring - Verify CAM Alarm and Interlock Set point 


BACKGROUND - RPP-SPEC-3 6062, Rev. 0, Section 3.3.4.2, #12: The local cabinet will 

have an alarm box assembly with indicating amber lights, a flashing beacon, and alarm bell. 

They will sound and illuminate when the alarmn condition exists. 

COMPONENT B~EING TESTED: 

. CAM Alarm and Interlock 

ACCEPTANCE CEJYCERIA - High Beta Alarm activates and exhauster fan shuts down at 

2000 CPM. Indicator light, strobe, and bell will alarm. MCS will display condition (signal 

output check in FAT). Exhauster fan shuts down on Beta monitor loss of signal. Indicator 

light and strobe will alarm. MCS will display condition (signal output check in FAT.). All 

exhauster automatic dampers and valves shall close on all exhauster shutdowns 

(continuity/voltage test). 


6.14.1 REVIEW AMC Factory Acceptance Test Report section 4.6 (e AMW&AA~ur & .10) 



PREMIER TECHNOLOGY, INC. project No. 006765.0.000 

(~ M ~ E 

E Inc. 

& Tecnolgy, ic. 

RS - 242-A Evapramtor Ki Exhaust 

Vettion Sstem 

FACTORY &CCEPTANCE TEST PLAN 

Contract 

No. 

SpecNo. 

406 

RP.SEC0 66 

Pwiehooy 

6.14.2 CONFIRM the accptanc,_criteria have been met. 

6.14.3 Test Djjtr VERIFY test is Complete. 

Test Direcator S ignature 


Date 

QA Inspector Signatur ' Date 

6.15 Sampler line Vacuum Indicator - Functional Test (P1-i1) 

NOTE: see section 7.3 0 

6.16 Sampler Line Vacuum Idicator - Functional Test (P1-2) 

NOTE: Section was remnoved; P1-2 does not exist on final design. 

6.17 CAM Operation - Verify No Electromagnetic Radiation Interference 


6.18 Sampling system instrumnentationl and wiring - Continuity 


BACKGROUND - Testing per RPP-SPEC-3 6062, Rev. 0, Section 4.1.9 

COMPONENT BEIG TESTED: 

.Electrical wiring 

*ACCEPTANCE c~iTE1A -Resistance shall be S 1 olum for continuity checks for 

wiring #14 AWG and larger and 5 3 ohms for wiring #16 AWG and smaller. 

TEST PROCEDUJRE: 

6.18.1 REVIEW AMC shop traveler for Instrumentation and Control Enclosure (see 

Attachment 6. 18). 

6.18.2 CONFIRM the acceptance criteria have been met. 


006765.O.OOO-FAT-OO1-1 




( WEM4IER 

~wiTcn~gy n 

WRPS - 242-A Evaporator Ki Exhaust 


ecPP-SPEC-36062 

FACTORY ACCEPTANCE TEST PLAN 

Contract 

No. 

Spec No. 

40167 

RPPSev 0 6 

6.18.3 Test Director VERIFY test is complete. .- 



/ /c~ 


6.19 Sample Cabinet cooling fan - Functional test 


6.20 Flow Sensor - Verify Exhauster Flow Indication 


BACKGROUND - This test is to verify Exhauster Flow Indications. 

COMPONENT BEING TESTED: ~ ~ 

0 Flow Sensor ('~Y~"~IJ 

ACCEPTANCE CRITERIA - Flow is indicated at a range of " O e 19,50& scfm 

TE ST PROCEDURE: 

6.20.1 REVIEW AMC Factory Acceptance Test Report Section 4.5, UeF AVIITA~k E1& .IeA4. 



/4 HI'4 





(~ 


E I R WRPS - 242-A Elvaporator K1 Exhavist Contract 06 

~Ventilationl System ____ 


rechrio~og~ 

rAcTORY ACCEPTANCE TEST PLAN Spec No,. 

RMPSPEC-36062 

Rev 

6.21 Sampling Manifold - Qualification of Filter Samplingr System 


BACKGROUND - Sampling manifolds shall be qualified to demonstrate that they collect a. 

representable sainple equivalent to a single-point sample taken at a point at least ten, duct 

diameters downstream of the filters. 


* Filter Traia A 

* Filter rain B 


ACCEpTANCE cRrTERIA - Sampling manifolds shall be kWxa to or greater than the 

concentration detected with the single-point sample. 


6.21.1 REVIEW manufactilrer's certification documents located in Attachment 6.21 

6.21.2 CONFIRM the acceptance criterion has been met by initialing data table. 

FAT 6.21 

Sit1ter Thin LWt Saddled 

ASME N510 

Duisfied 

Initials 

Test QA 

Diretor to 

*FilterTr,iaDB 

Filter Train A 

I-A 

e 

Cb 

iter Train, C X 

6.21.3 Test Director VFIUFY test is complete. 

* Test Director Signature 


27 Premier Technolog y, Inc. 

Date 

006765.O.OOO-FAT-OO1-1 (Rev 7


PREMER TECHNOLOGY, INC. Project No. 006765.0.000 

(iM IERT~' AWS - 242-A Evaporator KI Exhaust Contract 40167 

Tehooy n. -Ventilation System -. No. 

FACTORY ACCEPTANCE TEST PLAN spe No RPPSPEC,36062 

_______________ 

________________________ Rev 0 


6.22 Fan and Motor - Vibration ()Driv*e motor rotating elements) & Sound. 

MATRIX REFERENCE - line 5 & 7 

BACKGROUND - Prior to taking the vibration measurements, the fans shall be operated at 

the'normal operating speed for a ran in period of time until the bearings reach a stable 

equilibrium temperature L+3 0 F over 10 minutes). 

The fin speed for the impeller over speed test requirement is 15% above the speed with the 

fan operating with a motor input frequency of 60Hz. Motor and fan speeds shall be 

recorded. Sound power level ratings shall be taken in accordance with either AMCA 300 or 

ASEAE 68 


* KI-5-2 

9 Kl-5-3 

ACCEPTANCE CRITERIA - 

* The criteria for low horsepower, industrial process or petrochemical applications, 

FanApplication Category BV-3, 3.8 mm/s peak velocity (filter in). The impeller of 

each fan shall be over speed tested to a minimum of 15% above its maximum 

operating speed for 10 minute duration without increased vibration. Visual 

inspection shall serve to further verify that no deformation or cracks have occurred. 

" Mechanical equipment noise emissions at the maximum flow rate condition shall 

not create noise levels equal to or greater than 85 dBA 8-hour time weighted 

average, or equivalent noise dose, takcen 1 m away from source. 


6.22.1 REVICEW manufacturer's certification documents located in Attachment 6.22 (see 

Twin City Fan Test Procedure/Report Fan Vibration test Sound data will be attached 

in test report) 

6.22.2 CONFIRM the acceptance cr iterion has been met by initialing data table. 

FAT 6.22 Vibration Initials 


PREMIER TrECHNOLOGY, INC. ProjeetNo. 006765.0.000 

(~T~ AT R 

4T 

wRPS 242-A Evaporator KI Er~haUgt 

~Ventilation sstem 

ContrAct 40161 

FACTORY ACCEPTANCE TEST P'LAN SpUcNo. It 

E~quipmenlt Stsk UuibdD~eda -W 

K1-5-2 -4 

KI-5-3 

Equipment S~dDoo mc 

6.22.3 Test Director VBEFY test is complete. 


6.22.4 QAban ector VXBXFY test is complete. 


Date 

Date 


6.23 Inlet Plenum & Expansion Joints - Pressure Dlecay Test & Bubble Leak 

Test 

7 Procedure 


7.1 Valves/Damapers Visual Inspectionls 

* ]&.nIX PR PENCF, - linie 22 

BACKGROUND - (ASWvI AG-i TA-3510) a visual inspection is to be conducted to verify 

all components are istalled in accordance with the Owner's design specification. This 

inspection is to be co-nducted prior to releasing the equipment for normal operation. 

ASME AG-i TA--1200 DAMPER. INSPECT[ON ITEMS: 

* housing and duct interface 

. actuator linkage, motor, and controller 

0 interferences with moving parts 

* damper shaft seal 

0 blade edge seals and damper seat 


006765.O.OO-FAT-0O1-1 (Rev 7)


PREMIER TECHNOLOGY, INC Project No. 006765.0.000 

. P -., MT ju_/rRS VWPS - 24-2-A Evaporator I Exhaust Contract 40167 

\~.L~.~j.J.J..Ll.Ventilation SystemNo 

FACTORY ACCEPTANCE TEST PLAN Spec No. RP-SEC366 

* limit switches 

* supports and attachments 

'9 bolting and fasteners 

* electrical connections 

a as-built configuration in accordance with design drawings 

* damper nameplate 

m provisions for access for performing tests and maintenance 


* KI-MOV-001 

* KI-MOV-002 

* KI-BDD-001 

* Kl-BDD-002 

- K1-DhPR-001 

a Kl-DNTR-002 

ACCEPTANCE CRITERIA - Visual inspections are acceptable when there are no 

indications of improper installation, physical damage, structural distress or degradation that 

would impair the ability of the component or system to perform its intended fimotion. 

TEST PROCEDIJRE: 

7.1.1 VERIFY all inspection items listed in ASME AG-lTA-I-1200 

7.1.2 CONFIRM the acceptance criteria have been met for each damper. 

FAT 7.1 ASME AG-i, TA-3510 Iiil 

Daprit Improperly Installed Physical Damage Structural Distress Test QA 

Iapelis es No Yes No Yes No 'Drector Inkspector 

KI-MOV-001 

K1-MOV-002 __ 

KI-BDD-001 

KI-BDD-002 

Xl-DMPR-001 

Kl-DMPR-002 

30 Premier Technology, Inc. 006765.0.000-FAT-0O1-1 (Rev 7)

PREMIER TECENOLOGY, INC. Projeet No. 006765.0.000G 

~ ~~M ER WES - 24Z A vaor tor 1(1 EXhaust Conftic 016 

P " E IER: 

& Tcho]Og, nc FACTQRY ACCEPTANCE TES~PLAN Spec No. Re 0 


~ s-2"k SytemPN. M C-3 6 0 62 

7.1.3 .Test Director VERIY test is comaipete4 ve-' wait 


7.1.4 QA Inspector yERF testis comple 

QA inspector Signature 

7.2 Valve/Dampers - Verify Isolation Valve Position Indication and Function 

MATRIKX FERE9NCE -line 25' 

'BACKGROUJND - prior to the initial pressurizing of the dampe conirol system, Pneumatic 

system shall be checked for proper installation And 1eak-tightflesS. Dampers having remote 

position indicators shall be observed during operation to verify tgat the mechanical damper 

position corresponds to the remote indication, power-operated dampers shall be fuly cycled 

using a contrul switch or other actuating device to Verify operation. 

COMPONEZNT BEING TXSTE 

* KI-MOV-001 

" Kil-MOV-QO2. 

ACCEPTANCE CRMREIA- 

*ASME AG-i TA-4244 Verify that thp.dampers indicator corresponds to the remote 

indication. 

.ASNM AG-I TA-4245 Damper must fully Cycle 

*ASME AG-i TA-4246 Maximum time for any of the cycles shall be less than 20 

seconds. 

TEST PROCEDUPE- 

7.2.1 CONFIEM indicator mark position matches actual damper Position. 

7.2.2 RECORD the position of the shaft where it enters the duct in the table below (the 

mark should be perpendicular to the duct when the damper is Closed). 

31 Premier Technology, Inc. 0O75.OJA OI(ev) 

Dat 

Dt


PREAMR TECHNOLOGY, WNC. Project No. 006765.0,000 

UP~E MA IER WRPS -2Z42-A Evaporator Ki Exhaust Contr-d 40167 

~Technology, jic Ventilation SystemN. 

FACTORY ACCEPTANCE TEST PLAN Spec No. PP-SPE-36062 

____________________ 

_______________________________Rev 0 

7.2.3 ENSURE power to the controller/positioner is on (Note MPZ Breaker in the table 

below). 

7.2.4 'INSTALL temporary power source to TB-6 terminals 13 and 14 (this is to bypass the 

high radiation interlock to the fans). 

7.2.5 CHECK for Initial Voltage on the "D~amper Closed" terminal to ground - should be 

.0 VAC (See location in table below). 

7.2.6 CHECK for Initial Voltge on the "Damper Open" terminal to ground - should be 

120 VAC.(See location in table below). 

7.2.7 REMOVE the "Run Permissive (RPR) Relay" wire to prevent the fan from starting 

and protect it from shorting with a wire nut or other appropriate means (Get location 

ftrm table). 

7.2.8 SELECT Run on the VFD and verify that the dam per moves to the fll open position 

(Mark should be parallel with the duct) 

7.2.9 RECORD the Final Voltages of the "Damper Open" and "Damper Closed" 

terminals (These should be 120 VAC and 0 VAC respectively). 

7.2.10 RECORD the Final Observed position of the damper. 

7.2.11 RETURN the VFD Run switch to the Stop Position and note that the damper closes. 

7.2.12 RE-CONNECT the RPR relay wire. 

7.2.13 INITIAL for completion. 

7.2.14 REPEAT steps 7.2.2-7.2-12 for the other fan. 

7.2 Isolation Damper Position Initials 

ENCIld.i 

__ a0 Dam~per Cosed Toradls Damper pn Terminals~ 

Limpt Dtmt 0rIpe# TtPRQ 

Lit RRpesigiti amer ]3k, 

By Direotor Inspector 

MOV- 1 Tn-S 

001 #1 

X1. T&S 11 

Nov- 2 2 

002 

7.2.15 CONFIRM damper fully cycles. 


MBMIXR TECHNOLOGY, INC. Project No. OW6610.000 

ER WR PS - 242-A Evaporator KI Exhaust Contract 40167 

P noec Ventilation 8 Stemn No. 

FACTORY ACCEPTANCE TEST PLAN Spec No, Rev 0 

7.2.16 MEASUIM the time for the damper to fully open or fully close. 

7..7REMOVE temporary power from terminals 13 and 14 on TB-6. 


MC-MOV-001 

matches damper Damper Pully cycdes Te QA 

7.2.19 Test Director VERIFY test is competes III 


7.2.20 QA Insp ector RY eBIteis 011 WV , i~ 

QA Inspector $ignaline 

7.3 Filter Train - Visual Inspectioui 

MATRIX DFERENCE, - line 38 

Date 

Date 


BACKGROUND - (ASMB AG-i TA-3 510) a visual inspection is to be conducted to verify 

-all omponejIts ame installed in accordance with the Owner's design specification. This 

inspection is to be conducted prior the releasing the equipment for normal operation. A 

Visual inspection is to be performed on the filter train, inlet, outlet, cormmon switching 

plenum isolation valves, transition to fan inlet, and flexible metal connector sections in 

accordance with AG-I 


* Filter Train A 

* Filter Train B 


33 Premier Technology, Inc- 

006765..O00FATOO01-1 (Rev 7)



(P& EA4II3R MWIRWS - 242-A Evaporator KI Exhaust Contract 40167 

\ciTechnolog. nc. Ventilation System No. 

FACTORY ACCEPTANCE TEST PLAN Spec No. 

ACCEPTANCE CRMTRIA - Visual inspections are acceptable when there are no 


would impair the ability of the component or system to perform its intended function. 


7.3.1 VERITY all inspection items listed, check box for if item is free of physical damage, 

structural. distress or degradation that would impair the ability of the component or 

system of perform its intended function. 

FAT 7.3 ASME AG-i, TA-3510 

inpetin tes-Filter Filter Filter 

Insecton t~n5~Trai A Train D Train C 

Housing and duct connections (no caulking) ____ 

Access door scals ad gaskets 

Sample and injection ports, location and caps ____ 

Supports and attachments 

molting dframe cnsgdei 

Anstrumeltaconratonncodnce tdsg 

Housio5dc pntaio el 

lriionufor acessforke housing tests (flns 

mauntedanc 

Pleniatin alveetrtsselwdd 

7 la3es2 C ndtI rtheaccpac rtrahsbe mtfrec itrTan 

34 Premier moTnchnolgyam Iclapn 0076.0O8-ATOc (ev7



(t PV1PR W ps - 242-A4 Evaporator 1(1 xhausft Contract 416 

VetiatonSyte No. 

vent RPPtSflCsystem 


7.3.3 Test Director VERIFY test is cop~ft4 - ii-- '1PJ 


7.3.4 QA Inspector VERIFY test is 0mlt-' 

QA Inspoctor Signtature 

7.4 7242-4 Evaporator 1(1 Exhaust - Pressure Decay Test & Bubble Leak Test 

MATPIX REFERENCE - Line'23 

Date 

Date 

BA&CKGROUND - A pressure boundary: leak test shall be conducted to verify leaktightnesof 

the damper housing and interfaces with systehil in acordance with ASME ACY-1 

Section TA- 3 5 23. and Mandatory Appendix TA-M. (TA-3 5 23 -TA-rn- 100) SUMMARY 

OF METHOD Ducts and housings that form the pressureboundary of the system shall be* 

leak tested, with air, using one of the methods listed in this procedure. Either method may be 

used and will produce a similar test result The constant pressure method is useful for testing 

small volumes and is conducted at the maximum operating pressure for the system. The 

pressure decay method is useful in testing large volumes and is conducted by pressurizing to 

I % times the maximum operating pressure, then allowing the pressure to decay for a fixed 

period of timre, or until the pressure decreases to 80% of the maximum operating pressure, 

whichever obours first. Fans, dampers, and other components that ate part of the pressure 

boundary shIl be installed and tested with the pressure bo undary to verify interface 

*connection leak tightness. If the measured leak rate is in excess of the acceptance criteria, 

the leaks shall be located by one of the methods listed in this procedure. After leaks are 

repaired, the ducat and housing shall be reteste to verify leak-tightniess. 

COINPONENTS BNGTESTED: 

9 All gasket joints on the system 

ACCEPTANCE CRfl2RI: 

0 No bubble indications 

0 The leak rate shall not exceed 0.1% of the system volume per hour at the system 

leak test pressure as defined in ASME AG-1 for leakage Class I (Table SA-B-13 10) 


35. Premier Technology, Inc. 

006765.0.000-FAT-0O1-1 (Rev 7)



WRPS - 242-A Evaporator KI Exhaust 

_4__,___ 

Te6Ch loy - Ventilation System 

Contract 

N. 406 

FACTORY ACCEPTANCE TEST PLAN SpecNo. RPP-SPEC-36062 

~M IER ___ 

7.4.1 INSTALL blankng plate between each Fan Assembly and Fan to Switching Plenum 

Expansion Joint. (location 1 & 4) See Figure 7.4 Test Locations 

7.4.2 VERIFY valves/dampers are set in accordanc to valve line up table 96 

Valve/Damper Description Position Initials 

KI-HV-001 Inlet Plenum to Filter Train A ClosedV 

KI-HV-002 Inlet Plenum to Filter Train B Closed7 

KI-HV-003 Inlet Plenum to Filter Train C Closed d 

KI-HV-01O Filter A To Switch Plenum Open 

K1-IiV-017 Filter B To Switch Plenum Open 

KI-RV-024 Filter C To Switch Plenum Open 

KI-MOV-001 Plenium to Fan Isolation Damper (North) (Open) 

KI-MOV-002 Plenum to Pan Isolation Damper (South) (Open) _____ 

7.4.3 INSTALL pressure relief device set at 25 inH 2O 

7.4.4 PRESSURIZE system with compressed air to 1 4 times Max Operating Pressure 

(23.7 inH2O) 

7.4.5 CONDUCT bubble leak test in accordance with PT-TP-1.7 Rev 5 Bubble Leak Test 

Procedure. 

36 Premier Technology, Inc. 006765.0.0O-FAT-O0l-l (Rev 7)

PREMIER TECHNOLOGY, INC. Praject No. 006765.0.000 

W.RpS -242-A Evaporator K1 Exhaust Contract 40167 

A EMIER Vniainsse o 


& crchnoiogy, Inc. Vetlto Syte npp-SPEC-36062 ;No. 

FACTORY ACCEPTANCE TEST PLAN Spec No. RevO0 

91 

Figure 7.4 Test Locations 

7.4.6 VFRIFY no bubble indications are detected at locations shown if figure 7.4 Test 

Locations. 

FAT 7A4 ASME AG-i, TA-4233 & TA-4234 nfa 

Location V DeAzitO aise satused Directo Ins1 

2 KI-EJ-004 Ki-MOV-01 

3 Ki-MOV4Oi1 SECTION 4 ___ 

4 TEST PLATE 30-WJ-0113___ 

5 II-0 K1-MOV-M0 

6 KI-MOV-002 PLENUM 

8 SECTON I ETO 


___ 

006765.0.OOO-FAT-001-1 (Rev 7)



WRPS -242-A Evaporator KI Exhaust Conrct 406 

TR I RVentilation System No. 416 

FACTORY ACCEPTANCE*TEST PLAN Spec No. RPP-SPEC-36062 

____ ___ ___ ____ 

_ _ ___ ____ ___ ___ ____ ___ ___RevO 

FAT 7.4 ASME AG-i, TA-4233 & TA-4234 Initials 

LoaimDescription 

__________ From 

PLE NUM 

To 

PLENUM 

Unsatisfied 

Test 

Director 

QA 

InspectoroU 

----- 9 

11 

SECTION 2 

10 PLENUM 

10 SECTION 3 

FEN 

SECTION 4 

12 PLENUM 

SECTION 4 

SECTION 3 __ 

PLENUM 

SECTION 4 

PLENUM END 

CAP (NORTH)___ 

KI-EJ-001 

11 0 

13 KI-EJ-001 KI-HV-010 

14 KI-HY-OlO FJOLTER TRAIN A 

is PLENUM 

________SECTION 3 _____ ____ 

16 K1-BJ-002 KJ-I-017 

17 KI-HV-017 FILTER TRAIN B I 

is PLENUM 

_________SECTION 1I__ 

03 

- -- 

__ 

19 KI-EJ-003 1-HV4)U 4 

20 KI-RV-024 FILTER TRAIN C 

21 FILTER TRAIN C K1-RV-003 

22 FILTER TRAIN R K1-KW-002 

23 FILTER TRAIN A ICI-HV-001 

7.4.7 CONFIRM the acceptance criteria have been met by initialing table. 

7.4.8 CONDUCT rat of decay test in accordance with PTI TP-1. 15.6765 Pressure Decay 

Test, using 1949 f 3 (see Attachment 6.23) as the system volume and -23.7 inH 2O as 

the test pressure. 

7.4.9 CONFIRM TP-1. 15.6765 data table is complete. 

7.4.10 REMOVE blanking plates in all three locations. 


,!g CV 0§W_ fft 

'Test Director Signature Date 

7.4.12 QA Inspector VERIFY test is Complet " 


38 Premier Technology, Inc. 006765.O.OO0-FAT-01-l (Rev 7)

P EMIER vniainSse O 

PRtEMI= TECHNOLOGY, INC. Pi-oject No. 006765.0.000 

WRPS -22A Evaporator K1 Exhaust Contr~act 40161 

& echnolog, Inc. Venilaio Spcyo.temOBC 

FACTORY ACCEPTANCE TEST.PA pe o Rev 0 

7.5 Power Instrument and Control Cabling - Proper voltage and phase 

sequence at equipment served 

M~ATRIX REFERENCE - line 60 

BACKGROUND - Perform inspection during cable energizing. 


a; Power Instrument and Control Cabling 


ACCEPTANCE CRITERIA - Specified voltage (see table FAT 7.5) at equipment served. 

to applicable nameplate ratings. GFI, breakers, and other circuit protection devices function. 


7.5.1 RECORD equipment and calibration information. 

Equipment Model # Serial #Dte 

7.5.2 VERIFY that the power to the panel is on. 

Calibration Due 

7.5.3 MIEASURE voltage on the Bus-side of the panel using a calibrated Volt Meter. 

Record data in data table. 

Date 

NOTE- if the circuit is a GFCI press the test button and record proper function. 

7.5.4 V.ERIFY breaker is on. 

7.5.5 MEASURE voltage at the receptacle/equipment 


006765.0.O00-FAT-OO1-1 (Rev 7)


PREIIR TECHNOLOGY, INC. Project No. 006765.0.000 

f PV ?1\4 IER WRPS - 242-A Evaporator Ki Exhaust 

\ws/~mhnoioy h~.Ventilation System 

IFACTORY ACCEPTANCE TEST PLAN 

coot .. t 40167 

No.________ 

Sp,, No. P.PP-SPEC-36062 

___________________~~~Rn 

0_______________Rv 

7.5.6 INTIA2L each circuit as it is completed. 

FAT 7.5 Circu~it Breaker/Voltage and Phase Sequence Verification. Iiil 

Panel N Circuit Eupt F GFCl TEST sp~ecified Measured Test Q 

KIMP-OI I K] -MO V-001 NO 110 VAC 

KIMZO1 3 KI-MOV-002 NO 110 VAC 

KI-MPRZ-001 5.7 I-ENCL-400 NO 220 VAC 

K1.MPZ-001 6 kI-RCPT-001 YES 110 VAC 

K1-MPZ-001, 8 KI-Rr-PT.002 YES 110 VAC 

XI-MPZ001 9 K-RCPT-003 YES 10 

KI-MPZ-001 10 SPARE NOVC 

KI-MP-001 11 HET TAE YES 110 VAC 

K-P-0 2 SpAr N 110VC 


7.5.8 Test Director VERIFY test is compiI 

~ fJ 

~~~4 1S)5 I 

Test Director Signtr Date 

7.5,9 QAk Inispector VERIFY test is complete. 


7.6 Dampers - Damper Cycle Time and Operation 


BACKGROUND -ASME AG-I DA-5 121 The damper or louver assembly, as applicable, 

shall be cycled a minimum of 10 times from the full-open to the full-closed position to 

verify' the free operation of all parts and the correct adjustment, positioning, and seating of 

all blades. 

COMPONENTS BEING TESTE D: 

KI-BDD-001 

40 Premier Technology, Inc. 006765.O.000-FAT-OO1-1 (Rev 7)


ppyWMTECHNOLOGY, INC. ProjectNa. 0W0-750.00 

® M J R W1~pS 242-,, 1vaporatr K1 Eithaust o.tat 06 

& TechnlogyInc. P-.SPEC-36062 

FACTORY ACCEPTANCE TEST PLAN SRec 0o 

* KI-BDD-002 

*K1-DMPR-O01 

* KI-DMPR-002 

ACCEPTANCE CBITER[M- 

* Verf free operation of all parts and the correct adjustment, positioning. and seating 

of all blades. 

6 Maximum time for operation of any of the cycles shall be less than 20 seconds. 

& Movement of the blades and actuators and linkage shall be smooth and without 

hesitation. L- cai position indication oporates as required. 

TEST PROCEDUlU9:' 

7.6.1 VERIFY each damiper can be cycled 10 times 

7.6.2 CONFIRM cycle tine is less than 20 seconds 

7.6.3 CONFIRM dampers operate without hesitation. 


Fat 7.6 ASME AG-1, TA-4244, TA-4245 &TA-4246 initials 

Correct adustmeit Operates Smoothly Test QA 

Damper List Cycle Time ositlon, ad sefiln 0 Drco 

10-BDD-001 

KI-BDD-002 

7.6.5 Test Director VE3RIFY test is Ip 


7.6.6 QA inspector VERIFY test is eo 



Date 

Date 

006765.O.OO-FAT001-1 (Rev 7)

P$ 


PREMIER TECHNOLOGY, INC. Project No. 00676i.0.000 

LEM IJER WRPS - 242-A Evaporator Ki Exhaust Contract 40167 

~Tchnolo, Inc. Ventilation System No. 

FACTORY ACCEPTANCE TEST PLAN Spec No. RP- 0C366 

7.7 K1-5-2M Motor and VFD - Proper voltage at equipment served 

MATRIX REFERENCE - Mie 14, 15,26,27 & 74 

BACKGROUND - This test is to show that the fan motor supply voltage and amperage 

does not exceed the full amp rating of the motor excluding service factor considerations. 


" K1-5-2M 

* KI-5-2 VFD 

ACCEPTANCE CRITERIA - Thle fan motor supply voltage and amperage shall be 

measured for each phase. Motor current is not to exceed full amp rating (85.9 A) of motor 

excluding service factor considerations. Voltage will be within t 10% of the nameplate 

rating for the motor and VFD. Breakers and other circuit protection devices function. 



Equipment Model # Serial # Calibration Due 

____________ 

___________ ____________Date:- 

7.7.2 RECORD all initial VFD settings in table FAT 7.7. 

7.7.3 VERIFY valves/dampers are set in accordance to valve line up table 

Valve/Damper Description Position Initials q 

KI-HV-001 Inlet Plenum to Filter Train A Closed 

KI-UV-002 Inlet Plenum to Filter Train B Open 

K1-H[V-003 Inlet Plenum to Filter Train C Open 

Kl-HV-010 Filter A To Switch Plenum Closed 

42 Premier Technology, Inc. 006765..OO-FAT-OO1-I (Rev 7)

( EMIER w~" aNt'e"""t No. 

echnology, m ~'Ventilation Sse 

24',contact 40167 

FACTORY ACCEPTANCTSPAN peNo Rev 0 

KI-HV-017 Filter B To Swftch Plenum CIOsed. 

KI-HV-M2 Filter C To Switch Penum Closed 

K-MQV-OO1 Plnu a 1o ioato Damper (North) (Closed 

K1-O-0 plenum to Fan isolation Damper (Sorth) (Closed) 

KI-DMPR-OO2 Fan to Stack Isolation Damper (South) Open 

7.7.4 vE.RWY power tOboth VFD's are on. 

7.7.5 MASURE9 voltage oil the VFD Supply side and record value in table 


NOTE: if the voltage is higher than 600V. stop the test and resolve the issue before 

4 

continuing. 

7.7.6 CONNECT amps meter to the Phase A-of the Kl-5-2-M. 

7.7.7 SET the VEDspeedto10 Hz (17%/) 

7.7.8 INSTALL temnporary power source to TB-6 terminals 13 and 14 (this is to bypass the 


7.7.9 MXASVRE voltage at terminal 22 to neutral of relays KI -K-005 inside KI-ENCL- 

300, there should beiZO0 VAC at this terminal . (if not, this could indicate that there. is 

a high Radiation alarmn or that the control circuit fuise is blown resolve issue as 

needed.) 

7.7.10 MEASURE voltage atterminal 21 to neutral of relays K1-:K-005 inside Kl-ENCL-, 

300, there should be 120 VAC at this termninal. Note: checking initial conditions for 

fan KI-5-3 interlock., 

7.7.11 MEASURE resistance between terminals 7 ant 8 on TB6 in KI-BNCL-300 (should 

be > lOldl) Note: this checks initial condition for supply fan interlock relay KI-5-1 

7.7.12 OPEN the K.1-HV-017 and KI-EHV-024 dampers to 10% 

.7.7.13 START the motor and record the peak amperage as the motor winds up (should be 

less than 6X Name plate FLA rating). Note that the Kl-K-005 Relay changed stats. 

7.7.14 VERIFY KI -MOY-00l is open. 


006765.O.000-FAT-0OI-1 (Rev 7)



P EM JE R WRPS - 242-A Evaporator KI Exhaust C.nr.td 06 

& ~Tehnokogy, Inc, Ventilation System No. 407 

FACTORY ACCEPTANCE TEST PLANJSpec No. RPC6Q 

7.7-15 VIERIFY Kl-BDD-001 is open. 

7.7.16 MEASURE voltage at terminal 21 to neutral of relays K1-K-005 inside K1-ENCL- 

3060, there should be 0 VAC at this terminal. Note: this verifies that the K1 -5-3 fan 

interlock is enabled. 

7.7.17 MIASURE resistance between terminals 7 ant 8 on TB6 in KI -ENCL-300 (should 

be 0 Mf) Note: this verifies that the fan interlock relay Kl-5-1 is working properly. 

7.7.18 RECORD the amps on all three phases once the motor has come to steady-state 

operation. 

7.7.19 INCREASE the VED set point to 60 Hz 

7.7.20 VERIFY that the amp distribution across all phases is within 2% of each other. 

7.7.2 1 OPEN slowly the Kl-EHV-017 and KI-UV-024 to 50% 


operation. 

7.7.23 OPEN slowly the Kl-HV-017 and K1-HV-024 to 100% 


operation. 

Fat 7.7 VFD Output FLA Kl-5-2 InitiW 

RlyTerminal otge En VlaeF T Q 

RayStopped VRun xrector Imtector 

KI-K-00S 221Z 

R~esistance Check 0os OHMS Initials 

Resistance between terrninals'7 and 8 k 

Name Plate Data VD@1 9 1% 

IN Volts - -Phase inrush Dampers @ 10% Test QA 

ELA Volta Hz Pb-A Pb-B Ph-C Director Inspector 

amvs amos amp 

VFD @60Hz (100%) 

ampe rs @ 10% TT Dampers @ 50% Dampers @ 100% Iiil 

44 Premier Technology, Inc. 006765.0.000-FAT-001-1 (Rev 7) 

Iiil

TcchnPogyMInc. 

PREMYIER TECHNOLOGY, INC. ProjectNo. 006765.0.00 

P,-A ~vapo~r 

1 1 MR t -Tontract 406 

Ventilation SytemNo 

FACTORY ACCEPTANqCE TEST PLAN Spec No. FX 

PhAP bh-A -AP- h-C Ph-A Ph-B Ph-C 

gs 7.7.2 VEJY1- 

7.7.2 

O 0 

closed.F 

IEIF is AMPSD0 closed.omu 

7.7.29 ECOD) i all final VFD settngs 

7..3 CNIRM'e0cetne crteri haeben -t 

7.7.3 

MetietrV~Ft~i Z - &02 

7I7.= QA 

QA Inspcto Ma Sinaur 

45 rme Temolgin. 

Daedb 

FnpctrVdUYtstk 

0075..OOFT-a- 

bRel 


7)



(IE?~'AE 'WRPS - 242-A Evaporator Ki Exhaust Contract 40167 

\~m~'rchnioy; nc..~Ventilation System No. 

FACTORY ACCEPTANCE TEST PLAN Spec No. RPPEC-30 

7.8 KI-5-2 Fan and Motor - Vibration Test (Minimum System Loss) 

MATRIX REFERENCE - line 8,47 & 48 


the normal operating speed for a run in period of time until the bearings reach a stable 

equilibrium temperature, at which point the temperature no longer rises (+3*F over 10 

minutes).This test is to determine the vibration of the fan and motor under minimum system 

loss conditions (clean filters). This test is done to determine any problems in the system 

prior to the Fan Performanice/Airflow Capacity test. ASME AG- I TA-3533 - Vibration 

measurement shall be taken on the accessible motor/fan bearing housing in at least two 

different orthogonal planes approximately perpendicular to the line of the rotating shaft. 

When the bearing housing is not accessible the frame of -the component may be used if it 

will be representative of bearing housing vibration. 

COMPONE NTS BEING TESITED: 

a KI-5-2 Pan and Motor 

ACCEPTANCE CRITERIA. 

*Vibration: Measured in all three planes. The criteria for low horsepower, industrial 

process or petrochemical applications, Fan Application Category AMCA 204 BV-3, 

8.8 mm/s RMS velocity (filter out) 




7.8.2 INSTALL new clean filters in filter housings A, B, and C. 

7.8.3 ENSURE valve line-up is in accordance with valve table 

46 Premier Technology, Inc. 006765.O.000-FAT-001-1 (Rev 7)


PREMIER TECHNOLOGY, INC- project No. 006765.OJO00 

(V EIE 

%w hhooyIc 

RpS - 242-A Evaporator Ki Exhaust 

etlainSse 

ACCEPTANCEMn TES PLA 

FACTORY ACPACTETPA 

Contrac 

No. 

Se No. 

I -N 

406 

406 

V.PSP 3C-36062 

RevO 0 

Valve/Damper 

D Descrton Position Initials 

Kl-EV-0O1 Inlet plenum to Filter Train A Closed 

Yll-HV-002 Inlet Plenum to il1ter Train B Coe 

K.I-HV-003 Inlet Plenum to Filter Train C Wlse 

KI-DMPR-001 

Plenu to tan Isolation Damper (Nrh) (Cose 

KI DWKPR00Z Fan to Stack Isolation Damper (South) open 

7.8.4 vERIFY power to the VFD is on. 

7.8.5 CONSULT and IPLEM[ENT any additional safetay precaultionS as required by 

Premier 1ab-safety/safety-moflitor personnel. 

7.8.6 SET the VFD speed to 10 Hz.(17%) 

7.8.7 iNSTALL temporary po wer source to T13-6 terminals 13 and 14 (this is to bypass the 


7.8.8 OPEN K1-HWOO02 and Kl-HV-003 to 75 % 

7.8.9 START KI-5-2 fan and allow is to run for one hour. 

7.8.10 INCREASE VFD Hz setig until 13,500 scfm is Measured. 

7.8.11 CONFIRM fan and motor bearings reach a steady equilibrium temperature at which 

point the temperature no longer rises (+3 0 F over 10 minutes). 

7.8.12 MEASURE the differential pressure between P DIT location KI-PDIT-309 up stream 

of the filters and atmosphere, adjust valve setting until a differential pressure of -3.6 

+/- 0.5 inH2O is observed 

7.8.13 MEASURE the differential pressure between PDIT location Kl-PDIT-3 12 up stream 

of the fiter and atmosphere, adjust valve setting until a differential pressure of -3.6 

+/- 0.5 inH2O is observed 


006765.0.OO-FAT01-1 (Rev 7)


PREvMER TECHNOLOGY, INC. Project No. 006765.0.000 

S WRI'S - 242-.A Evaporator Ki Exhaust Conftat 40167 

VniainSystem No. 5EC366 

FACTORY ACCEPTANCE TEST PLAN Spec No. "PS 0 366 

7.8.14 RECORD controller out % on FITO 2 and 3, motor input frequency, differential 

pressure at PD]J7 location Kl-PDIT-3 09, differential pressure at PDIT location 1(1- 

PDIT-3 12, stack flow, motor current, motor and fan bearing temperature, fan shaft 

bearing vibration, and motor bearing vibration in Attachment 7.8. 

7.8.15 RECORD the %open of the FCV-1 and FCV-2 at 13,500 scfmn 

7.8.16 INCRE, ASE input frequency by .5 Hz and repeat steps 7.8.11 - 7.8.14 until fan 

reaches 19,500 scfin. 

NOTE: Data is to be taken over the entire operation range from 13,500-scfin to 

19,500-sofm at 30 rpm increments. In cases where the recorded values are close to 

the acceptance criterionreading are to be taken at 10 rpm increments. 

7.8.17 INCREASE input frequency to 60 Hz and repeat step 7.8.14. 

j7.8.18 RECORD the %open of the FCV-1 and FCV-2 at 19,500 scftn 

7.8.19 M[EASTJRE the differential pressure between PDIT location KI-PDIT-308 

downstream of the filters and 1 " nozzle located just above stack wye section. 

7.8.20 RECORD) PDIT to Stack differential pressure..j H 2 

7.8.21 REVIEW test results. 


7.8.23 'Test Director VERIFY test is coa ~e. 


7.8.24 QA Inspeo VERIFY estZist)omj), 


7.8.25 CONTIN[JE to, sound test 7.9 K-1-5-2 Fan and Motor - Sound Test 

48 Premier Technology, Inc. 006765.0.O00-FAT.-001-4 (Rev 7)


(~E 4I -R WRPS - 247,A Evaporator K1 Exhaust Contract. 40167 

\iwt~ehnk~g Ijc.Ventilation System No. 


FACTORY ACCEPTANCE TEST PLAN Spec No. RPPSev 0 -3 

7.9 KI-5-2 Fan and Motor - Sound Test 

MATRIX REFERENCE - line 5.. 

BACKCGROUND - This test is to show that the sound level ratings are in accordance with 

RPP-SPEC-36062. Rev 0 

ACCEPTA&NCE CRITERI - Mechanical equipment noise emission at the maximum 

flow rate condition do not create levels equal to or greater than 85 dBA over a.weighted 8hour 

average or equivalent 


.K175-2 Fan aud Motor. 

fl9ST PROd~IVZ 

7.9.1 RECORD equipment and caibration information. 

Mode # eril ~ aliraton Due 

Equipment 'oe#Sril#Date: 

7:9.2 VERIFY that the exhauster fan has reached steady state operation. 

7.9.3 RECORD max sound at I meter from mechanical equipment. Ala4 

Max sound level at I meter from mechanical equipment..... dBA 

NOTE: if any sound level is greater than 85 dBA the cause shall be determined and 

noted in Attachment 1. 



006765.0.OOO-FAT-O01-1 (Rev 7)


PREMIER TECHNOLOGY, INC. Projcct No. 006765.0.000 

( i iM ER VWS - 242-A Evaporator Xl Exhaust Contract 40167 

FACTORY ACCEPTANCE TEST PLAN Spec No. evPSPC-0 



7.9.6 QA Inspector VERIFY test is complee 


7.9.7 CONTINUJE to sound test 7. 10 Section 1 Valves/Dampers - System Pressure 

Bouniday Leak Test 

7..10 Section 1 Valves/Dampers - System Pressure Donn.dary Leak'Test 

BACKGROUJND - A pressure boundary leak test shall be conducted to verify leaktightness 

of the damper'housing and interfaces with system. 


0 Kl-BDD-001 

6 Kl-DvIR-001 

a KI-MOV-001 

ACCEPTANCE CRITERIA - no bubble indications 


7.10.1 SET fan speed to achieve 19,500 scfm. 

7.10,2 CONDUCT bubble leak test in accordance with PTI-TP-l.7 Rev 5 Bubble Leak Test 

Procedure. 

FAT 7.10 ASME AG-1, TA-4233 & TA-4234 Initials. 

From j~io To satisfied ~ Director Inspecto 

I STACK Kl-DMPR-001 ___ 

2 KI-DMPR-001 DUCT __ ___ 

3 DUCT KI-BDD-001 

1(-BDD-00l 

EXCPANTION 

EXPANTION FAN OTT 

________JOINT TRANSION ____________ 


- PpyMIER TECHNOLOGY, INC. Project No. 006765.0.000 

r~T~LA ER WRPS - 242-A Evaporator KI Exhaust Contract 40167 

\iiL~og .; Inc.Ventilation 

SystemN. 

FACTORY ACCEPTANCE TEST PLAN Spe No. 'Rev 0 


7.10.3 TEST KI -BDD-O01 frame f bubble leaks. (This is for customer information Only) 

VZPV ell[ 

TEST NOTES: Leak No leak 

(Add description of severity and location of leaks) 

7.10.4 CONFIRM the acceptance criteriafhave been met for each damper. 

7.10.5 Test Director VER1 FY test is completeJ 

Test Director S ignature' 

7.10.6 QA Inspector VERIFY test is comp~J~ 


Date 

Date 

7.10.7 CONTINUE to Kl-5-2 Fan and Motor 7.11- Vibration Test (Maximum System 

Loss) 

7.11 K1-5-2 Fan and Motor - Vibration Test (Maximum Systent Loss) 

MA&TIU REFERENCE - line 4,9,47 & 48 


the normal operating speed for a run in peripd of time until the bearinLgs reach a stable 

equilibrium temperature, at which point the temperature no longer rises (+3*F over 10" 

minutes). ASME AG-i TA-4159 Fan PerformanceAirflow Capacity Test For systems with 

filter or absorber banks, the fan performance shall be measured under maximum design dirty 

filter conditions. This may be done by increasing the system resistace to the design dirty 

filter differential pressure, (design basis maximum dirty filter condition), using artificial' 

resistance. 


*KI-5-2 Fan and Motor 


006765.0.OG0-FAT-0I-1 (Rev 7)


PREMIER TECHNOLOGY, INC. Project No. 00675~..00 

(~~P~A TP WRPS - 242-A Evaporator Ki Exhaust Contract 

'- Thnkry i.Ventilation System No. 416 


FACTORY ACCEPTANCE TEST PLAN Spec No. RPPeC-306 

* Vibration: Measured in all three planes. The criteria for low horsepower, industrial 


8.8 mm/s peak velocity (filter out) 

" Sample flow is constant as the exhauster flow is varied. Sample flow will be within 

2 scfin. 




7.11.2 MVEASUYRE the differential pressure between PDI]? location K1-PDIT-309 up stream 

of the filters and atmosphere; adjust valve setting until a differential pressure of -8.9 

+/- 0.5 inHO is observed. 

7.11.3 MEASURE the differential pressure between PDIT location Kl-PDIT-312 up stream 


+1- 0.5 in:H 20 is observed. 

7.11.4 MEASURE the differential pressure between PDIT location Kl -PDIT-3 08 

downstreamn of the filters and 1" nozzle located just above stack 'wye section. 

7.11.5 RECORD PDIT to Stack differential -presur ejn H0 lI" 

7.11.6 RECORD motor input frequency, differential pressure at PDIT location K1-PDIT- 

3109, differential pressure at PDIT location KI -PDT-3 12, stack flow, motor current, 

motor and fan bearing temperature, fan shaft bearing vibration, differential pressure 

at filter train PDIT's, and motor bearing vibration in Attachment 7.11. 


52 Premier Technology, Inc. 006765.0.000-FAT-00I-1 (Rev 7)


3iP zK ITTP WRPS - 242-A Evaporator Ki Exhaust Contract 4, 

Ventilation sstem 

No. 

7.11.8 ar0 

7.11.9 REVIEW test results 


FACTORY ACCEPTANCE TEST PLAN Sp-c No. RPPSey 30 6 


7.11.11 STOP motor and allow it to come to rest. 

7.11.12 REMOVE temporary power from terminals 13 and 14 on TB-6. 

7.11.13 Test Director VERIFY test is op 

Test Director Signatare 

7.11.14 QA Inspector VERIFY test is compete.,~ 


7.12 KI-5-3M Motor and VFD -Proper 

MATRIX REFERENCE - line 14,15,26,27 & 74 

Date 

Date 

voltage at equiipmnent served 




9 Kl-5-3 Fan and VID 

ACCEPTANCE CRITERIA - The fan motor supply voltage and amperage shall be 

measured for each phase. Motor current is not to exceed full amup rating (85.9 A) of motor 

excluding service factor considerations. Voltage will be yvithin + 10% of the nameplate 

rating for the motor and VFD. Breaker s and other circuit protection devices function. 


7,12.1 RECORD equipment aid calibration information. 

Equipment Model # Serial #. Calibration Due 


006765.O.OOO-FAT-O01-1 (Rev 7)


PREAMER TECHNOLOGY, INC. 'Project No. 006765..O000 

M IERRPS - 242-A Evaporator Ki Exhaust Contract 406 

& 11Fechnology' 111. Ventilation System No. 406 


~ ~~-Rev 0 

7.12.2 RECORD initial VFD settings in table FAT 7.12 C 


Valve/Damper Description - Position Initials 

KI(-iIV-0O1 inlet Plenum to Filter Train A Open 

KI-HV-002 Inlet Plenum to Filter Train B Open 

KI-HfV-003 Inlet Plenum to Filter Train C Closed 

K1-{v-01O Filter A To Switch Plenum Closed 

KI-HV-017 Filter B To Switch Plenum Closed 

KI-ITV-024 Filter C To Switch Plenum Closed 

KI-MOV-001 Plenum to Fan Isolation Damper (North) (Closed) 

Ki-MOV-02 Plenum to Fan laclation Damper (South) (Closed) 4 

KI-DMP>R-00I Fan to Stack Isolation Damper (North) Open 

KI-DMPR-002 Fan to Stack Isolation Damper (South) Open 

7.12.4 VERIFY power to both VFD's is on. 

7.12.5 MEfASIJRE voltage on the VFD Supply side and record value in table 

NOTE: if the voltage is higher than 600V stop the test and resolve the issue before 

continuing. 

7.12.6 CONNECT amp meter to Phase A of the KI-5-3-M. 

7.12.7 SET the VFD speed to 10OHz (17%) 

7,12.8 INSTALL temporary power source to TB-6 terminals 13 and 14 (this is to bypass the 

high radiation interlock to the fans)., 

54 Premier Technology, Inc. 006765.O.OOO-FAT-001-1 (Rev 7)

PREMIER TECHNOLOGY, INC. Proj ect No. 006765.0.00 


(1.E\JER WRPS - 242-A Evaporator 1(1 Exhaust Contract 40167 

\(wi'echnoogyy, 11C. VetltonSse No. 

SpcN. RPP-PEC-36062 

FACTORY ACCEPTANCE TEST PLANI RpeeN. 

7.12.9 MEASURE voltage at terminal 22 to neutal of relays Kl-K-006 inside K .I-ENCL- 

300, there should be 120 VAC at this terminal. (If not, this could indicate that there is 

a high Radiation alarm or that the controcircuit fu.selis blown resolve issue as 

needed.) 

7.12. 10 MEASUJRE voltage at terminal 21 to neutral of relays K1I-K-006 inside K1 -BNCL- 

300, there should be 120 VAC at this terminal. Note: checking initial conditions for 

fan Kl-5-2 interlock. 

7.12.11 MEASURE resistance between terminals 23 ant 24 on TB6 in KI -ENCL-300 

(should be > Il00kal) Note: this checks initial condition for supply fan interlock relay 

KI1-5-1 

7,12. 12 OPEN the KI-R-010 and KI-EIV-O11 damers tol10% 

7,12-13 START the motor and record the peak amperage as the motor winds up.(should be 

less than 6X Name plate FLA rating). Note that the KI -K-006 Relay changed states. 

7,12.14 VERIFY KI-MOV-002 is open. 

7.12.15 VERIFY Kl-BD-002 is open. 

7.12.16 MEASURE voltage at terminal 21 to neutral of relays KI-K-006 inside KI-ENCL- 

300, there should be 0 VAC at this terminal. Note: this verifies that the KI-5-2 fan 


7.12.17 MEASURE resistance between terminals 23 ant 24 on TB6 in KI-ENCL-300 

(should be 0 kfl) Note: this test is to verify' supply fan interlock for Kl1-5-1 is 

workcing properly.. 


operation. 

7.12.19 INCREASE the VFD set point to 60 Hz 

7.12.20 VERIFY that the amp distribution across all phases is within 2% of each other. 

7.12.21 OPEN slowly the K1-IEV-010 and KI-EHV-017 to 50% 


operation. 


006765.O.O00-FAT-O01-1 (Rev 7)



(ThjiEM1'ER WRPS - 242-A Evaporator K1 Exhaust Contract 40167 

\wai~chnolo)gy, Inc. -Ventilation System No. 

FACTORY ACCEPTANCE TEST PLAN Spec No. RP.SPEC-36062 

____ ___Rev ____ ____ 

0 

7.12.23 OPEN slowly the KI-EHV-010 and KI-HV-017 to 100% 

7.12.24 RECORD the amps on all three phases once the motor has came to steay-state t 

operation. 

Fat 7.12 VFt) Output FLA KI-5-2 initials 

RMay Terminal 1Voltage Fani -voltage Fain Test ;A 

, 

-KSlowed Running Director As ector 

1(1-K-006 22 

Resis tan ce Check j OHIMS OHMS Z Initials 

Resistance between terminals 23 and 24 J_________ 

NamuePlate Data 

IN Volts A-Phase Inrush 

V'FD @10Hz (17% 

Dampers @1I Test QA: 

FLA Volts IH. Ph-A Pb- Ph-C Drco npco 

_______________ VFD @60Hz (100%) 

Dampers @ 10% Dampers @ 50% /Dampers @ 100 Initials 

Ph-A IPh-B Ph-C Ph-A Ph-B Ph-C bP-A Ph-B 1Pb-C 

ap amn .P.~ aw aMp SPam RI amps amps 

___Initial VP]) Settints Finafl Settigs 

ICC 

CFG 

U~r 

____ 

IFLO 

A02 

Al2t 

____ 

ICC 

QG 

bFr 

_____ 

FLO 

A 

Al2t 

ACC ACC____ 

dEC _______ A bk _____ dEC App)Fdbk 

LSP _____ Ref _____ ISP App Ref 

sFr 

tCt 

CrL2 

______ in Fdbk 

XMax Fdbk 

Z Min Ref 

_____ SFr 

itCt 

CrL2 

_____Min Fdbk 

Max Fdbk 

Mmn Ref 

r2____ 4 Max Ref _____ r2 ____ Max Ref _____ 

Flu 

CHCF 74PG 

Int Ref _____ FRI 

CIICP 

_____ 

__ 

Intkef 

PG 

-nST )c___ 10 T ____ IG 

rb ____ DO rCbs ____ D ___ 

Fri _____ Ramp Frib I____ tI amn 

99f _____ Min Out _____ liSf Min out ______ 

_____ IM2 Out FLR ____Max Out 

OPL IRev I IOPL I___ I Rev 



PREMIER TECHINOLO)GY, INC. ProjectNo. 006765.0.000 


WRPS - 242-A Evaporator Ki Exhaust contract 40167 

TTVentilation System No. RIPSC366 

-60o gy,11c, FACTORY ACCEPTANCE TEST PLAN Speco RMSEC- 0 

7.12.26 VERIF~Y Kl-MOV-002 is closed. 

7.12.27 VERIFY KI-BDD-002 is closed. 


7.12.29 RECORD final VFD settings. 

7.12.30 CONFIRM the acceptance critei have been met 

7.12.31 Test Director VERIFY test is cmlt 

~14 rr0~~ahpopir 


7.12.32 Q4 ispctrVERIFY testisonea 

QA Wnpector Signature 

Date 

Date 

7.13K:1-5-3 Fan and Motor -VbainTest (Minimum System Loss) 


BACICGROUIID - Prior to taking the vibration measurements, the fans shall be operated at 

the normal operating speed for a run in period- of time until the bearings reach a stable 

equilibrium temperature, at which point the temperature no longer rises (+3 *F over 10 

minutes).This test is to determine the vibration of the fan and motor under ninmum system 


prior to the Fan Perfornaiie/Airflow Capacity test. ASMB AG-I TA-3533 - Vibration 

measurement shall be taken on the accessible motor/fkn bearing housing in at least two 

different orthogonal planes approximately perpend icular to the line of the rotating shaft. 

When the bearing housing is not accessible the frame of the component may be used if it 

will be representatve of bearing housing vibration. 

CONIPONENTS BEING TESTED: 

0Kl-5-3 Fan and Motor 



006765.0.000-FAT-001-1 (Rev 7)


PREMIER TECHNOLOGY, INC. ProjetNo. 006765.9.000 

IE WRS 11-AEvaporator K1 Exhaust Contract 406 

EM 

m entilation Systemn No. 407 

FACTORY ACCEPTANCE TEST .PLAN Spec No. RPP-SPEC-36062 

_____________ ___________________Rev 0 

Vibration: Measured in all three planes. The criteria for low horsepower, industrial 


8.8 minis RMS velocity (filter out) 


7.13.1 CONFIRM new clean filters are installed in filter housings A, B, and C. 


Valve/Damper Description Positiona Initials 

KI-RV-001 Inlet Plenum to Filter Train A Closed 

Y-1-HV-002 Inlet Plenum to Filter Train B Closed 

KI-EHV-003 Inlet Plenum to Filter Train C Closed 

K1-HV-01O Filter A To Switch Plenum Open 

KI-RV-017 Filter B To Switch Plenum Open 

KI-H[V-024 Filter CTo Switch Plenum Closed 


KI-MOV-002 Plenum to Fan Isolation Damper (South) (Closed) 

Kl-DNWR-00i1 Fan to Stack Isolation Damper (North) Open 

K1-DNWROOU- IFantoStack ,Iation Damper(South) Open ____ 

7.13.3 VERIFY power to the VFD is on. 

7.13.4 CONSULT and ThILEM[ENT. any additional safety precautions as required by 

Premier lab-safety/safety-monitor personnel. 

7.13.5 SET the VFD speed tolo0Hz(17%) 

7.13.6 INSTALL temporary power source to TB-6 terminals 13 and 14 (this is to bypass the 


7.13.7 OPEN KI-HV-001 and Kl-HV-002 to 75 % 

7.13.8 START Kl-5-3 fan and allow it to run for one hour. 

7.13.9 INCREASE VFD Hz setting until 13,500 scfni is measured. 

58 Premier Technology, Inc. 006765.0.OO0-FAT-O01-1 (Rev 7)


PREIMfERTECHNOLOGY, INC!. Project No. 006765.0.000 

IEM R 'wRPS - 242-A Evaporator 1(1 Exhaust 

\~Tch okg ~Ventilation System 

qtontraet 

No. 

406 

FACTIORY ACCE&PTANCE TEST PLAN SpecNo. - SE-66 

( h 

7.13.10 CONFIRM fan and motor bearings reach a steady equilibrium temperature at which 

point the temperature no longer rises (W3F over 10 minutes). 

7.1'3.11 MEASUR~E the difeential pressure betwee PDIT location Ki-PDIT-306 up stream 

of the filter and atmosphere, adjust valve setting until a differential pressure of -3.6 

+-0.5 inH2O is observed 

7.13.12 MEASURE the differential pressure between PDIT location K1-PDIT-309 up stream 


+-0.5 inH20 is observed 

7.13.13 RECORD Beta and record flow from I1TC 2 & 3, mot or input frequency, 

diferential pressure at PD1T: location KI-PDIT-306 , differential pressure at PDIT 

location K1-DTM309, flow at 'stack sixnpling, motor current, motor and fan beating 

tertpertore, fan. sh~ft bearinig vibration, differential pressure at filter train PDrr's, ..and 

motor bearinig yibration in Attachment 7.13. 

7.13.14 INCREASE input frequency by .5 Hz and repeat steps 7.13.11 - 7.13.13 

NOTE- Data is to be taken over the entire operation range from 13,500-scfln to 

19,500-scfmn at 30 rpm increments. In cases where the recorded values are close to 

the acceptance criterion, reading are to be taken at 10 rpm increments. 

7.13.15 MEASURE the differential pressure betwee PD1T location K1-PDIT-3 14 

downstream of the filters and 1" nozzle located just above stack wyc section, 

7.13.16 RXCO1kD PDIT to Stack differenttial pressure 0!!7jnizo 

7.13.17 REVIEW test results. 


7.13.19 Test Director VERIFY test is cop - $T 

Teat Director Signature 

7.13.20 QA Inspector VERIFY test i;cmlt 



Date 

Date 

006765.O.000-FAT-O01-1 (Rev 7)



ciU EA IER VWPS - 242-A Evaporator KI Exhaust Contract 

FACTORY ACCEPTANCE TEST PLAN S&"cNo. RPP-SPEC-36062 

7,13.21 CONTINIJE to 7.14 KI-5-3 Fan and Motor - Sound Test 

7.14KI-5-3 Fan and Motor - Sound Test 


BACKGROUND - This test is to show that the sound level ratings are in accordance with 

RPP-SPEC-36062, Rev 0 


KI-5-2 Fan and Motor 

ACCEPTANCE CRITERIA - Mechanic41 equipment noise emission at the maximum 

flow rate condition do not create levels equal to or greater than 85 CIBA over a weighted 8hour 



7.14.1 VERIFY that the exhauster fan has reached steady state operation. 

7.14.2 RECORD max sound at 1 meter from mechanical equipment. 

Max sound level at 1 meter from mechanical equipment: r- dBA 

NOTE: if any sound level is greater than 85 CIBA the cause shall be determined and 





7.14.5 QA Inspector VERIFY test iscope. 


7.14.6 CONTINUE to sound test 7.15 Section 2 Valves/Dampers - System Pressure 

Boundary Leak Test 




(~R.MIIER WRpS - 242-A Evaporator KI Exhaust otat 401,67 

~lcc,~g~Ic VentilftfiOl Sstem apNo.M6 

FACTORY ACCEPTANCE TEST PLAN o.~ Rev 0 

7.15 Section 2 Valves/Dampers - System Pressure Boundary Leak Test 

BACKGROUND - A pressure boundary leak. test shall be conducted to verif leak- 

tightness of the damnper housing and interi'aces with system 

COMPONENTS BEIG TESTED: 

*KI-BDD-002 

*KI-DMPR-002 

*Kl-MOV-002 

ACCEPTANCE CRffER1A - no bubble 'indications 

TEST PROCEDURMi 1 .;:1 

7.15.1 SET fan speed to achieve 19,500 scfn. 

7.15.2 CONDUCT bubble leak test in accordance with PTI-TP-1 .7 Rev 5 Bubble Leak Test 

Procedure. 

FAT 7.15 ASME AG-i, TA-4733 &TA-4234 Initials 

LoainDes 

Lnctio 

tion 

To Tof~c 

Saified Ua*-ie Test 

Director~ 

QA 

IMsPoc i 

1 STACK KI-D)MYR-I01 

.2 KI-DMPR-01 DUCT 

3 DVjCT VJ-BDD-002 

4 . KI-BDD-001 JM O 

EA NTN FAN OUTLET 

JOIN 

TRANSION 

7.15.3 TEST KI-BDD-002 framne for bubble leaks. (This is for customer inforination. only) 


TEST NOTES: Leak No leak 

vat) _ __ __ _ __ _ 

(Add description of severity and locatio of leaks) 

006765.O.000-PAT-0O1-1 (Rev 7)


FREM[ER TECHNOLOGY, INC. Project No. 006765.0.000 

( ~EM IRI) WRPS - 242-A Evaporator KI Exhaust 

\,,,~i~ehnooy; nc.Ventilation System 

Contract 

No. 

406 

406 



-Rev 0 

7.15.4 CONFIM the acceptance criteria have been met for each damper. 

7.15.5 Test Director VERIFY test is coxpl~ 7 j 1 

'e~rv-eI b 91 


7.15.6 QA Inspector VER Ytest s co jI" 


7.15.7 CONTINUE to sound test 7.16 Stack Joint -onayLeak Test 

7.16 Stack Joint - Bubble leak test 

BACKGROUND - ECN 727024 test is to be performed per ASME AG-l (SA-4533) a 

bubble leak tests is to be performed to ensure t hat unmonitored exhaust does not escape 

through the joint. The leak test shall be set-up to mimic the on-site conditions, specifically 

with respect to gasket material and size, hardware material and size and torque applied to the 

bolting. 


Stack Assembly gasketjoint 

ACCEPTANCE CRITERA - NO Bubble indications 


7.16.1 CONFIRM sampling monitoring system is operating. 

7.16.2 CONDUCT bubble leak test in accordance with PTI-TP-1.7 Rev 5 Bubble Leak Test 

Procedure at all mechanical joints listed for equipment in table below. 

FAT 7.16 ASMiE AG-i, TA-4233 & TA-4234 initials 

Equipment Frm Descripition To Satisfied tid Test 1 QA~ 

62 Premier Technology, Inc. 006765.O.O00-FAT-OG1-1 (Rev 7)


PREMME TECHNOLOGY, INC. Project No. 06765-0.000 

(iI~E I R WRpS - 242-A Evaporator Ki Eihanst Contract 406 

&,e~Technology, Inetca.n te o i'P-STEC36062 

FACTORY ACCEPTANCE TEST PLAN *Spec No. -R 0 

7.16.3 CONFIRM the acceptal)ce criterion has been met 

7.16.4 Test Director VE2RIFY test is cop - jjia I 

~ £. ~-C.( C.-' F 


7.16.5 QA Inspector VERIFY test i 

QA Inspector signature 

Date 

Date. 

7.16.6 CoNTINUE to 7.17 1(1-5-2 Fan and Motor -Vibration Test (Maximum System 

Loss) 

7A17 KI-5-3 Fan and Motor - Vibration Test (Maximum Syste m Loss) 

MAT=I~ pEFERENCE - Hune 4 & 8 

BACKGROUND - prior to taking the vibration measureents, the fans shall be cperated at 


equilibrium temperature, at which point the temperature no longer rises (+3 0 F over 10 

minutes). ASM.E AG- I TA-4159 Fan Petformance/Airflow Capacity Test For systems with 

filter or absorber banks, the fan perforM11nce shal be measured under maximum design dirty 

filter conditions. Thi may be done by increasing the system resistance to the design dirty 

filter differential pressure, (design basis maximum dirty filter condition), using artificial 

resistance. 


.Kl-5-2FanfdMotor 


a Vibration: Measured in all three planes. The criteria for low horsepower, industrial 




-006765.0.OOO-FAT-0O1- (Rev 7)


i PREMIOER TECHNTOLODGY, NC. Project No. 006765.0.000 

J ~MH ER WRPS - 242-A Evaporator Ki Exhaust Contract 406 

1Ri-Chnolog. 111C. Ventilation System No. 4016 

FACTORY ACCEPTANCE TEST PLAN spec No. RPPSC-W62 

_____________________________________________________Revo 



of the filters and atmosphere, adjust valve setting until a differential pressure of 8.9 

+-0.5 inH 2O is observed 

7.17.2 MEASURE the differential pressure between PDIT location Kl-PDIT-309 up steamn 

of the filters and atmosphere, adjus valve settinig until a differential pressure of 8.9 

+-0.5 in}{ 20 is observed 

7.17.3 MEASURE the differential pressure between PDIT location K1-1'DIT-314 

downstream of the filters and 1" nozzle located just above staye sect 

7.17.4 RECORD PDIT to Stack differential pressure nH 2 0 

7.17.5 RECORD motor input frequency, differential pressure at PDVT location KI -PDIT- 

306, differential pressure at PDfl' location K1-PDIT-309, flow at stack sampling, 

motor current, motor and fan bearing temperature, fan shaft bearing vibration, and 

motor bearing vibration in Attachment 7.17. 





7.17. 10 Test Director VERIF'Ytestiscope. 


7.17.11 QA hispector VERIFY test is cmIit 

6W (T #6A-f(eU -r:: /L 


7 .181Filter Train A - Airflow Distribution (Fall Systemi) 

MATRIX REFERENCE - line 42 A&Q Lj, "D 4c 4,- ~J 


(VEMVntlainERse 


PREMIER TECHNKOLOGY, INC. Project No. 006065.000O 


FACTORY ACCEPTANCE TEST PLAN SPecNo. wr-, CM 

BACKGROUND -th& section provides the field acceptance test requirements for installed 

pre-flter and KEPA filter banks. Acceptance tests shall 1 be conducted with pre-filter and 

HqEPA filter banks installed. (ASMB AG-I TA-4632 Airflow Distribution. Test) With the 

system operating at design flow rate (18,000 sei; 19,500 max) the airflow distribution shall 

be measured downstream of each pre-filter and HEPA filter bank. 

CO1%~IoNENTS ]BEING TESTED: 

a Filter Train 

0 inlet 

& Outlet 

* Common switching plenum 

a isolation valves 

* Transition to fan inlet 

.. .* Flexible mqta connector 

Ductwork 

ACCEPTANCE CRTIA -Velocity measurements across the HEPA filter banks sha) 

be limited to ±201/ of the average./ 

TEST PROCEDVU: 

7.18.1 ENSURE valve line-up is in accordance with valve tablefL 

Vave/Damr Deciio POSitOn ntil 

K3-EV-OO1 Inlet Plenum to Filter Train A Closed 

KI-!:V-001 inlet Plenum to Filter Train B Closed 

K1-EV-003 Inlet Pleaum to Filter Train C CIOse 

KI-HV-010i Filter A To Switth Plenum open 

IU-HV-017 Filter I To Switch Plenumn Open 

KI-EV-024 Fiter C To switch Plenum Closed 

KJ-MOV-001 Plenm to Fan isolation Damper (North) (lsd) 

XI-MOV-002 plenum to Fan isolation Damr (sou-th) (led) 

K1-DMPR-001 Fano to Stack Isolation Damper (Nort) Open 

KI.DNMR0 .. Fan to stack isolation Damper (South) Opens 

7.18.2 VERIFY power to theVFD ison. 


No. 

006765..000-FAT-00l-l (Rev 7)


PREMIER TECH3NOLOGY, INC. Project No. Q06765..000 

(~ ~ M J R WRPS - 242-A Evaporator K1 Exhaust Contract 40167 

FACTORY ACCEPTANCE TEST PLAN Spec No. RPPSPC-3O6 

RevO0 

7.18.3 CONSULT arnd IMEPLEIMENT any additional safety precautions as required by 


7.18.4 SET the VFD speed to the required Hz to achieve 18,000 scfin ±1 0% (use 

Attachmnent 7.18 information) 



7.18.6 OPEN KI -HV-001 and Kl-HV-002 

7.18.7 START Kl-5-3 fan 

7.18.8 RUN NUCON procedure 12-101 rev 7 (Attachment 7.18) 


7.18.10 Test Director VERIFY test is omlt 

Aa/J S r-S&"nj c 


7.18.11 QA Inspector VERIFY test is compete, 


7.18.12 CONTINUE to 7.19 Filter Train B - Airflow Distibution (Full System) 

7.19 Filter Train B - Airflow Distribution (Full System) 


BACKGROUND --this section provides the field acceptance test requirements for installed 

pre-filter and HEPA filter banks. Acceptance tests shall be conducted with clean pre-filter. 

and BPA filter banks inastalled. (ASME AG-i TA-4632 Airflow Distribution Test) With 

the system operating at design flow rate (18,000 cfmn; 19,500 max), the airflow distributiou 

shall be measured downstream of each pre-filter and HEPA filter bank. 


0 Filter Train 

a Inlet 

66 Premier Technology, Inc. 006765.O.000-FAT-00I-l (Rev 7)


PREMIER TECHNOLOGY, INC. ProjedtNo. 00676S5A000 

NWS - 242-A EVaporator KI Exhaust 

(VEMIERtinSgeNo 

& Tcchnology, In. Vetlto Sse 

contract 

o 

401j67 

RpP.SPKC-36062 

FACTORY ACCEPTANCE TEST PLAN Revc 0o 

* Outlet 

*'Common switching plenum 

*Isolation valves 

*Transition to fan inlet 

*Flexible metal connector 

*Ductwork 

ACCEPTANCE CRITERIA - Velocity measurements across the HEPA filter banks shall 

be limited to ±20'/o of the average. 


7.19.1 RUN NUCON proced=r 12-101 rev 7 (Attachment 7,18) 

7.192 CONFIRM the icoolta13c criterion haes been met for each damper. 

7,19.3 Test Director VERIFY test is o'P , 


7.19.4 QA lnsiector VERIFY test is 00 

Date 

7,19.5 QAlInspector Signatllr Date 

7.19.6 CONTINUE to 7.20 Filter Train C - Airflow Distributfion (Full System)' 

7.ZOFilter Train C - Airflow Distribution (Full System) 

MAT= IXEERENCE - line 42 

BACKGROUND -this section provides the field acceptance test requirements for installed 

pre-filter and HEPA filter banks. Acceptance test shall be conducted with clean pre-filter 

and HEPA filter banks istalled. (ASME AG-i TA-4632 Airflow Distribution Test) With 

the system operating at design flow rate (18)000 cfm; 19,500 max), the airflow distribution 

shall be measured downstream of each pre-filter and HEPA filter bank. 


* Filter Train 

67 Premier Technology, Inc- 

006765.0.OO-FAT-001-1 (Rev 7)


PREMIER TECHNiOLOGY, INC. -Project No. 006765.0.000 

(PR E I ERT WRPS -242-A Evaporator Ki Exhaust Contract 406 

Ventilation System No. 407 

FACTORY ACCEPTANCE TEST PLAN Spec No. PSEC36 

0 Inlet 

* outlet 

0 Common switching plenum 

a Isolation valves 


a Flexible metal connector 

* Ductwork 

ACCEPTANCE CflITRIA - Velocity measurements across the IHEPA filter banks shall 

be limited to +20%4 of the average. 


7. 20.1 OPEN KI-HV-003 and KI-HV-024 

7.20.2 CLOSE KI-HV-001 and K1-HV-0l0 

7.20.3 RUJN NTCONprocedure 12-101 rev 7 (Attachment 7.18) 

7.20.4 CONFtM the acceptance criterijon has been raot for each damper. 

7.20.5 Test Director VERIFY test iscope. 

LW 4 1 M 

* Test Director Signature Date 



7.20.7 CONTINTUE to 7.21 Stack sampling location - Angular or Cyclonic flow 

7.21 Stack Sampling location - Angular or Cyclonic flow 

*MATRIX REFERENCE - line 56 

BACKGROUND -IThis test is to show the angular or cyclonic flow at the stack sampling 

location. An appropriate method for determining if a proposed location meets this criterion 

is described in 40 CFR 60, Appendix A, Method 1, Section 2.4. 


PREMER TECHNOLOGY, INC. ProicctNo. 006765.0.00 

WRPS - 142- Evaporator KI Exhaust Contract 40167 

EM.E Ventilation SystemNo 

& nc.RPP.SPEC-36062 

1Jre~bnOlgY, 

P .hooy 

FACTORY ACCEPTANCE TEST PLAN Spot No. Re 0 


2.4 Verification of Absence of Cyclonic Flow. in most stationary sources, the direction of 

stack gas flow is essentially parallel to the stack walls. However, cyclonic flow may exist (1) 

after such devices as cyclones and inertial demisters following venture scrubbers, or (2) in 

stack having tangential inlets or other duct configurations which tend to induce swirling; III 

these instances, the presence or absence Of cyclonic flow at the sampling location must be 

determined. The following techniques are acceptable for this determination. Level and zero 

the manometer. Connect a Type S pitot tube to the manometer. Position the Type S pitot 

tube at each traverse point, in succession, so that the plane of the face openings of the pitot 

tube are perpendicular to the stack cross-sectional plane; when the Type S pitot tube is in 

this Position, it is at "0 dog. reference." Note the differential pressure (DELTAp) reading at 

each traverse point. If a null (zero) pitot reading is obtained at 0 dog. reference at a given 

traverse point, an acceptable flow condition exists at that pdi. If the pitot reading is not 

zero at 0 dog. reference, rotate the pitot tube (up to + 1 -90 dog. yaw angle), until a null 

reading is obtained. Carefully determ~ine and record the value of the rotation angle (alpha) to 

the nearest degree. Aut the null tecilhf been applied at each traverse point calculate 

the average of the absolute values of alpha; assign alpha values of 0 degrees to those points 

for which no rotation was requird and include these in the overall average, if the average 

value of alpha is greatr than 20 degrees, the overall flow condition in the stack is 

unacceptable and alternative methodology, -subject to the approval of the Administrator, 

must be used to performn accurate sample and velocity traverses. 

COM IOMT BEING TESM:~ 

0 Stack Sampling system 

ACCEPTANCE CRITERIA - The average flow angle shall no~t exceed 200 relative to the 

longitudinal axis of the stack. Tracer gas coefficient of variation (COy) shall be less tha or 

equal to 20% across an area that encompasses at least the center-Awo-thirds of the crosssectional 

area of the stack The COV of stack gas velocity shall be with + 200/ across the 

ceter two-thirds of the area of the stack. For the entire cros section, the maximum value of 

tracer gas concentration shall not exceed the mean value by more than 3 0% of the meani 

value at any point on a complete set of velocity traverse points. Aerosol particle 

concentration COV shall not exceed 20% over the center region of the stack that 

encompasses at least two-third of the stack area. 




PREMIER TECHNOLOGY, INC. Project Na. 00l6765.0.00 

C7~'IEL/IJER RPS - 242-A Evaporator KI Exhaust Contract 

\wfTchnoog. Te.Ventilation System No. 40167 


7.21.1 MEASUJRE the pressure at each point using an S Type pitot tube. 

7.21.2 RECORD pressure and yaw angle. 

FAT 7.21 Angular or Cyclonic flow Iiil 

Location Measurement Sade Ua- Test QA 

___ Pressure Yaw Angle satisfied Di~ r inspector 

2___ ________ 

3 ____ __________ 

34 __________________________ 

4 ___ ___ /A? 

Rev0 

U. Initials 

Data Smmarysatisfi sfed Test QA 

___ __ __ __ __ __ ___ _ __ _ __ fircctor Iipco 

7.2 1.3 CONFIRM the acceptance criterion has been met. 

7.21.4 Test Director VEIFY test is complete. 

70 Premier Technology, Inc. 006765.O.000-FAT-O01-1 (Rev 7)



~i~~EvIIER WRPS - 242-A Evaporator 1(1 Exhaust contraet 407 

,reh ioIe Ventilation SystemN. 

RPP-4PEC-36062 


5t!L- piap '5 AK1516?L -OFF I' 


7.21.5 QA Inspector VEREFY test is complete. 


7.21.6 CONTINUE to 7.22 Stack sampling location - Contamination Concentration and. 

Velocity Profiles 

7.22 Stack Sampling Location - Contaminant Concentration and Velocity 

Profiles 

MATRIX REFERENCE -line 57 

BACKGROUND - This test is to show the velocity ai~d concenitration profiles of a 

Concentration of 10 ±1I pm AD tracer aerosol (e.g. helium, sulfur hexafluoride) at the stack 

sampling location. 


Stack Samnpling System 

ACCEPTANCE CIIIIA. - Tracer gas coefficient of variation (COV) shall be less than 

or equal to 20% across an area that encompasses at least the center two-thirds of the crosssectional 

area of the stank. Th e COV of stack gas velocity shall be with + 20% across the 

center two-thirds of the area of the stack. For the entire cross section, the maximum value of 

tracer gas concentration shall not exceed the mean value by more than 30% of the mean 

value at any point on a complete set of Qeocity traverse points. Aerosol particle 

concentration COV shall not exceed 20% over the center region of the stank that 

encompasses at least two-tird of the stack area. 


7.22.1 WNE CT tracer gas after HEPA filters in Filter Train C. 

7.22.2 MEASURE concentration of tracer gas at each location. 





P MI R WRPS - 242-A Evaporator Ii Exhaust Contract 

______________________________________ No. 40167 

yVentilation Syte No.__ ______ 

FACTORY ACCEPTANCE TEST PLAN Spc RPPSEC-36 

7.22.3 RECORD 00oncentration of pratical. 

FAT 7.22 Angular or Cyclonic nlow nts 

Location Meas red 

LocationConcentration Sa 

U-Q 

atsf fid Dr npc 

2 

3d 

4 

5 

7 

10 

11 

12 i 

13 

Resu Data Summary Satisfied sans-e Ini a 

eOAverage 

72 Premier Technologry, Inc. 006765.O.000-FAT-ool-1 (Rev 7) 

ur

PRE1MIE R TECHNOLOGY, INC- Project No. 006765.0.00 

®~W JE TgEch noof E 

RPS - 242-A Evaporator K.1 Exhaufft 

etlation SystemNo 

Contract 40167 


FACTORY ACCEPTANCE TEST PLAN Spec No. 1PRC-306 

7-22.4 VERIFY that tracer gas variation is less than 20% across the area of the stack 



7.22.7 REMOVE temporary power from termninals 13 and 14 on TB-6. 

7.22.8 Test Director VERIFY test is cmlt 

TetDirector Signature 

7.22.9 QA Inspector VE RIFY test is corn3 e 


Date 

-Date 

7.23 Exhaust Stuck Sample Line - Hleat Trace Thermostat for CAM airborne 

Radiation Detector (GS.) 


BACKGROUND - this test is a functional test that is to verify the operability of the sample 

line heat tracing. Continuous Air Monitor (CAM) Vendor literature limits the internal gas 

temperature to 120 0 F. 


0 Stack Heat Trace 

ACCEPTANCE CRITERIA - Verify the thermostat functions to turn the heat trace "ON" 

and "OFF' (change of state determined by detection. of heating or energized circuit) at 

115 0 F. 


7-23.1 ENSURE that the contlroller is-wired as por-instruction manual 

7.23.2 ENSURE power to the heat trace circuit is on. 

7.23.3 CONNECT an ohm /continuity meter to the Heat trace connections. 


006765.0.OOO-PAT-O01-1 (Rev 7)


PREMIER TECHNOLOGY, INC. ProjeetNo. 006765.0.000 

E M ITER WRIS - 242-A Evaporator Ki Exhaust -Contat 40167 

\/i 'chnolog, Inc. Ventilation System No. 

( M1 

FACTORY ACCEPTANCE TEST PLAN spec No. RMPE-306 

7.23.4 SET the thermostat to 11 S 0 F and note that whether that controller relay is open or 

closed via the meter reading (should be closed). 

7.23.5 HEAT (using a heat guns) the RTD at the end of the thermocouple lead (white cable) 

7.23.6 CONFIRM when the temperature reading passes I150'F, note whether or not the 

relay opens as the temperature passes the 1 15'F point. 

7.23.7 ALLOW the RTD to cool past the set point and note that the relay closes. 

7.23.8 RESET the set point to 40 0 F, remove the power And sign off the test. 

Fat 7.23HetTaeIial 

Reat Trace Step 7.23A Step 7.23.6 Step 7.23.7 Tea QA 

Controller (OpenIClosed) (Open/Closed) (Open/Closed) Director Inspector 

HTC-1 

HTC-2Z7 

4 

HTC-3 ______ 

HTC-KI-6-2 

Drain ______ 

UMCK1.5-3 

Drain_______ 

H-TC.Stack 

7.23.9 CONFIR.M the acceptince criterion has been met 

7.23. 10 Test Director VERIFY test is complete. 


.7.23.11 QA Inspector VERIFYk test is complete. 


7.24Continuous Air Monitoring - Verify CAM bypass feature 


BACKGROUND -CAM bypass feature allows functional testing and filter paper change 

out while maintaining continuous exhauster operation. 


PREMIE TECH:NOLOGY, INC. Project No. 006765.0.000 

(~~ M IE WlPS- 4- Evaporator K1 Exhaust Contract 401,67 


EpP.SPE-C-36062 

FACTORY ACCEPTANCE TEST PLAN Spec qNo. Rev 0 

COMPONENTBEING TESTED: 

0 CAM bypass 

ACCEPTANCE CRITERIA -CAM bypass feature allows functional testing and filter 

'paper change out while maintaining continuous exhauster operation. 

TEST PROCEDURE, 

7.24.1 ENSURSk valve line-up is in aocordance with valve table 

Valve/Dmp Desciption IPosition - 

KiI--1 Inlet Plenum to Filter Train A Open 

K1-HV-002 Inlet Plenum to Filter Train B open 

KI-E[V-03 inlet PJeLumto Filter Train C open 

KI-HY-010 Filter A To Switch Plenum Open 

KI-HIV-01.7 Filter B To Switch Plenum Open- 

KI-HV-024 Filter C To Switch Plenum Open 

KIi-MOV-001 Plenum to Fax Isolation Damper (North) 1(Closed) 

KI-MOY-002 Plenum to Fan Isolation Damper (South) (Closed) 

K1-DMPR-0Ol Fan to Stack Isolation Damper (North) Open 

KJ-MPR00 Fa t StckIsoaton Damper (South) Open 

7.24.2 VERJXI cabinet 400 is ON. 

iitiaw 

7.24.3 REMOVE red wire #65 for 1-8 terminal from, AM-i (smart relay). (NOTE: this is to 

simulate a high radiation alann). 

7.24.4 SET Kl-5-3 VFD to 45 Hz, 

7.24.5 START KI-5-3 (NOTE: Kl-5-3 should not be able to start.)A0 

7.24.6 CONFIRM if Kl-5-3 will start YES NO 

7.24.7 TURN CAM bypass switch to the ON position. 

7.24.8 START KI-5-3 (NOTE: KI-5-3 should be able to stalt)/ 

7.24.9 CONFIRM if Kl-5-3 will start YES NO 


006765.O.OO-FAT-0O1-I (Rev 7)



U EM IERTT 'WRPS - 242-A Evaporator K1 Exhaust Contra 416 

,InVentilation System No. 406 

FACTORY ACCEPTANCE TEST PLAN Spec No. RP-PC-66 

7.24. 10 STOP motor and allow it to come to rest. 

7.24.11 RECONNECT red wire #65 to 1-8 terminal. 


.7.24.13 Test Director VERIFY test i o0 e 

~-O/ 


7.24.14 QA Inspector VERIFY test is cr 

~ ~ 4~L .. Ono 


7.25 Vacuum Pump - Verify Pump operation 


BACKGROUND - This test is to verify the pump operation and cabinet environmental 

conditions. 


*Vacuum Pump 

ACCEPTANCE CITERIA - The vacuum pumps shall be capable of drawing a minimum 

of 1.42 US (3 scfhi both pumps running) at system static pressure through the 

sample/monitor loops. The pumps will not surge during operation. 

*TEST PROCEDURE: 

7.25.1 )SURE cabinet 400 is turned on and a vacuum pump is running. 

7.25.2 RECORD FITC-2 and FITC-3 flow readings. 

F1TC-2 Flow Reading FITC-3 Flow Reading_ 

Sum of FITC-2 and FITC-3 flows~ 1401J 

7.25.3 CLOSE HV-3 and HV-4 (NOTE: relief valves should lift) 


PR1.EMIER TECHNOLOGY, INC. Project No. 006765.0.000 

P E M ~IJER WUPS -242-A Evaporator Ki EhAlist Contract 406 

\ w'nog, ~t etltion S stem No. 406 

fbhnloyIn. FACTORY ACCEPTANCE TEST PLAN Spec No. 

7.25.4 RECORD max vacuum level on PrTC-4 (should be over 12 imug) 

P]TC-4 Max Vacuum Readings :5 V 0 (14a -,Ol 

7.25.5 OPEN HV-3 and HV-4 

7.25.6 CONFIRM thq acceptance criteria. have been met. 

7.25.7 Test DirectoZ kP test is comnplet. 

'Tst Director Signature 

7.25.8 QA Inspector VERIFy to s ee 


Date 

Date 

7.26 CAM Operation -Verify No Electromagnetic Radiation Interference 



BACKGROUND - CAM unit is to be checked with exhauster components per RPP-SPEC- 

36062, Rev. 0, Section 3 2.4.2 


*AMS-4-1 

ACCEPTANCE CRITERIA - No inadvertent alarms, interlocks, or sporadic indications in 

the CAM operation due to interference from outside electronic devices 


7.26.1 ENSURE valve line-up is in accordance with valve table ' 

-Valve/Damper- Description Position 1til 

I KkHV4O01 Inlet Plenumj to Filter.Traln A Open 

KI-HV-002 Inlet Plenum to Filter Train B Open 

KI-HV-003 Inlet Plenun to Filter Traini C Open 


K1.V-1C Filter A To Switch Plenum Open 



PREMIIER TECH[NOLOGYp [NC. Project No. 906765.0.ooo 

&P AHER 

'llechno13gy i1C. 

WRPS -242-A Evatporaitor Ki Exhaust 

Vetlon Sste 

Contract 

No. 40167 

FACTORY ACCEPTANCE TEST PLAN Spec No. R?-PC-66 

KI-HV-DI7 Filter 1B To Switch Plenum Open 

K.1-HV-024 Filter C To Switch Plenum Openl 

KI-MO V-001 Plenum to Fan Isolation Damper (North) (Closed) V 

K.1-MOV-OOZ Plenum to Fan Isolation Damper (South) (Closed) 41 

rKI-DMPR-O0l Fan to Stack Isolation Damper (North) Open 

K-i-DAM-oo Fan to Stack Isolation Damper (South) Open 

7.26.2 VERIY cabinet 400 is on. 

7.26.3 SET K1-5-3 VFD to45 Hz. 

7.26.4 START Kl-5-3 

7.26.5 KEY a hand held radio around cabinet 400. 

7.26.6 CONFIRM no invert alaums, interlocks Or sporadic indications are observed at the 

CAM 

7.26.7 CONFIRM if KI-5-3 does not shut down. YES NO 


7.26.9 Test Director VERIFY test i o ' 


7.26.10 QA Inspector VERIFY testi a et 

(erw~f~ 2 

)P 




BACKGROUNhD - this test is to simulate a temperature conditions to show the proper 

function of the sample cabinet cooling fan per RPP-SPEC-36062, Rev. 0, Section 4.1.20 


78 Premier Technology, Inc. 006765.0.000-FAT-ool-1 (Rev 7) 

Rev

*F-400 

ACCEPTANCE CRITERIA -Fan 


7.27.1 vERIFY cabinet 400, is on, 


PREMWER TECHNOLOGY, INC. Project No. 006165.0.000 

WRPS - 242,A Evskporator Ki Exhaust Coutract 40167 

Ventilation SystmN 

iPSC-6l 

FACTORY ACCEPTANCE TEST PLAN SPCN. Rev 0 

will turn on at 110* F 

7.27.2. EAT cabinet thermostat area with a heat gun. 

7.27.3 VERIF cabinet fanwill turnl1ofatl11 0 F 

7.27.4 Temperature when fan turned On ~ V 

7.27.5. CONFIRM the accptance Criterion has been met. 

7.27.6 Test Director VERIFY test isci-WD~ 


7.27.7 QA Inspector VERIFY i tsomlt Q 

QA Inspector- Signature 

Date 

Date 

7.281nlet Plenum & Expansion Joint& -,ifessi re De cay Test & Bubble Leak 

Test 

MATRIX REFERkNCE - Line 23 

)BACKGROUND - A pressure boundary leak test shall be conducted to verify leaktightness 

of the damper housing and interfame with system in accordance with ASME AG-i 

Secton TA-3 523 and Mandatory Appendix TA-I]L (TA-3 523-TA-Ill-i 100) SIJMMAWR 

OF METHOD Ducts and housings that form the pressure boundary of the system shall -be 

leak tested; with air, using one of the methods listed in this proceure. Either method may be 

used and will produce a similar test result. The constant pressure method is useful for testing 

small volumes and is conducted at the maximum operating pressure for the system. Thle 

pressure decay method is useful in testing large volumes and is conducted by pressuizing to 

114 times the maximum operating pressure, then allowing the pressure to decay for a fixed 

period of time, or until the pressure decreases to 80% of the maximum operating pressure, 

79 Premier Technology, Inc. 006765.0.OOO-FAT..OO1- (Rev 7)



(i~F1\4IER 

.cn-g,11C 

WRPS -242-A Evaporator Ki Exhaust 

Ventilation SystemN. 

Contract 06 

FACTORY ACCEPTANCE TEST PLAN~ Spec No. RP-P30 Re 2 

whichever occurs first. Fans, dampers, and other components that are pat of the pressure 

boundary shall be installed and tested with the pressure boundary to verify interface 

connection leak tightness. If the measured leak rate is in excess of the acceptance criteria, 


repaired, the duct and bousing shall be retested to verify leak-tightness. 


0 All gasket joints on the inlet plenum and expansion joint on the inlet of the filter 

trains 

ACCEPTANCE CRMIRIA: 

9 No bubble indications 

a The leak rate shall not exceed 0.23 ft 3 per hour at a pressure of -23 .7 inH 2O (see 

Attachment 6.23). 

TEST PROCEI)URE: 

7.28.1 INSTALL blanking plate on Ember Screen. 



KI-HV-001 Inlet Plenum to Filter Train A Closed j7jjj 

Il-HV-002. Inlet Plenum to Filter Train B Closed o 

KI-HV-003 

I-HV-010 

Inlet Plenum to Filter Train C 

Filter A To Switch Plenum 

Closed 

open 

k 

j. 

K21-HV-017 

KI-HV-024 

KI-MOV-001 

KI-MOV-00.2 

Filter B To Switch Plenum 

Filter C To Switch Plenum 

Plenum to Fan Isolation Damper (North) 

Plenum to Fan Isolation Damper (South) 

Open 

Open 

(Open) 

(Open) 

l 

CI( 

(/ 

3 

7.28.3 INSTALL pressure relief device set at-25 inH 2.O 

7.28.4 PROVIDE a vacuumi pressure of I 4 times Max Operating Pressure (-23.7 in}{ 20) 

7.28.5 CONDUCT bubble leak test in accordance with pT-TP-1 .7 Rev 5 Bubble Leak Test 

Procedure. 5a~ f cxc ep xitn 010. , / 

80) Premier Technology, Inc. 006765.0-O0O-FAT-001-1 (Rev 7)

PREMIE TECHNOLOGY, INC- Project No. 006765.0.000 


WRP -242A vapraorK1 Elbaust Cootract 40167 

(P~nlg~ Ic Ventilation stem No. RPSE-66 

FACTORY ACCEPTANCE TEST PLAN Spec No.' Rev 0 

7.28.6 vERIFy there are no babble indications on gasketjoints. 

7.28.7 CONDUCT rate of decay test i n =cOrd&n= with pTT-l.1 5.6765 Pressure Decay 

Test (see Attachment 7.4). 



Test Director Signatur 

7.28,.10 QA Inspector VERMF test is complete. 


-7.29Exhaust Stack Sample Pitot Tube a nd Transport Lines - Leak test & Pitot 


MATRIX RIEZENCE - line 46 

Date 

Date 


installation in accrdance with ANTSI NI3.1,. Section 6.9. PIC 3 stack allows for inspection 

as satisfactory method. Isolate and pressurize sample line to .75 psi. 

COMIPONE NT BEING TESTED: 

* Exhaust Stack sample pitot tube and transport lines 

ACCEPTANCE CBJ.TEIA -No leaks detected using bubble testing on joints and weld 

seams. 


7.29.1 CAP open ends of sample lines. 

.7.29.2 INSTALL pressure relief device set at 25 inE2O. 

7.29.3 PRESSURIZE system with compressed air to 23.7 inH2O 


006765.O.OOO-FAT-001-1 (Rev 7)



IJER 

.Tchno ) ER 

WPS - Z42-A Evaporator Ki Exhaust 


Cotac 

No. 40167 

(~E1 

FACTORY ACCEPTANCE TEST PLAN Spec No. RPPSP-30 6 

7.29.4 CONDUCT bubble leak test in accordance with PnhTP-1 .7 Rev 5 Bubble Leak Test 

Procedure (see Attachment 7.4). 


7.29.6 Test Director VERIFY test is c ee 

Test Director Sigpatre Date 

7.29.7 QA Inspector VERIFY test is compete. I ~ 

C ~ ~-rf -OP ' 


7.30 Sampler line Vacuium Indicator - Functional Test (P1) 

MIATRIX REFERENCE - Hune 51 

BACKGROUND -this test is to verify vacuum indicator reads on scale for the normnal 

sample flow rate range of 0 to 2 SCFM per RPP-SPEC-3 6062, Section 4.1.16. 


0PI-I 

ACCEPTANCE CRITERIA - The vacuium indicator will indicate over the calibrated span 

of instrument, 0 to 20 in HG vacuum. 


7.30.1 REMOVE PI1 from cabinet 400. 

7.30.2 CONNECT calibrator. 

7.3 0.3 RECORD equipment and calibration information. 

Equipment Model # Serial #Dae 

7.30.4 SET calibrator toO ming. Sc &. i' ) 



PRE1M TECHNOLOGY, INC. Project No. 006165.0.000 

( 7 ~TZ AIE . wR2PS - 242-A Evaporator K(1 Exbaust Contract 40161 

\~~tg h~C.ventilation S stemn 

FACTORY ACCEPTANCE TEST PLAN Spec No. Re 

7.30.5 RELEASE anY residual pressure inl P1 by liftig relief plug on top of gauge. 

7.30.6 RBCORD P1 readout in table. 

7.3 0.7 jNCREASE calibrator setting. 


7.30.8 REPEAT steps 6.15.6 - 6.15.7 until a total of six reading are taken from 0-19 inHg. 

FAT 7.30 Sampler Line Vacuum Indicato r - Calibration Initials 

2 

3 

4 

6 

Caebrto "Oudg P1: Readoti (Ih111) % Uri-o Director necr 

See- ecv, 

7.30.9 REMOVE calibra tor. 

7.3 0.10 COMFIIOM relief plug is returned to 'Plugged" position. 

7.3 0.11 REINSTALL P1 into cabinet 400, 


7.3 0.13 Test Director YERJFY test is complete. 

'St , 'v.£ Cq21 


7.30.14 QA Inspector VERFYF test is complete. 

Sce X. v. 6C 'I.Ii 



Date 

Date 



PREMIOER TECHNOLOGY, INC. Froject No. 006765.0.000 

(~b 'N UT~D WRPS - 242-A Evaporator Ki Exh~aust Confract 40167 

CVentilation System No. 

FACTORY ACCEPTANCE TEST PLAN Spec No. RPSev 0 06 

8. Completion of FAT Test 

8.1 Final Sign-off 

8.1.1 CONFIRM all testing is complete for sections 6 and 7 

8.1.2 Test Director VERI(FY test is complete. 



QA Inspector Signature 'Date 

9. Attachment List A 

Aw1A)A6Vr A. *F St4MQ~wu.-. V~-- 010- & w~ 

0riMC**-ar'B, Ffrr?. 6ti-pi h~upimfvvu 'A- N%. 

Attachment 1, FAT Test Exception Record 


Attachment 3, FAT Test Log 

Attachment 6.1 Electric Drive Motor Vendor Data 

Attachment 6.2 Valve/Damper Vendor Data 

Attachment 6.3 Damper Manufacturer Certification Documents 

Attachment 6.4 Damper Frame Leakage Documents 

Attachment 6.5 Filter Train Pressure Boundary Certification Documents 

4 F(, %&w)C AGM& Ltw 7V~ueLf- Pn*4-er- -. h n' t OE~ 

Attchment 6. 10 AMC Factory Acceptance Test Procedure of 242-A Exhauster Sampling '? 

Ssem 

Attachment 6. 18 AMC Ship Traveler 

Attachment 6.21 Flanders Sample Manifold Certification 

Attachment 6.22 Twin City Fan test reports 

84 Premier Technology, Inc. 006765.O.0OO-FAT-OO1-1 (Rev 7) 4Ji

PREMIER TEC1HNOLOGY, INC- Project No. 006765.0.000 

WRPS -R 

w~s- 22-kEvaortorK1 xhast Contract 40167 

No. 


FACTORY ACCEPTANqCE TEST PLA spe No. Rev-30 6 

Attchment 6.23 Volume calculations A1 OA Ol rrp~- 

Afc*f 7. xas Fa W)1-- anV Eas Traini Flow Teat (Minimum system Loss) 

/~ Attachment 7.11 Exhaust Fan KI -5-3 and Exhaust Train Flow Test (Maximum System 

-Attachment 7.13 Exhaust Fan 1(1-5-3 and pjTrain Flow Test (Minimum System Lass) 

p~XMA~ -T. 16 *UW&W &Mt 1CW- m 

K'T,' 4a* ,=~n Flow Test (Maximum System 

Lass) 

~Attachment 7.18 NUCON procedures 12-101 rev 7 

ew'* r' 1 -46~ e e q ~-~ r 

85 Premier Technology, Inic. 

006765.O.OOO-FA'iI>O1i1 (Rev 7)

Attachment A 


Page A-i

PREIER TE CHNOLOGY, FqC. Project No. 006765.0.000 

(mkNIE D WRI'S - 242-A Evaporator KExhaust 

~~T-hnkk3 l'cVentilation 

System 

ContaMCt 

No. 

40167 


Spc o- 

SpcN- Rev 0 

COPONEN BING TESTED: 

0 KI-MOV-001 

0 KI-MOV-002 

* KI-BDD-001 

& KI-BDD-002 

* KI-DMPR-001 

* KI-DMPR-002 


Page A-2 

RP-SPEC-360 62 

ACCEPTAC C jrRA -Visual inspections are acceptable when there are no 

indiatins o imrope intallatiolt, physical damage , structual distress or degadation that 

would impair the ability Of the component or system to perform its intended function. 

TEST PROCEDURTE: 

-7.1.1 VERIFY all inspection items listed in ASME AG..ITA-1-120 0 

7.1.2 CONqFIRM the acceptance criteria have been met for each damper. 

FAT 7.1 ASME AG-i, TA-3510 Initials 

improperly Installed Psieft Damag.e structural Distress Test QA 

Damper List Ye o Ys N o Director Inspector 

KI-MOV-001 

Kl-MOV-002. 

KI-BDD-001 

KI-BDD-002 

KI-DMPR-001 

KI-DMPR-002 

7.13 Test Director VERIFY test is complete. 


7.1.4 QA Inspector VEPIFY test is complete. 


Dt 

O6765.0.000FrAT-001-1 (Rev 6)


Page A-3 

PREMIER TE CHNOLOGY, INC. Project No. 006765.0.000 

VentilationSystem 401___ 7______ 

FACTORY ACCE PTANCE TEST PLAN Spec No. RPP-SPEC-36062 


______Rev 0 

7.2 Valve/Dampers - Verify 190latiOlt ValVC Position Indication and Function 

MATIX REFE4RENCE - line 25 

BACKGROUND - Prior to the initial pressurizing of the damper control system, pnieumatic 

systems shall be checked for proper installation and leak-tightnless. Dampers having remote 

position indicators shall be. observed during operation to 'verify that the mechanical damper 

position corresponds to the remote indication. Power-operated dampers shall be fully cycled 

using a control switch or other actuating device to verify operation. 

COMPONENT BEING TE STED: lt&Sot 

SKI-MOV-.00l fhJk r,2 ~ AtwIi-Ihi lc 

*KI-MOV-002 i o4~4 e;t' 3/o/zo?- 

ACCEPTANCE CRITERI (K1?os C //' 

*ASME AG- I TA-4244 Verify that the dampers indicator corresponds to the remote 

indication. 

*ASME AG-I TA-4245 Damper must fully cycle 

*ASMEff AG-i TA-4246 Maximum time for any of the cycles shall be less than 20 

seconds. 


7.2.1 CONFIRM indicator mark position matches actual damper position. 

7.2.2 RECORD the position of the shaft where it enters the duct in the table below (the 

mark should be perpendicular to the duct when the damper is closed). 

7.2.3 E NSURE power to the controller/positioner is on (Note MTPZ Breaker in the table 

below). 


high radiation interlock to the fanls). 

S7.2.5 CHECK for Initial Voltage onl the "Damper Closed" term-inal to ground - should be 

0 VAC (See location in table below). 

& S-c .Tr-- 10F CNOTQ Co e (jF 4' q 11bi 

31 Premier Technology, Inc. 006765.0.000-FAT-oo1-1 (Rev 6)

IERITTT 


Page A-4 


WRPS - 242-A Evaporator KI Exhaust Contract 406 

-,y .Ventilation System No. 406 

FACTORY ACCEPTANCE TEST PLAN Spec No. RPPEv -300 

.,7.2.6 CHECK for Initial Voltage on the "Damper Open" terminal to ground - should be 

120 VAC (See location in table below). 

7.2.7 REMOVE the "Run Permissive (RPR) Relay" wire to prevent the fan from starting 

and protect it from shorting with a wire nut or other appropriate means (Get location 

from table). 

7.2.8 SELECT Run on the VFD and verifys that the damper moves to the full open position 

(Mark should be parallel with the duct) 

)7.2.9 RECORD the Final Voltages of the "Damper Open" and "Damper Closed" 

terminals (These should be 120 VAC and 0 VAC respectively). 

7.2.10 RECORD the Final Observed position of the damper. 

7.2.11 RETURN the VFD Run switch to the Stop Position and note that the damper closes. 

7.2.12 RE-CONNECT the RPR relay wire. 

7.2.13 INITIAL for completion. 

7.2.14 REPEAT steps 7.2.2-7.2-12 for the other fan. 

7.2 Isolation Damper Position Initials 

ENCL. 

0 

In~itial 300 'rp Clousd T-rnis.I 0 nsper Opess T-inat., Finalr TetQ 

List D-npu r P RPR Posto B Tiector A 

Positions Brkr N RoDiecty Inspector 

T-n Initial Final Initial Final nslpation 

Voltago Volrogp Voltog. Voltog, 

001 #10 k__T 

KI- 

Mov- 2 TB.5 # 

002 CL0Z 22 


7.2.16 MEASURE the time for the damper to fully open or fully close. 

7.2.17 REMOVE temporary power from terminals 13 and 14 on TB-6.. 


FAT 7.2 AM AG-1, TA-4244, TA-4245 &TA-44 Initials 





P E I RVentilation System No. 

FACTORY ACCEPTANCE TEST PLAN Spec No. ,PSP. 366 

Remote indication 

matches damper Damper Fully cycles Test QA 

Damper List Cycle Time YesItlI o N Director Inspector 

Kl-MOV-002 12,2 o K Ys Ie N 

K--01 SW Xse 

7.2.19 Test Director VE RIFY test is complete. 




Date 

Date 

7.3 Filter Train - Visual Inspection 'C e v, ' .# S'ioyi o 


BACKGROUND - (ASME AG- I TA-3 5 10) a visual inspection is to be conducted to verify 

all components are installed in accordance with the Owner's design specification. This 


Visual inspection is to be performed on the filter train, inlet, outlet, common switching 


accordance with AG- I 


* Filter Train A 







7.3.1 VERIFY all inspection items listed, check box for if item is free of physical damage, 

structural distress or degradation that would impair the ability of the component or 



006765.O.OOO-FAT-OO1-1 (Rev 6)


Page A-6 

PREMiER TECHNOLOGY, INC. Project No. 006765.0.000 

VW S - 242-A Evaporator 1(1 Exhaust contract 40167 

ii -Ventilation System No. 

FACTORY ACCEPTANCE TEST PLAN Spec No. ReP-PE-30 6 

F AT 7.3 1ASM AG-i, TA-3510 

Inspection items: Ftra Filter Filter 

TrainA Trin B Train C 

Housing and duct connections (no caulking) _________ _____ 

'Access door seals' and gaskets 

Sample and injection pores location and caps 

Supports and attachnments 

Bolting and fasteners 

Instrusmentation, connections 

Electrical connections 

H1ousing/duct penetration seals 

lighting conduits and socket husing seals (flush 

mRounted) 

HEPA frame continuous seal welds 

Mounting frame penetrations seal welded 

Mounting frame seating surface (weld splatter, 

flatness, and scratches) 

mounting frame clamping devices 

As-built configuratiais in accordance with design 

drawings 

provisions for access for performing teats and 

maintenance 

Prefilter mediat, frame, clamps, and gaskets 

HEPA filter media, frame, clamps, and gaskets ____ 

Sealant or caulking (inone allowed) 

Blolting and fasteners 

IJEPA filter nameplate_____ __________ 

Plenum isolation valves_____ 

Flex Connector s 

Test Director 

QA Inspector 

7.3.2 CONFIRM the acceptance criteria has been met for each Filter Train. 

7-3.3 Test Director VERIFY test is complete. 


7.3.4 QA Inspector V-ERJFY test is complete. 


34 Premier Technology, Inc. 006765.O.OO-FAT-0OI-1 (Rev 6)

PREMIER TE CHNOLOGY, INC. Project No. 006765.0.000 


Page A-7 

WRS - 242-A Evaporator KI Exhaust Contract 40167 

C~cdmolgy~in ~Ventilation SystemN. 

& _T'':hnlogynC.RPP-SPE C-36062 


7.4 242-4 Evapo rator KKI ExEhaust - Pressure Decay Test & Bubble Leak Test 

-c . 

rAt 5 " '3)%~ 1 A 

MATRIX REFERENCE - Line 23 r 

hOCA 

BACKGROUND - A pressure boundary leak test shall be conducted to verify leaktightness 

of the damper housing and interfaces with system in accordance with ASME AG-i 

Section TA-3 523 and Mandatory Appendix TA-EL1. (TA-3 523-TA-ill-i 100) SUMMARY 

OF MvIETHIOD Ducts and housings that form the pressure boundary of the system shall be 



small volumes and is conducted at the maximum operating pressure for the system. The 

* pressure decay method is useful in testing large volumes and is conducted by pressurizing to 

1 V 4 times the maximxum operating pressure, then allowing the pressure to decay for a fixed 


whichever occurs first. Fans, dampers, and other components that are part of the pressure 

* boundary shall be installed and tested with the pressure boundary to verify interface 

connection leak tightness. If the measured leak rate is in excess of the -acceptance criteria, 

the leaks shall be located by one of the methods listed in this procedure. After leaks are( 

repaired, the duct and housing shall be retested to verify leak-tightness. 

COMPONENTS BEING TESTED-. 

*All gasket joints on the system 

* ACCEPTANCE CRITERIA: 

No bubble indications 

*P The leak rate shall not exceed 0.1% of the system volume per hour at the system 

leak test pressure as defined in ASME AG-I for'leakage Class!I (Table SA-B-13 10) 


7.4.1 INSTALL blanking plate between each Fan Assembly and Fan to Switching Plenum 

Expansion Joint. (location 1 & 4) See Figure 7.4 Test Locations 



KI-HV-001 Inlet Plenum to Filter Train A Closed Ch 

KI -HV-002 Inlet Plenum to Filter TrainsCoe / 




Page A-B 

PREAMER TECHNOLOGY, INC. Project No. 006765.0.000 

(PRE IER WRPS - 242-A Evaporator KI Exhaust Contract 406 

Tehooy n.Ventilation System No. 407 

FACTORY ACCEPTANCE TEST PLAN Spec No. RPFSev0 0 

KI-HrV-003 Inlet Plenum to Filter Train C Closed 

K1-HV-010 Filter A To Switch Plenum Open 119Y 

KI-HV-017 Filter B To Switch Plenum Open 6k 

KCI-HV-024 Filter C To Switch Plenum Open 

Kl-MOV-001 Plenum to Fan Isolation Damper (North) (Open) CI 

KI-MOV-002 Plenum to Fan Isolation Damper (South) (Open) 

743 TAIJ pressure relief device et at 25 inH 20 

7.4.4 PRESSU(RIZE system with compressed air to 1 14 times Max Operating Pressure 

(23.7 inH 2O) 

7.4.5 CONDUCT -bubble leak test in accordance with PTI-TP-1 .7 Rev 5 Bubble Leak Test 

Procedure (see Attachment 7.4). 

W2312W 

EEll 

11 .13 

6W16 

36 PrmierTecholog, 

In. OO76S..OO~F22]O- (ev6


Page A-9 

PREMIER TE CENOLOGY, INC. Project No. 006765.0,0007 

J,~ T NA E WRPS -242-A Evaporator XCI Exhaitst Contract 40167 

\w Tehnoy 01nlc. -. Ventilation SyternNm 

FACTORY ACCEPTANCE TEST PLAN Spec NO. I PeCvo O 


7.4.6 VERIFY no bubble indications are detected at locations shown if figure 7.4 Test 

Locations. 

FAT 7.4 ASME AG-1, TA-4233 & TA-4234 Iitials 

Description Un- Test QA 

LoTationFroTO Satisfie Director In spector 

4 TEST PLATE *KI-ET-05 ___ 

S IETION 2 SECTON 3 - 

1'PLENUM 

3 KI-MO-001 SECION 401 

4 TE-SV-LAT FILER TRIN 

21 ILER0 TRICI-OV-002 

26 

ILTER00 T PLNB ENUM02 

77 CNPIP the aetnecItrahvbenmtyiiilngal. 

IO 

79 CONRT-.56 dat tableO iscmpee 

37 PreEier TehKlgy-nc 

___ 

066.-00A1014(ev6


Page A-10 

PREMIER TECHNOLOGY, EINC. Project No. 006765.0.000 

CIchio' vm - RPS -242-A Evaporator Kl Exhaust Con~act 406 


RPP-SPEC-3600- 


7.4.10 REMOVE blankinga plates in all three locations. 

7,4.11 Test Director VERIFY test is complete. 

* Test Director Signature Date 

7.4.12 QA Inspector VERIFY test-is complete. 

k' 

IqlI 


7.5 Power Instrti-ment and Coutrol Cabling - Proper voltage and phase 

sequence at equipment served S, 


f e- k ' vS~i~ 

BACKGROUND - Perform inspection during cable energizng 


*Power Instrumrent and Control Cabling 

ACCEPTANCE CRITERIA- Specified voltage (see table FAT 7.5) at equipment served 


TEST PROCEDURE:. 


Equiment Mode -#Seril #Calibration Due 

Equimen Modl #Seril ~Date: 

38Premier TcnlgInc. 006765.0.000-FAT-001-1 (Rev 6)


Page A-1l1 

PRE AMER TEC~iNOLOGY, INC. Project No. 006165.0.000 

'~' WRPS - 242-A Evaporator 1(1 Exhaust Contract 40167 

Inc.Ventilation System No. 

3T P S. No. R-PP-SPEC-36062) 



7.5.3 AMASUIRE voltage oh the Bus-side of the panel using a calibrated Volt Meter. 


NOTE: if the circuit is a GECI press the test burtton and record proper function. 

7.5.4 -VERIFY breaker is on. 

7.5.5 MEASUJRE voltage at -the receptacle/equipment. 

7.5.6 MNIAJ- each circuit as it is completed. 

FAT 7.5 Circuit Breaker/Voltage and Phase Sequence Verification Jiil 

panel # Circuit Eupet GFC1 GFC1 T)EST Se d Mese Test Q 

# qimn good/bad voltage Voltage Director Inspco 

KI-MPZ-001 I KI-MOV-001 NO 110 VAC 

KJ-MPZ-001 3 KI-MOV-002 NO 110NA 

KI-MPZ-001 5.7 K1 -ENCL-400 N 2 A 

K1-MP7-001 6 KI-RCPT-001 YES 110 VC____ 

KSl-MPZ-001 8 K1-RCPT-002 YFS 110 VAC _____ 

KI-MZ01 9 KI-RCPT-003 YES 110 VAC 

KI-MPZ-00I 10 SPARE NO 110 VAC 

KI.MP'L-001 11 HEATTRACE YES 110 VAC 

K.1-MPZ-001 12 SPARE No - 110 VACI 

7.5.7 CONFIRM the acceptance criteria have been met 


TPest Director Signature 

7.5.9 QA Inspector VE RIFY test is complete. 



Date 

Date 

006765..OOO-FAT-OO1-1 (Rev 6)

FPREAMER TECHNOLOGY, 

RiC. [Project 


Page A-12 

No. 006765.0.00 

(~>~iE~1II~IR. WRPS - 242-A Evapolrator Ki Exhaust Contract 406 

)&Y ici , Ventilation System No. 

FACTORY ACCEPTANCE TEST PLAN Sp, ]o RPPeC-306 

KI-K-005 22 

Resistance Check OHMS OHMS Initials 

Resistance between terminals 7 and 8 

Name Plate Data VD@1 ~ 1% 

IN Volts A-Phase Inrush Dampers @ 10%' Test QA 

FLA Volts Hz Ph-A Ph-B Ph- fetr npco 

amos amps amps ______ 

_________________ VFD @ 60HIz (100%) __________ 

Dampers @10% Dampers @ 50% Dampers @ 100% Initials 

Ph-A Ph-B Ph-C Ph-A Ph-B Ph-C Ph-A PiB-B Ph-C 

.1p s amps aps Tp am s at-jAmos 

____Initial VFD Settings Final VFD Settinos____ 

tCC I___ FLO I____ teC I___ FLO f____ 

CFG _____ A02 CFG jA02 

bFr _____ Al2t _____ Fr . Al2t 

ACC ____ACC 

dEC ______App Pdbk dEC i App Fdbk ____ 

LSP ___ I App Ref LSP App Ref 

fr- I _-Min Fdhk SFr jMin Fdbk ____ 

tCtc ____ Max Fdbk tCt _____..Max Fdbk_____ 

CrL2 Min Ref' CrL2 Min!l Ref'_____ 

r2 Max__ MRef r2 Max Ref 

FRI _____ IntRef FRI I atC Ref 

C1ICF -___ PG CHCF ____I PG 

aST ______ DC ST _____ IG 

rCb, ____ G eCb Di G 

Frib ___ _ R-Amp FrIb _____jRamp 

RSf _____ Min-Out RSf Min Out 

FLR -_____ flX Out FLR LMax Out 

OL _____ Rev OPL L Rev 


7.7.26 VERIFY Kl-MO-001 is closed. 

7.7.27- VERIFY KI-BDD-001 is closed. 

7.7-28 REMOVET temnporary power from terminals 13 anid 14 on TB-6. 

7.7.29 RECORD all final VFD settings. 


7.7.31 Test Director VERIFY test is Complete. 

44 Premier TechnologyIc 006765.0.9O-FAT-OO1-1 (Rev 6)

PIRE MIER TECHNOLOGY, INC. Project No. 006765.0.000 

E\/lIRWPS - 242-A Evaporator Ki Exhaust 

\~w9~Thchology, ~Ventilation SstemNo 

TEST PLAN 

coulract 

SpecINo. 

406 

407 

(f~L 

FACTORY ACCEPTANCE TETIRev 

/0 

Test Director Signiature 

7.7.32 QA Inspector VEIMJY test is complete. 


Date 

Date 

7.8 KI-5-2 Fan and Motor - Vibration Test (Minimum System Loss) 

MATRIX REFERENCE - line 8, 47. & 48 


Page A-1 3 


the normal operating speed for a ruin in period of time until the bearings reach a stable 


minutes) .This test is to determine the vibration of the fan and motor under minimum system 


prior to the Fan Performance/Airflow Capacity test. ASME AG-I TA-3533 - Vibration 



When the bearing housing is not accessible the frame of the. component may be used if it 



0 KI-5-2 Fan and Motor 

ACCE PTANCE CRITE RIA: 

* Vib ration: Measured in all three planes. The criteria for low horsepower, industrial 


8.8 mm/s EMS velocity (filter out) 


7.8.1 RE CORD equipment and calibration information. 

Equimen Modl #Seril #Calibration Due 

Equimen Modl #Seril #Date: 

/'Iop) e J(C VprSteteS 75' enx-3 Ll 1 


006765.O.000-FAT-001-1 (Rev 6) 

0

PREMIER TECIINOLOGY, INC. Project No. 006765.0.000 

R MTRPS - 242-A Evaporator Ki Exhaust Contract 406 

hn~iog~, ~Ventilation System No. 496 


Page A-14 

RPP-SPEC-3606Z? 


Vib Aa~ 00 '2 S 51 CI 

7.8.2 INSTALL new clean filters in filter housings A, B, and C. 



KI-I{V-01 Inlet Plenum to Filter Train A Closed OW~ 

K] -HV-002 Inlet Plenum to Filter Train B Closed L 

KI-HV-003 Inlet Plenum to Filter Train C Closed 

KI-HV-010 Filter A To Switch Plenum Closed L 

K1-E[V-017 Filter B To Switch Plenum Open LTI 

KI-HV-024 Fitter C To Switch Plenum 

I~lMOVO0 PlnumtoFanIsoaton ampr Norh) 

Open 

Clsed 

~ j 

0Ie 

KI-MOV-001 Plenum to Fan isolation Damper (South) (Closed) L4 

IU-MOV-02 Faenu to tak Isolation Damper (oth) (Cosed) LA 

KI-DMPR-001 Fan to Stack Isolation Damper (South) Open Ok' 

7.8.4 VERIFY power to the VFD is on. 

7.8.5 CONSULT and EMLEMME T any additional safety precautions as required by 


7.8.6 SET the VED speed to 10 Hz (17%) 



7.8.8 OPEN K1-HV-002 and KI-HV-003 to 75 % 

7.8.9 START Kil -5-2 fan and allow is to run for one hour. 

7.8.10 INCREASE VFD Hz setting until 13,500 scfrn is measured. 


006765.O.OO0-FAT-O9I-1 (Rev 6)


Page A- 15 

b PREMIER TECffNOLOGY, INC. Project No. 006765.0.000 

EM ER WRPS - 242-A Evaporator I Exhaust Contract 40167 

~TC OO ~ FCORY ACCEPTANCE TEST PLAN SpcON. RPEC-306 

7T8.]11 CONFIRM fan and motor bearings reach a steady equilibrium temperature at which 

point the temperature no longer rises (+3 0 F over 10 minutes). 

7.8.12 MEASURE the differential pressure between ?DIT location K1-PDIT-'109 up stream 


+/- 0.5 inl120 is observed 

7.8.13 MEASURE the differential pressure between PDIT location KI -PDIT-312 up stream 

of the filters and atmosphere, adjust valve setting until a differential pressure of -3. 6 

+/- 0.5 inH 2O is observed 

7.8.14 RECORDX. controller out % on FITO 2 and 3, motor input frequency, differential 

pressure at PDIT location K1-PDIT-309, differential pressure at PDIT location KI - 

PD]J7-3- 12, stack flow, motor current, motor and fan bearing temperature, fan shaft 

bearing vibration, and motor be aring vibration in Attachment 7.8. 

7. 8.15 RE CORD the % open of the FCV-1 and FCV-2 at 13,500 scfin 

FCV-1 L 0 FCV-2 3 d 

7.8.16 INCREA&SE input frequency by .5 Hiz and repeat steps 7.8.11 - 7.8.14 until fan 

reaches 19,500 scfm. 

NOTE: Data is to be taken over the entire operation range from 13,5 00-scfin to 

19,500-scfin at 30 rpm increments. In cases where the recorded values are close to 

the acceptance criterion, reading are to be taken at 10 rpm increments. 

7.8.17 INCREASE input fr-equency to 60 Hz and repeat step 7.8.14. 

7.8.18 RECORD the % open of the FCV-1 and FCV-2 at 19,500 scfmn 

FCV-1_______0 FCV-2 2U 

7.8.19 MEASURE the differential pressure between PDIT l ocation KcPI-3 I 

downstream of the filters and I" nozzle located just above stack wye section. 

7.8.20 RECORD PDIT to Stack differential pressure, 5 , 71f' ii 2o 

7.8.21 REVIE W test results. 


47 Premier Technology, Inc. 006765.O.OOO-FAT-0O1-1 (Rev 6)


Page A-16 

PiREM~IER TECHNOLOGY, INC. Project No. 006765.0.000 

jN'IIER WRPS - 242-A Evaporator K1 Exhaust 

FACOR ACEPANCE TEST PLAN 

contact 16 

Spec No. 1RPP-SPIIC 

(7~K 

(PREM IERx A Ventilation System No. 406 

7.8.23 Test Director VE RIfY test is complete. 


/ 3/2-qh 

7.8.24 QA Inspector VER)IFY test is complete. 

/4 / /'/b 4 ~ 4f 


Date 

Date 

7.8.25 CONTINUE to sound test 7.9 K-1-5-2 Fan and Motor - Sound Test 

7.9 KI-5-2 Fan and Motor - Sound Test 


BACKGROUND - This test is to show that the sound level ratingsp are in accordance with 

RPP-SPEC-3 6062, Rev 0 

ACCEPTANCE CRITERIA - Mechanical equipment noise emission at the maximnum 

flow rate condition do not create levels equal to or greater than 85 dBA over a weighted 8hour 



KI-5-2 Fan and Motor 



Equipment IModel # Srial # Calibration Due 

_________________ ________________ Date: 

7.9.2 "VERIFY that the exhauster fan has reached steady state operation. 

48 Premier Technolog, jnc. 

006765.O.OO-FAT-0I-1 (Rev 6)


Page A-17 

PREMIE R TECHNOLOGY, INC. Project No. 006765.0.000 

WRPS - 242-A Evaporator K1 Exhaust Contraet 40167 

& TVentilation System No. RVSE-66 

FCOYACCEPTANCE TEST PLAN Spec No. RPPSev 0 -3 

7.9.3 RECORD max sound at 1 meter from mechanical equipment 

Max sound level at 1 meter fromn mechanical equipment:.. R .. dBA 

#NOTE: if any so-Lnd level is greater than 85 dBA the cause shall be determained and 



7.9.5 Test Director VERITY test is complete. 



/ q ~i 

Date 

QA Inspector Signature 'rkL~t % Date 

7.9.7 CONTINUE to sound test 7.10 Section 1 Valves/Dampers - System Pressure 


7.10 Section I Valves/Dampers - System Pressure Boundary Leak Test 


of the damnper housing and interfaces with system. 


*Kl-BDD-001 

0KI-DMPR-001 

.KI-MOV-001 

ACCEPTANCE CR][TERIA - no bubble indications 


7.10.1 SET fan speed to achieve 19,500 scfmn. 

7.10.2 CONDUCT bubble leak test in accordance with PTI-TP-l .7 Rev 5 Bubble Leak Test 

Procedure. 

49 Premier ecnloy Ic 

006765.0.000-FAT-OQ1-1 (Rev"6

(~v 

PREMIWER TECHNOLOGY, INC. Project No. 006765.0.000 

,r~~'R WRPS - 242-A Evaporator 1(1 Exihaust Contract 

C ,n, ,gII 

.Ventilation System N. 4I 


Page A-18 

FACTORY ACCEPTANCE* TEST PLAN. Spec No. R"Sev 06 


Location Description Satfisfied U11- Test QA 

___________ From To _____satisfied Director inspector 

2 KI DMPR-001 DUCT 14 IA 

3 DUCT KI-BDD-001 y 

4 Kl-*BDD-001 EXPATION j~ _ 

JIT RANSIXON 

EXPANTIoN FAN OUTfLET 

__ C 

7.10.3 TEST KI-BDD-001 frame for bubble leaks. (This is for customer information only) 

TEST NOTES: Leak o e 

(Addesipon of severity and location of leaks) 

e, ksr e yeed~n 44 60 7, M 3soI 


7.10-5 Test Director VERIFY test is complete. 


7.10.6 QA lInspector VERIFY test is complete. 


7.10.7 CONTE14UE to Ki -5-2 Fan and Motor 7.11 -Vibration Test (Maximum System 

Loss) 

7.1.1 11-5-2 Fan and Motor - Vibration Test (Maximum System Less) 

MATRIX REFERENCE - line 4, 9,47 & 48 



50 Premier Technology. Inc. 006765.0.000-.FAT-001-1 (Rev 6)

®entM1ER 


Page A-1 9 

PRE MIFER TE CHNOLOGY, INC. Project No. 006765.0.000 

WRPS - 242-A Evaporator K(1 Exhaust Contract No. 40167 

- hll~ 1 UP. VetiatonS tePEC-36062) 


equilibrium temperature, at which point thle temperature no longer rises (+3 OF over 10 

minutes). ASME AG-i TA-4 159 Fan Performiance/Aiflow Capacity Test For systems with 

filter or absorber banlcs,'the fan performance shiall b e measured under maximum design dirty 

-filter conditions. This may be done by increasing the system resistance to the designadirty 

filter differential pressure, (design basis maximum dirty filter condition), using artificial. 

resistance. 


* Kl1-5-2 Fan and Motor 


* Vibration: Measured in all three planes. The criteia for low horsepower, industrial 

process or petrochemiical applications, Fan Application Category AMCA 204 BV-3, 


* Sample flow is constant as the exhauster flow is varied. Sample flow will be with 

within 2 scfm. 




Equimen Modl USeril #Date: 

Theovywc r S'IL& 94. FiUS 

ce. AlAt er, P6~ 

ovtoy4 

Odo V - 



+/- 0.5 inH2O is observed. 

7.11.3 ME ASURE the differential pressure between PDIT location KI -PDIT-3 12 up stream 

of the filters and atmosphere; adjust valve setting until a differential pressure of-8.9 

+/- 0.5 inHO is observed. 




a,. E I R WPS - 242-A Evaporator 1(1 Exhaust Contract 406 

Te2~chno.-jrf- Ventilation System No. 406 


Page A-20 

FACTORY ACCEPTANCE TEST PLAN Spec No. RPPSev 0 06 

7.11.4 MEASURE the differential pressure between PDIT location K1-PDIT4G Vi2'111 

downstream of the filters and 1" nozzle located just above stack Wye section. 

7.11.5 RECORD PDIT to Stack differential pressureJa± 7nH 2 

7.11.6 RECORD motor input frequency, differential pressure at PDIT location KI-PDIT- 

309, differential pressure at PD1T location Ki -PDIT-3 12, stack flow, motor current, 

motor and fan bearing temperature, fan shaft bear ing vibration, differential pressure 

at filter train PDIT's, and motor bearing vibration in Attachment 7.11. 


7.11.8 p.of-or 







7.11.14 QA Inspector VERIF'Y test is complete. 


7.A2KIbS-3M. Motor and --- ,D - Proper voltage at equipment ser'ed 

See 1e?& 67 iAprtSri off CA' 9/1t) 

MATRIX REFERENCE -line 14, 15, 26, 27 & lr 



COMIPONENTS BEING TE STED: 

9*KI -5-3 Fan and VFD 

52 Premier Technology, Inc. 006765.O.OOO-FAT-0OI-1 (Rev 6)


N IT R WEPS - 242-A Evaporator Ki Exhaust Contract 40167 

\~~i~Y LJIVentilation System No. 


Page A-21 

FACTORY ACCEPTANCE TES TPLA Spec No. , 0SPC366 



excluding service factor considerations. Voltage will be within + 10% of the nameplate 

rating for the motor and. VFD. Breakers and other circuit protection devices function. 


7.12.1 RE CORD equipment and calibrati on information. 


Equiment Modl ##Seril #Date: 

7.12.2 RECORD initial VFD settings in table FAT 7.12 

7.123 VERIFY valves/dampers are set in accordance to valve line up table 

Valve/Damper .Description Position Initials 

KI-HV-001* Inlet Plenum to Filter Train A Open _____ 

I-HV-002 Inlet Plenum to Filter Train R Open 

KI-HV-003 Inlet Plenum to r iter Train C Closed 

KI-HV-010 Filter A To Switch Plenum closed 

KI-11V417 Filter B TJo Switch Plenum Closed 

KI-HV-07,4 Filter C To Switch Plenum Closed 



Kl-DMPR-01 Fan to Stack Isolation Damper (North) Open 

I-DW~R-O00 Fan to S tack Isolation Damper (South) Open 


7.12.5 MEASURE voltage on the VED Supply side and record value in table 

53 Premier Technology, Inc. 006765.0.OO-FATOQ01-l (Rev 6)

PREM IR TECHNOLOGY, INC. Project No. 006765.0.000 

EbTNERrl WRPS - 242-A Evaporator KI Exhaust Contract 406 

iX Ventilation System No. 406 


Page A-22 

FCTORY ACCEPTANCE TEST PLAN Spec No. RPPSev 06 

rCb DG r~b I DG 

FrI b Ramp Frib Ramn 

ESf Min Out fS Mini Out 

FLR Mal Out FLR Max Ot'r 

OPL Rev OPL Re, 


7.12.26 VERIFY KI -MOV-002 is closed. 

7.12.27 VERIFY Kl-BDD-002 is closed. 


7.12.29 RECORD final VFD settings. 






7.13 K1$-53 Fan and Nlt~ - Vibration Test (Minimium Systemt Loss) 

MIATRIX REFERENCE -line 8 

BACKGROUND - Prior to taking the vibration, measurements, the fans shall be operated at 

the normal operating speed for a run in. period of time until the bearings reach a stable 


minutes) .This test is to determine the vibration of the fan and motor under minimum system 


prior to the Fan Performance/Airflow Capacity test. ASIE AG-i TA-3 533 -Vibration 

measurement shall be taken on the accessible motor/fiai bearing housing in at least two 


56 Premier Technology, Inc. 006765 .0000-FAT001-1 (Rev 6)


Page A-23 

REMJER TECHNOLOGY, INC. Project No. 006765.0.000 

1W T N I 1 WRPS - Z4Z-A Evaporator Ki Exhaust Contrac 

Y RLt~ Ventilation Systern No. ct 40167 

FiACTORY ACCEPTANCE TEST PLAN Spec No. Re 

When the bearing housing is not accessible the frame of the component may be used if it. 


COMPWONENTS BEING TESTED: 

*Kl-5-3 Fan and Motor 

ACCE PTANCE CRITERIA: 

*0 Vibration: Measured in all three planes. The criteria for low horsepower, industrial 




7.13.1 CONFIJRM new clean filters are installed in filter housings A, B, and C. 



KI-HV-O0i Inlet Plenum to Filter Train A Closed CVk' 

K1-H1V-002 Inlet Plenum to Filter Train 11 Closed ck' 

KII-HV-003 Inlet Plenum to Filter Train C Closed C 

Ki-HY-OlO Filter A To Switch Plenum Open 

KI-HV-017 Filter D To Switch Plenum Open 

KI-HV-024 Filter C To Switch Plenum Closed 

Kl-MOV-001 Plenum to Fan Isolation Damper (North) (Closed) A 


lKI-DMPR-001 Pan to Stack Isolation Damper (North) Open 

KIDPR-002 Fan to Stac k Isolation Damper (Suth) IOpen J C 

7.13.3 VER]W power to the VFD is on. 

7.13.4 CONSULT and IMPLEIMENT any additional safety precautions as required by 

Premier lab-safetyfsafbty-moflitor personnel. 

7.13.5 SET the VFD speed to 101Hz (17%) 


006765.0.OOO-FAT-001-1 (Rev 6)

EM 

PREMvUR TECHNOLOGY, INC. Project No. 006765.0.000 

IE WRPS - 242-A Evaporator KJ E xhaust Contc 406 



Page A-24 

FACTORY ACCEPTANCE TEST PLAN Spec No. PP-SPEC-36062 

R~ev 0 



7.13.7 OPEN KI -H%7-001 and KI -HV-002 to 75 % 

7.1 3.8 START Kl-5-3 fan and allow it to run for one hour. 

7.13.9 INCREASE\TFD Hz setting, until 13,500 scfm is measured. 

7. 13. 10 CONFIRM fan and motor bearings reach a steady equilibrium temperature at which 

point the temperature no longer rises (+3 'T over 10 minutes). 




7.13.12 MEASURE the differential pressure between PDIT location K1-PDIT-3 09 up stream 



7.13.13 RECORD Beta and record flow from FITO 2 & 3, motor input frequency, 

differential pressure at PDIT location KI-PDIT-306 , differential pressure at PDIT 

location Kl-PDIT-309, flow at stack sampling, motor current, motor and fan bearingol 

temperature, fan shaft bearing vibration, differential pressure at filter train PDIT's, 

and motor bearing vibration in Attachment 7.13. 

7.13.14 INCREASE input frequency by .5 Hz and repeat steps 7.13.11 - 7.13.13 

NOTE. Date is to be taken over the entire operation range from 13,5 00-sofin to 

19,S00-scfba at 30 rpm increments. In cases where the recorded values arc close to 

the acceptance criterion, reading are to be taken at 10 1pm increments. 

*7.13.15 ME ASURE the differential pressure between PDIT location KI-PDIT-3-t4' 

downstream of the filters and 1" nozzle located just above stack wye section. 

7.13.16 RECORD PDIT to Stack differential pressure...i 5 1LnH 2 O 

7. 13 .17 REVIEW test results. 

7. 13.IS CONFIRM the acceptance criteria have been met. 


58 Premnier Technology, Inc- 006765.O.0O-FAT-001-1 (iRev 6)

PREMIE R TE CH:NOLOG Y, INC. Project No. 006765..000 

I~)N T fh WRPS - 242-A Evaporator Ki Exhaust Contrnct 406 

E I RVentilation stemn No. 4D 

& nc.RPP-SPEC-360 

T,6 noig7, 

rFACTORY ACCEPTANCE TEST PLAN Spec No. Re 

F 


7-13.20 QA Inspector VE RITY test is complete. 


Date 

Date 

7.13.21 cONTJNU[Mto 7.14 KI-5-3 Fan and Motor - Sound Test 

7.14KI-5-3 Fani and Motor - Sotmd Test 

.1* 



Page A-25 

BACKGROUNTD - This test is to show that the sounid level ratins are in accOrdance wt 

RPP-SPEC-3 6062, Rev 0 

COMPONENTS BETG TESTED: 

K1-5-2 Fan and Motor 

ACCEPTANCE CRITERIA - Mchanical equipment noise emission at thle maximum 

flow rate condition do not create levels equal to or greater than 8 5 dBA over a weighted 8hour 


TEST PROCE DURE: 

7.14.1 VERIFY that the exhauster fan has reached steady state operation. 

.7.14.2 RECORD rnax sound at 1 meter fromn mechanical equipment. 

Max sound level at 1 meter from mechanical equipment: 3 1 dBA 

.&NOTE: if any sound level is greater than 85 dBA the cause shall be determined and 



7.14.4 Test Di rector VERIFY test is complete. 



/x-/'~i 

Date 

006765.0.000-FAT-001-I 

6 2 



Page A-26 


WVRPS - 2,42-A Evaporator KI Exhaust Contract 

& EM IER Ventilation System No. 40167 

FACTORY ACCEPTANCE TEST PLAN Spec No.Re0 


6.. c / 

QA Inspector Signature A\~'Date 

Z-,GFTEl ET-rEPrT1:- DL Ie 

7.14.6 CONTINUE to sound test 7.15 Section 2 Valves/Dampers - 


System Pressure 

7.15 Section 2 Valves/Dampers - System Pressure Boundary Leak Test 


of the damper housing and interfaces with system. 


uKl-BDD-002 

*Kl-DMPR-002 

*KI-MOV-002 

ACCEPTANCE CRITERIA -no bubble indications 


7.15.1 SET fan speed to achieve 19,500 scfrn. 

7.15.2 CONDUCT bubble leak test in accordance with PTI-TP-l.7 Rev 5 Bubble Leak Test 

Procedure. )( Ste (cs e.-CeeP&'W~2CQjoI 

FAT 7.15 ASMEf AG-i, TA-4233 & TA-4234 Initials 

LoainDescription ISatisfied Un- Test QA 

LoainFrom ] To Satisfied Director Inspector 

I STACK KI-DMPR-001 'FAIsi.. 

2 Kl-DMPR-001 DUCT A L( 

3' DUCT KI-]3DD.02 ...L..i1±.- 

4 KI-BDD-001 EXI'ANTION ~ ___ A 

________JOINT 

_________ 

5 EXPANTION FAN OUTLET _ _ ~A / 


Tcnig 

Teo. 

PREMIER TECHINOLOGY, IWC. Project No. 006765.0.000 

W RIS - 242-A Evaporator 1(1 Exhaust Contract 40167 

Ventilation 

No.ei 


Page A-27 

FACTORY ACCEPTANCE TEST PLAN Spec No. P-SC366 

7.15.3 TEST Kl -BDD-002 frame for bubble leaks. (This is for customer information only) 

TEST NOTES: Leak lora: 

(Add des ription of severity and location of leaks) 

j 0S't (-)Y C0c~r- ~ 0oo7,ek- 3/ya/1, 

7.15.4 CONFIRM the accepdonce riteria have been met for each damper. 

7.15.5 Test P)or VERIFY test is complete, 


7.15.6 QA Inspector VE RIFY test is complete. 


Date 

7.15.7 CONTINUE to sound test 7.16 Stack Joint -Boundary Leak Test 

7.16 Stack Joit - B tbble leak test 

BACKGROUND - ECN 727024 test is to be performed per ASME AG-1(SA-4533) a 

bubble leak tests is to be per formed to ensure that unmonitored exhaust does not escape 

through the joint. The leak test shall be set-up to mimic the on-site conditions, specifically 

with respect to gasket material and size, hardware material and size and torque applied to the 

*bolting. 


* Stack Assembly gasket joint 

ACCEPTANCE CRITERIA -NO Bubble indications 



Dt 

006765.O.OO-F'AT-001-l (Rev 6)

3 ~ 


Page A-28 

PREATIER TECHNOLOGY, INC. Project No. 006765.0.00)1 

i IE R WRPS - 24-2-A Evaporator Ki Exhaust Contract 406 

RE Inc Ventilation System No. 406 

Technkogy 11"C Spe No. RPP.7PEC-36062. 

FACTORY'ACCEPTAINCE TEST PLAN SpcN. Rev 0 

7.16.1 CONFIRM sampling monitoring system is operating. 

7.16.2 CONDUCT bubble leak test in accordance with PT1-TP-1 .7 Rev 5 Bubble Leak Test 

Procedure at all mechanical Joints listed for equipment in table below. 

-~~~~~ 

7.. TA- 42O34 2 

FAT 7.16 ASMIE AG-i1, TA-4233 & TA-4234 initials 

Description Satisfied san- ed t Q 

Equipment roTosatisfied Director Inspector 

Stak STACKSTC 


7.16.4 Tes D tor VE RIFYtest is complete. 


Date 

/ 

7.16.5 QA Inssetor VERFY test is complete. 


Date 

7.16.6 CONTINUE to 7.17 KI-5-2 Fan and Motor - Vibration Test (Maximum System 

Loss) 

7.17F,1-573 Fart and Motor- Vibrabtt Test (Maximum System Loss) 

MATRIX REFERENCE - line 4 & 8 

BACKGROUND - Prior to takingthe vibration measurements, the fans shall -be operated at 

the normnal operating speed for a run in period of time until the bearings reach a stable 

equilibrium temperature, at which point the temperature no longer rises (+3'F over 10 

minutes). ASME AG- I TA-4159 Fan Performance/Airflow Capacity Test For systems with 

filter or absorber banks, the fan performance shall be measured under maximum design dirty 

filter conditions. This may be done by increasing the system resistance to the design dirty 

filter differential pressure, (design basis maximum. dirty filter condition), using artificial 

resistance. 

62 Premier Technology, Inc. 006765.0.OO-FATOOIA- (Rev 6)

~choio~ 

PREAIER TECHNOLOGY, INC. Project No. 006765..00 

WRPS - 242-A E vaporator Ki Exhaust Contract 40167 

~Ventilation System No. 


Page A-29 

FACT'ORY ACCEPTANCE TEST PLAN Spec No. RFPP*SPEC-~36062 


COMPONE NTS BEING TE STED: 

* K] -5/fian and Motor 


* Vibration: Measured in all three planes, The criteria for low horsepower, industrial 


8.8 mm/s EMS velocity (filter out) 


7.17.1 MASURE the differential pressure between PDIT location Kl-PDIT-306 up stream 



7.17.2 MASURE the differential pressure between PDIT location KI -PDIT-309 up stream 


+-0.5 in&I2O is observed 

7.17.3 ME ASURE the differential pressure between PDIT location K1 -PDIT-3 14 


7.17.4 RECORD PDIT to Stack differential pressure 10-1 inFI 2 O0 

7.17.5 RECORD motor input fr-equency, differential pressure at PDIT location Kl-PDIT- 

306, differential pressure at PDIT location K1-PDIT-3 09, flow at stack sampling, 



7.17.6 RE VIEW test results 


7.17.8 STOP motor and allow it to come to rest 

7.17.9 REMOVE temporary power fromn terminals 13 and 14 on TB-6. 

7.17. 10 TestDim otor VERIFY test is complete. 



PREMIER TECHJNOLOGY, INC. ProjectNo. 006765.0.000 


E I RVentilation System No. 406 


Page A-30 

FACTORY ACCEPTANCE TEST PLAN Spec T'o. RPEC-306 

7.17.11 QA Inspector 'VERIFY test is complete. 

QA Inspector Signature .'Dat 

F. F4.;-7nai Ac -~ Aifo D Atib o F (lS ll S!'Sew 

Rce lier -49 r S'-CC41i,/ 


BACKGROUND) -this section provides the field acceptance test requirements for installed 

pre-filter and HEPA filter banks. Acceptance tests shall be conducted with pre-filter and 

HEPA filter banks installed. (ASMEff AG-i TA-4632 Airflow Distribution Test) With the 

system operating at design flow rate (18,000 scfmn; 19,500 max) the airflow distribution shall 

be measured downstream of each pre-filter and HEPA filter bank. 

COMONENTS BEING TESTED: 

*Filter Train 

*Inlet 

*Outlet 


*Isolation valves 

*Transition to fan inlet 

*Flexible metal connector 

*Ductwork 

ACCE PTANCE CRITERIA -Velocity measurements across the HEPA filter banks shallI 

be limited to +20% of the average. 


7. 19.1 ENSURE valve line-up is in accordance with valve table 


KI-HTV-001 In let Plenum to Filter Train A Closed 

Kl-HV-002 Inlet Plenum to Filter Train B Closed 


KI-HV-010 Filter A To Switch Plenum Open ____ 

K] -H V-Oil Filter B To Switch Plenum _t Open 

64 Premier Technology, Inc. 006765.0.OO-FAT-001-1 (Rev 6)


Page A-31 

PREMFER TECHNOLOGY, INC. Project No. .006765.0.000 

~IN T R WRPS - Z42-A E vaporator KI Exhaust contract 40167 

.)E I R Ventilation. System ____ 

FACTORY ACCEPTANCE TEST PLAN Spec No. RPPSev 06 

ICI-HV-024 Filter C To Sivitch Plenum Closed 


KI-MOV-002 Plenum to Fan isolation Damper (South) (Closed)_____ 


IIDP-0 Fan to Stack Isolation Dampe (South) Open 

7.18.2 VERIFY power to the VFD is on.. 

7.18.3 CONSULT and IMPLEMENT any additional safety precautions as required by 

Premier lab-safetylsafety-imonitor personnel. 

7.18.4 SET the VFD speed to the required Hz to achieve 18,000 sofin +10% (use 

-Attachment 7.18 information) 



7.19.6 OPEN Kl-HV-001 and KI-HV-002 

7.18.7 START K1-5-3 fan 

7.18.8 RUJNNUCON procedure 12-101 rev 7 (Attachment 7.18) 



Test Dir'ector Signature 

7. 19.11 QA Inspector VERIFY test is complete. 


Date 

Date 

7.18.12 CONTINUE to 7.19 Filter Train B - Airflow Distribution (Full System) 

7.19IFilter Train~ B - Airflow Distribution (Full System) 



006765.O.OO0-FAT-0O1-1 (Rev 6)

PREMIER TECHNOLOGY, [NC. Projct 1N. 006765.0.000 

~r~MTVT WRPS - 242-A Evaporator K11 Exaust Contract 

(AI RVentilation System N.. 40167 


7.22.4 VERIFY that tracer gas variation is less than 20% across the area of the stack 


7.22.6 STOP motor and allow it to come to rest 

7.22.7 REMOVE temporary power from termninals 13 and 14 on TB-6. 





Date 

Date 


Page A-32 

RP'P-SPEC-36062 

7.23 Exhaiist Stack Sample Line - -Heat Trace Thermostat for CAkM airborne 

Radiation Detector (GS) 

MATRIX RZEFERENCE - line 45 

BACKGROUND - this test is a functional test that is to verify the operability of the Sample 

line heat tracing. Continuous Air Monitor (CAM) Vendor literature limits the internal gas 

temperature to 120"F. 


* Stack Heat Trace 

ACCEPTANCE CRITERIA - Verify the thermostat functions to turn the heat trace "ON" 

and "OFF" (change of state determined by detection of heating or energized circuit) at 

11 5 0 F. 


7.23.1 ENSURE that the controller is wired as per instruction manual 

7.23.2 ENSURE power to the heat trace circuit is on. 

7.23.3 CONNECT an ohm /continuity meter to the Heat trace connections. 

72 Premier Technology', Inc. 

006765.O.OOO-FAT-O01-1 (Rev 6)

PREM~IiER TECHNOLOGY, INC. Project No. 006765.0.000 

(PEM I ER WRPS - 242-A E vaporator K1 Exhaust Contract 40167 


Page A-33 

:llfll~gI 


FACTORY ACCE PTANCE TEST PLAN Spec No. Rev 0 

7.23.4 SET the thermostat to 11 5 0 F and note that whether that controller relay is open or 

closed via the meter reading (should be closed). 

7.23.5 HEAT (using a heat guns) the RTI) at the end of the thermocouple lead (white cable) 

7.23.6 CONFIRM when the temperature reading passes 11 5 0 F, note whether or not the 

relay opens as the temperature passes the 1 15'F point. 

7.23.7 ALLOW the RTD to cool past the set point and note that the relay closes. 

7.23.8 RESET the set point to 40 0 F, remove the power and sign off the test. 

Fat 7.23 Heat Trace Inbitials 

Hest Trace Step 7.23.A Step 7.23.6 Step 7.23.7 Test QA 

Controller. (Open/Closedl) (Open/Closed) (Open/Closed) Dirctlor Inspector 

IrC-3 

HTC-KI-5-3 1~-5~ 

tod j xi~ 

k 

Drain 610c___ 

HTC-Staek Clarr. * ge- Cjar 

7.23.9 CONFIRM the acceptance criterion has been met., 




Date 

7.24 Continuous Air Monitoring - Verify CAM by ass feature 

MATRIX REFERE~NCE - line 50 

BACKGROUND --CAM bypass feature allows functional testing and filter paper change 

out while maintaining continuous exhauster operation. 

73,- Premier Technology, Inc. 

006765.O.OOO-FAT-0O1-1 (Rev 6)

PREMIIR TECHNOLOGY, INC. Project No. 006765.0.000 


Page A-34 

T, j p WRPS - 242-A Evaporator Ki Exhaust Contract 406 

Ventilation Sstem:NE.ha0s6 

Mc. RPP-SPEC-36062 

FACTORY ACCEPTANCE TEST PLAN Spec No. Rv 


CAM bypass 

ACCEPTANCE CRITERIA -CAM bypass feature allows functional testing, and filter 

paper change out while maintaining continuous exhauster operation. 

TEST PROCE DURE: 



KI-HV-001 Inlet Plenum to Filter Train A Open 

KI-BV-002 Inlet Plenum to Filter Train B Open CI( 

KI-HV-003 inlet Plenum to Filter Train C Open Iy 

K1-HY-OlO Filter A To Switch Plenum Open 

KI-13V-017 Filter B To Switch Plenum Open. 

KI-HV-024 Filter C To Switch Plenum Open COr 

LC1-MQV-0O1 Plenum to Fan Isolation Damper (North) (Closed) / 

KiI-MOV-D02 Plenum to Fan Isolation Damper (South) (Closed) 

KI-DMPR-001 Fan to Stack Isolation Damper (North) Open 

KI-DMPR-002 Fan to Stack Isolation Damper (South) Open C 

7.24.2 VEERFIY cabinet 400 is ON. 

7.24.3 REMOVE red wire #65 for 1-8 terminal from AM-I (smart relay). (NOTE: this is to 

simulate a high radiation alarm). 

7.24.4 SET KI1-5-3 VFD to 45Hz.7 

7.24.5 START KI-5-3 (NOTE: KI1-5-3 should not be able to start.) 

7.24.6 CONFIRM if KI1-5-3 will start YES (20V 

7.24.7 TURN CAM bypass switch to the ON position. 

7.24.8 START KI1-5-3 (NOTE: 1(1-5-3 should be able to start.) 

7.24.9 CONFIRM if Kl1-5-3 will start 


c7DNO 

006765.O.0O-FAT-01-1 (Rev 6)


Page A-35 

PREMIER TECHNOLOGY, INC. I'rojcct No. 006765.0.000 

U E IER WRPS - 242-A Evaporator KI Exhaust Contract 40161 

~Te-cnoo IncVentilation System No. 

FACTORY ACCE PTANCE TEST PLAN Spec No. P-EC30') 


7.24. 10 STOP nmotor and allow it to come to rest. 

7.24.11 RECONNECT red wire #65 to 1-8 terminal. 



Test'Director Signature Date 

7.24 .14 QA kbspector VERIFY test is complete. 


7.25 Vacuum Pump - Verify Pump operation 


BACKGROUND) - This test is to verify' the pumnp operation and cabinet envirounental 

conditions. 

COMPONENT BEING TE STEI): 

*Vacuum Pump 

ACCE PTANCE CRITERIA - The vacuum pumps shall be capable of drawing a minimum 

of 1.42 1'S (3 scfan both pumps running) at system static pressure through the 

sample/monitor loops. The pumps will not surge during operation. 


7.25.1 INSURE cabinet 400 is turned on and a vacuum pump is running. 

7.25.2 RE CORD FITC-2 eand FITC-3 flow readings. 

FITC-2 Flow Reading 1, q4 FITC-3 Flow Reading--0 

Sum of FITC-2 and FITC-3 flows ''I' 

7.25-3 CLOSE HV-3 and HV-4 (NOTE: relief valves should lift) 

75 Premier Technology, Inc. 006765.0.0-FAT-0l-1 (Rev 6)


WRPS .- 242-A Evaporator KI Exhaust E :1rac 

Tehooy iVentilation System No. 40167 


Page A-36 

FACTORY ACCEPTANCE TEST PLAN Spec No. RPPSE-30 6 

7.25.4 RECORD max vacuum level on PITC-4 (should be over 12 ing) 

PI1TC-4 Max Vacuum Reading 2, /3h 

7.25.5 OPEN HV-3 and )4V-4 

7.25.6 CONFIERM the acceptance criteria have been mot, 





Date 

Date 

7.126 CAM Operation - Verify No Electromagnetic Radiation interference 


BACKGROUND - CAM unit is to be checked with exhauster components per RPIP-SPBC- 

3 6062, Rev. 0, Section' 3.2,4.2 


AM-- 

ACCEPTANCE CRITERIA - No inadvertent a larms, interlocks, or sporadic indications in 

the CAM operation due to interference from outside electronic devices 




KI-H"V-001 Inlet Plenum to Filter Train A Open A 

Kl-HV-002 Inlet Plenum to Filter Train B Open 

KI-EV-003 Inlet Plenum to Filter Train C Open (J( 

KI-HIV-010 Filter A To Switch Plenum Opean 


OO6765.0.00-FAT-00I-l (Rev 6)


Page A-37 


(P'EMN4 ER WRPS - 242-A Evaporator Ki Exhaust Contract 416 

~cholo~ ic.Ventilation System No. 

FACTORY ACCEPTANCE *TEST PLAN SpcN. RPP-SPEC-36062 

ReevN. 0 

Kl-HV-017 Filter B To Switch Plenum Open 

KI-HV-024 Filter C To Switch Plenum Open 

KI-MOV-001 Plenum to Fan Isolation Damper (North) (Closed) ($ 

KIl-MOV-002 Plenum to Fan Isolation Damper (South) (Closed) 

Kl-DMIPR-001 Fan to Stack Isolation Damper (North) Open CI( 

KI-DMIPR-002 Fan to Stack Isolation Damper (South) Open ______ 

7.26.2 VERPIY cabinet 400 is on. 

7.26.3 SET Kl-5-3 VED to 45 Hz. 

7.26.4 START Kl-5-3 

7.26.5 KEY a hand held radio around cabinet 400. 

7.26.6 CONFIRM no invert alarms, interlocks or sporadic indications are observed at the 

CAM 

7.26.7 CONFIRM if Kl-5-3 does not shut down. YES ~ I 



?est Director Signature Date 


313' 




BACKGROUND - this test is to simulate a temperature conditions to show the proper 

function of the sample cabinet cooling fain per RPP-SPEC-3 6062, Rev. 0, Section 4.1.20 

COMPONENTS: BEING TESTED- 

F 77 Premier Technology, Inc. 006765.O.000-FAT-O01-l (Rev' 6)


Page A-38 

I PREMIER TECHNOLOGY, INC. Proj ectNo. 006765.0.000 

(~E I~ W RVentilation System 

WRES - 242-A Evafporator K1t Exibaust Cont ract 4016' 

NO. 

~ 1~~inoiigy~Inc.RPP-SPEC-36 


F-400 

ACCEPTANCE CRITERIA - Fan will turn on at I10'O F 

TE ST PROCEDURE: 

7.27.1 VTER]FY cabinet 400 is on. 

7.27.2 BEAT cabinet thermostat area with a heat gun. 

7.27.3 VERIFY cabinet fan will turn on at 1 100 IF 

7.27.4 Temperature when fan turned on S( c C 4Oywm 00 f 

7.27.5 CONFIR~M the acceptance criterion has been met. 




6> 4 /6 


Date 

Date 

7.28inlet Plenumi & Expansion Joints - Pressure Decay Test & Bubble Leak 

Test 

MATRI REFERENCE - Line 23 


of the damper housing and interfaces with system i accordance with ASMIE AG-I 

Section TA-3 523 and Mandatory Appendix TA-Hn. (TA-.3523-TA-IU-Ii10) SUNEMARY 

OF METHOD Ducts and housings thiat form the pressure boundary of the system shall be 


used and will produce a similar test result. The constant pressure method is -useful for testing 

small volumes and is conducted at the maximum operating pressure for the system. Thie 


1 / times the maximum operating pressure, then. allowing the pressure to decay for a fixed 

period of time, or until the pressure decreases to 80% of the maximum operating pressure. 


06 2 

006765.O.0OO-FAT001-1 (Rev 6)


Page A-39 


ER WRIPS - 242-A Evaporator KI Exhaust Contract 406 

Ventilation System No. 

FACTORY ACCEPTANCE TEST PLAN SpcN. RIP-SE-6 

whichever occurs fist. Fans, dampers, 'and Other -omIponents that are part of the pressure 


connection leak tightness. If the measured leak rate is in excess of the acceptance crteria, 


repaired, the duct and housing shall be retested to verily leak-tightness. 


*All gasket joints on the inlet plenum and expansion joint on the inlet of the filter 

trains 

ACCE PTANCE CRITERIA: 

*No bubble indications 

* The leak rate shall not exceed 0.23 ft? per hour at a pressure of -23.7 inHi2O (see 

Attachment 6.23). 


7.28.1 INSTA.LL blanking plate on Ember screen. 

7.28.2 VERIFY valves/dampers are set in accordiance to valve line up table 

-Valve/Damper' Description Position Initials 

KI-ffV-0D1 Inlet Plenum to Filter Train A Closed 

Kl-BV-00-7 Inlet Plenum to Filter Train B Closed 


I-HV-010 Filter A To Switch Plenum Open 

KI-HV-017 Filter DI To Switch Plenum Open 

K1-BV-024 Filter C To Switch Plenum Open 

KCI-MOV-001 Plenum to Fan Isolation Damper (North) (Open) 

KI-MOV-002 Plenum to Fan Isolation Damper (South) (Open) 

7.28.3 INSTALL pressure relief device set at 25 inH 2O 

7.28.4 PRESSURIZE system with compressed air to 1 V/4 times Max Operating pressure 

(23.7 inHi 2O) 

79 Premier Technology, Inc. O06765.O.OO-FAT-ool-I (Rev 6)


Page A-40 


r~I1?jA1IIR RMS - 242-A Evaporator K1 Exhaust 

E Inc. Ventilation S stem 

Techno.09v, nc. 

Contract 

No. 

40167 

pp-SPEC- 36 O 62 



Procedure see Atahent 7.4. 

7.28.6 VERIFY there are no bubble indications On gasket joints. 

7.28.7 CONDUICT rate of decay test in accordance with PTI TP-1.15,67 65 Pressure Decay 

Test (see Attachment 7.4). 






7.29 Exhaust Stack Sample Pitot Tube and Transport Lines - Leak test & Pitot 



Dt 

Date 


installation in accordance wit ANSI N 13. 1, Section 6.9. PIC03 stack allows for inspection 

as satisfactory method. Isolate and pressufize sample line to .75 psi. 


*Exhaust Stack sample pitot tube and transport lines 

ACCEPTAC CIERIA - No leaks detected using bubble testingy onjoints and weld 

seams. 

TEST PROCEDURE- 

7.29.1 CAP open ends of sample lines. 

7.29.2 INSTALL pressure relief device set at 25 inl{2O. 


0O6 7 65.0.000OFAT-001-1 



Page A-41 

PREMIER TECHNOLOGY, INC. Project No. :0067=65.0.000 

(i~~E.~4 JER WRPtS - 242-A Evaporator El Exhaust- Cotat 0 

Wrinlo, . nc. Ventilation SystemNo 406 

FACTORY ACCEPTANCE TEST PLAN Spec No. R~PsPEC36062 


7.29.3 PRESSURIZE system with compressed air to 23.7 inH 2O 

7.29.4 CONDUCT bubble leak test in accordance with PTI-TP-1.7 Rev 5 Bubble Leak Test 

Procedure (see Attachment 7.4). CKI/2 ell, 

7.29.5 CONFIRM the accepta nce, criterion has been met. 

.7.29,6 Test Director V7ERiFY test is complete. 




7.30 Sampler line Vacuium In~dicator -Fiunctional Test (Pb 1) 


BACKGROUND -this test is to verify *vacuum indicator reads on scale for the normal 

sample flow rate range of Oto 2 SCFM per RPP-SPEC-36062, Section 4.1.16. 

COMPON-ENT BEING TESTED: 

.pI1 

ACCE PTANCE CRITERIA - The vacuum indicator will indicate over the calibrated span 

Qf instrument, 0 to 20 in HG vacuum. 


7.3 0.1 REMOVE P1 fr-om cabinet 400. 

7.30.2 CONNECT calibrator. 


Equipment JModel # Seia 4 Date: De 

81 Premier Technology, Inc. 06765.0.000-FAT001- (Rev 6)

PREMIER TECHNOLOGY, INC. ProjctNo. 006765.0.000 

WRPS - 242-A Evaporator 1(1 Exhaust 

RVentilation System 

~O~g) ,AZ.RPP-SPEC-360 


Contract 

No. 

Spec Ne. 

40167 

RevO 0 

7.30.4 SET calibrator to 0 iig". 

7.30.5 RELEASE any residual pressure in Pl-I by lifting relief plug on top of gauge. 

7.3 0.6 RECORD P1I readout in table. 

7.30.7 INCREASE calibrator setting. 


Page A-42 

7.30.8 REPEAT steps 6.15.6 - 6.15.7 until a total of six reading are taken fom 0-19 inlig. 

FAT 7.30 Sampler Line Vacuum Indicator - Calibration Initials 

Test Cairtsin~g F5-1 Readout (In~g) %I Error Director Inspector 

2 ?- 2-0c -. 

S- . 

3 Lj.00 1.00 0 

4 - .0 q4 - .'?{ 

6 14 9!1o 05C( 

-7 1 '1. - q&voIO 1 *1 - > 

7.30.9 REMOVE calibrator. 

7 .30.10 COMFIRM relief plug is returned to "pluggred" position. 

7.30.11 REINSTALL PT1 into cabinet 400. 


7.30.13 Test Director V-ERIFY test is complete. 

24 





Date 

Date 

62 1 

006765.0.00-FAT-00I-1 (Rev 6)


Page A-43 

PRJEMIER TECHNOLOGY, INC. Project No. 006765.0.000 

- WRIS - 242-A Evaporator K] Exhaust Contract 407 

\wAchoogVenitilation1 System No. 406 

8. Comnpletion of FAT Test 

8.1 Finkal Sign-off 


8.1.1 CONFIRM all testing is complete for sections 6 and 7 

8.1.2 Test Director VE RIFY test is complete. 



9. Attachment List 

OA InspectornSigiature Date 



Attachment 3, FAT Test Log 

Attachment 6.1 Electric Drive Motor Vendor Data 

Attachment 6.2 Valve/Damper VendOr Data 

Attachment 6.3 Damper Manufacture Certification Documents 

Attachment 6.4 Damper Frame Leakage Documents 

Attachment 6.5 Filter Train Pressure Boundary Certification Documents 

Attachment 6. 10 AMC Factory Acceptance Test Procedure of 242-A Exhauster Sampling 

System 

Attachment 6.23 Volumne calculations 

Attachment 7.8 Exhaust Fan K(1-5-2 and Exhaust Train Flow Test (M inimurm System Loss) 

83 Premier Technology, Inc. 006765.0.OOO-FAT-00l-1 (Rev 6)

Attachment B 


Page B-i


Page B-2 

PREMIER TECHNOLOGY, 11C. Project No. 006765.0.000 

& M I R WRPS - 242-A Evaporator KI Exhaust Contract 40167 

Tehooyn.Ventilation System No. RPSE-66 

7 Procedure 





0 All gasket joints on the inlet plenum and expansion joint on the inlet of the filter 

trains 



* The leak rate shall not exceed 0.23 ft 3 per hour at a pressure of 23.7 inH 2O. 


6.23.1 VERIFY test results of PT! #6765 - Inlet Plenum Duct 






7.1 Valves/Dainer - Visual Ispections 


BACKGROUND - (ASME AG-l TA-35 10) a visual inspection is to be conducted to verify 


inspection is to be conducted prior to releasing the equipment for normnal operation. 

ASMIE AG-I TA-1-1200 DAMPER INSPECTION ITEMS: 

*housing and duct interface 

33 Premier Technology, Inc. 006765.0.000-FAT-001-l (Rev 5) 

Date


Page B-3 

PREAMER TECHNOLOGY, INC. Project No. 006765.0.000 

WRPS - 242-A Evaporator 1(1 Exhaust Contract 4017 

SV entlation S ste'm No. 01 

FACTORY ACCEPTANCE TEST PLAN Spec No. R0PSE366 

" actuator linkage, motor, and controller 

* interferences with moving Parts 

" damper shaft seal 

* blade edge seals and damper seat 

" limit switches 

* supports and attachments 

* bolting and fasteners 

* electrical connections 

* as-built configuration in accordance with design drawings 

* damper nameplate 

* provisions for access for performing tests and maintenance 


* KI-MOV-001 

* KI-MOV-002 

* Kl-BDD-001 

* Kl-BDD-002 

* Kl-DMPR-001 

* KI-DMPR-002 





7.1.1 VERIFY all inspection items listed in ASME AG-lTA-I- 1200 


FAT 7.1 ASME AG-i, TA-3510 Initials 

DmeLit Improperly Installed Physical :Daa,ge StlruuralDsrs Test QA 

Inspector 

I esirector 

Dampe LNs 

Kl-MOV-001 

KI-MOV-002 

KI-BDD-00 1 

Kl-BDD- 02C 


006765.O.O00-FAT-001-1 

e 


Kl-DMiPR-001 

KI-D1WR-00 2 XKC 

7.1.3 


Page B-4 

PREMIER TECHNOLOGY, INC. Project NO. o06765.0.000 

NWS - 242-A Evaporator K1 Exhaust 

Ventilation SystemNo 

Contract 40167 

6 0 62 

Rpp-spEC-3 

FACTORY ACCEPTANCE TEST PLAN SPec N. Rev 0 

Test Director VERIFY test is complete. 

Test'Director Signature 

/Date 

7.1.4 QA inspector VERIFY test is complete. 

QA inspector Signature 

'72 Valve/Dampers - Verify Isolation Valve positionl Indication and Functioni 

MATR-x REFERENCE - line 25 

BACKGROUD - Prior to the initial pressurizing of the damper control system, Pneumatic 

systems shall be checked for proper installation and leak-tightness. Dampers having remote 

position indicators shall be observed during operation to verify that the mechanical damper 

position corresponds to the remote indication. power-operated dampers shall be frully cycled 

using a control switch or other actuating device to verify operation. 


a KI-MOV-001 

a KI-MOV-00 2 

ACCEPTANCE CRITERIA- 

* ASME AG-i TA-424 4 Verify that the dampers indicator corresponds to the remote 

indication. fulcye 

* ASME AG-I TA-424 5 Damper must ul yl 

* ASME AG-1 TA-4246 Maximum time for any of the cycles shall be less than 20 

seconds. 

TEST PROCEDUE: 

7.2.1 

CONFIRMI indicator mark position matches actual damper position. 

35 Pemir nc. Tehn~O~, 

0 0 6 76 .0.00OFAT-0-1 

Dt 

- 



Page B-5 


tP E ~ E RPS - 242-A Evaporator K1 Exhaust Contract 406 

Ventilation SystemNo 406 

0022 




7.2.16 MEASURE the time for the damper to fully open or fully close. 



FAT 7.2 ASME AG-i, TA-4244, TA-4245 &TA-4246 Initials 

Remote indication 

matches damper Damper Fully cycles Test QA 

Damper List Cycle Time osio Director Inspector 

Kl-MOV-001 

Kl-MOV-002I 

Ys 





7.3 Filter Traini --. Visual Inspection 


N 

BACKGROUND - (ASME AG-l TA-3510) a visual inspection is to be conducted to verify 



Visual inspection is to be performed on the filter train, inlet, outlet, conmmon switching 


accordance with AG-i 


9 Filter Train A 

37 Premier Technology, Inc. 006765.0.OOO-FAT-0O1- (Rev 5) 

Date 

Date


Page B-6 




& TFACTORY ACCEPTANCE TEST PLAN Specr No. RPP-SPEC-36062 



Rev 0O 





7.3.1 VERIFY all inspection items listed, check box for if item is free of physical damage, 

structural distress or degradation that would impair the ability of the component or 


As-uil cnfstion itconem wilte desgnter 

drBi 

prvAo ccess forr perfrmin test andkets 

Srampler mdji fra, capo, and assI 

SupAortermdasrae and lms gasketntsIs 

Bolting and fasteners 

Pnsumisation calvects 

Eletia connectos 

HEPA fame setiaeld cntinuos 

TestneDirectoratches 

provisio nsfoacesorpeorntes a 

38 Premie rehnlogydi, Irac. aps and5..OOFT-O- (Revet) 

Tri


Page B-7 

I ~PREMIER TECHNOLOGY, INC. Project No. 006765.0.000 

wRPS - 242-A Evaporator KI Exhaust Contract 40167 

Ventilation System N. RPSE-66 

FACTORY ACCEPTANCE TEST PLAN SpecNo. Rev 0 

7.3.2 CONFIRM the acceptance criteria has been met for each Filter Train. 


TestDiarector Signature 

7.3.4 QA inspector VERIFY test is complete. 


7.4 242-4 Evaporator K1. Exhaust - Pressure Decay Test & Bubble Leak Test 

MATRIX REFERENCE - Line 23 

B3ACKGROUND - A pressure boundary leak test shall be conducted to verify leaktightness 

of the damper housing and interfaces with system in accordance with ASME AG-i1 

Section TA-3 523 and Mandatory Appendix TA-rn. (TA-3 523 -TA-ll- 100) SUMMARY 

OF METHOD Ducts and housings that form the pressure boundary of the system shall be 



small volumes and is conducted at the maximum operating pressure for the system The 


1 1/ times the maximum operating pressure, then allowing the pressure to decay for a fixed 


whichever occurs first. Fans, dampers, and other components that are part of the pressure 


connection leak tightness. If the measured leak rate is in excess of the acceptance criteria, 




* All gasket joints on the system 



Date 

Date 


*The leak rate shall not exceed 0. 1% of the system volume per hour at the system 

leak test pressure as defined in ASME AG-I for leakage Class I (Table SA-B-l 310) 

006765..000-FATO00ll (Rev 5)


Page B-8 

PREMIER TECHNOLOGY, INC. Project No. 006E765.0.000 

/~ A h ~WRS - 242-A Evaporator K1 Exhaust 


Contract No. 40167 0 

&T 


RPP-SPELC-36062 

Re 0 


7.4.1 INSTALL blanking plate between each Fan Assembly and Fan to Switching Plenum 

Expansion Joint. (location I & 4) See Figure 7.4 Test Locations 



Kl-HV-001 Inlet Plenum to Filter Train A Closed 

KI-HV-002 Inlet Plenum to Filter Train B Coe 

Kl-HV-003 Inlet Plenum to Filter Train C 

K1-H-010 A o SitchPlenm Filtr 

Closed 

Opn 

CA 

A 

K1-HV-010 Filter B To Switch Plenum Open 

Kl-HV-017 Filter B To Switch Plenum Open C 

K-EOV-024 PiletoFnIltonDmer lnmOpen) (Nrh (oSic 

KI-MOV-001 Plenum to Fan isolation Damper (South) (Open) 

7.4.3 INSTALL pressure relief device set at 25 inH 2 O 

7.4.4 PRESSURIZE system with compressed air to 1 1/ times Max Operating Pressure 

(23.7 inH2 O) 


Procedure. 




Page B-9 


/\Z~ iNA ER WRPS - 242-A Evaporator K1 Exhaust Contract 40167 

P E I RVentilation System No. 

FACTORY ACCEPTANCE TEST PLAN Spec No. .RPPSev 06 

10 

ii 13 

16 

4 5 L18J 20 

61 7 19 


7.4.6 VERIFY no bubble indications. are detected at locations shown if figure 7.4 Test 

Locations. 


Description 

Stsid Un- Test QA 

Location from To Stsidsatisfied Director hIspector 

I TEST PLATE KI-EJ-004e 

2 KI-EJ-004 Kl-MOV-001 

3 K-MOV-001 PLENUM x 6 

4 TEST PLATE KCI-EJ-00S 

5 Kl-EJ-005 Kl-MOV-002 

6 KI-MQV-0 PLENUM 

PLENUM END PLENUMl 

7 CAP> (SOUTH) SECTION 1C 

PLENUM 

PLENUM/ 

8 SEiO1 SETO2 


2 

PA 

21 

(4 

O 6765.O000FAT001-1 


PREMIER TECHNOLOGY, INC- Project No. 006765.0.000 


Page B-10 

W*RPS - 242-A Evaporator Ki Exhaulst Contract 40167 

toyPc 

Ventilation SystemNo 

), Y FACTORY ACCEPTANCE TEST PLAN Spec No. RPPSe 0 0 6 

FAT 7.4 ASME AG-i, TA-4233 & TA-4234 hitials 

Desritin atsfed Un- Test QA 

LocationiO satisfTo satisfied Director Inspector 

9 

PLENUM 

SECTION 2 

PLENUM 

SECTION 3 

& e 

10 

10 

PLENUM 

SECTION 3 

PLENUM 

SECTION 4of 

21 FLER ANM K--00 

22 KlFLTR001 N K-HV-00 

23 K-H-1 FILTER TRAIN iH-0 A 

18I, SECT/ONi 

6 

7.4.7 CONFIRM teapt11.6 ancrtea ae se cmet. ntiln tbe 

7.4.10 CODUC blankin pldeaytes In actrae lctions. -*5665Pesue ea 

7.4.11 TetDrcorrRF ~,x -r 

test Directore SintreDt 

esi opetehol 

7.4.12 QAs isector VERIFY test is complete. 

TestDiretor ignaureDate 


42 Premier Technolog~y, Inc. 

Dt 



/~r 'N/TERWS - 242-A Evaporator K1 Exhaust Contract 40167 

P I RVentilation System No. 

FACTORY ACCEPTANCE TEST PLAN SRec P.PC6 0 

7.5 Power I~nStrumnent and Control Cabling - Proper voltage and phase 

sequence at equipment served 


BACKGROUND - perform inspection during cable energizing. 


0 power Instrument and Control Cabling 


Page B-1i1 

ACCEPTANCE CRITERIA - Specified voltage (see table FAT 7.5) at equipment served 



7.5.1 

RECORD equipment and calibration infornmationl. 

Equimen Modl #Seril 

Equiment Mode~ 

#Calibration 

Seial#Date: 

0 141wc -C r' 3 14 


7.5.3 

Due 

MEASURE voltage on the Bus-side of the panel using a calibrated Volt Meter. 


NOTE: if the circuit is a GFCI press the test button and record proper functionl. 

7.5.4 VERIFY breaker is on. 

7.5.5 


MEASURE voltage at the receptacle/equipment. 

OO6 7 65 .0.000-FATOO1-1 

6 



7.5.6 

KI-MPZ00 

In- FACTORY ACCEPTANCE TEST PLAN Spec No. Rev 0 


Page B-1 2 

INITIAL each circuit as it is completed. 

Circi BreakerIV lage and Phase Sequence Verification 

initials 

Fael Crcit Eqipen GCIGFCI TEST Specified Measured Test QA 

Pael# Cicit Eqimet GF1 good/bad Voltage Voltage Dirmector Inspeco 

I K1-MOV- 00 1 NO 4- 110 VAC fjC 

KI.MPZ-0 5, KI-E-0 NO 

20VI- 

Kl 100 4 110 VAC 

O i 1 EATR1ACE YES 

Kl.MPZ-OM 12 SPARE NO /0 110 VAC 21 

7.5.7 

CONFERM the acceptance criteria have been met. 


'e'*' k____--.3 

7.5.9 


QAIsetrVRIFY test is complete. 


7.6 DamperS - Di=iPer Cycle Time and Operation 

19 

MATRIX REFERENCE-irne 

2 

Date 

BACKGROND -ASME AG-i DA-5 121 The damper or louver assembly, as applicable, 

shal becyced minmumof 0 tmesfrom the fll-open to the fullclosed position to 

verify the free operation of all parts and the correct adjustment, oiinn~adsaigo 

all blades. 

COMPOENS BEING TESTED* 

KI-BDD-001 

44 Premier Techolo~g, Inc. 

Dt 

00 6 7 65 .O.OOOFAT-001-1 (Rev 5)


Page B-1 3 



olg TcVentilation 

SystemNo 

FACTORY ACCEPTANCE TEST PLAN Spec No. RPP-SPEC-36062 

* Kl-BDD-002 

" Kl-DM!PR-001 

* Kl-DMPR-002 


* Verify free operation of all parts and the correct adjustment, positioning, and seating 

of all blades. 

* Maximum time for operation of any of the cycles shall be less than 20 seconds. 

* Movement of the blades and actuators and linkage shall be smooth and without 

hesitation. Local position indication operates as required. 


7.6.1 VERIFY each damper can be cycled 10 times 

7.6.2 CONFIRM cycle time is less than 20 seconds 

7.6.3 CONFIRM dampers operate without hesitation. 


Fat 7.6 ASME AG-i, TA-4244, TA-4245 &TA-4246 nitials 

Damper List Cycle Time 

Crt adutI t 

Position, and seatingDrco 

No 

Operates Smoothly 

Ye 

Test QA 

npco 

Kl-BDD-001 c 

C 

Yes x.5 

ki-DP-002 I'C7X. 

K1-DMPR-00, '7 X~ 



Date 


(4J' .A W 71cc ~ 


Date 

45 Premier Technolo--v. Inc. 

cj qj4I 

006765.O.OO0-FAT-001-1 (Rev 5)


Page B-14 


I ER WRPS - 242-A Evaporator K1 Exhaust Contract 406 

n Rg; Ventilation System 40167 ____ 

FACTORY ACCEPTANCE TEST PLAN Spec No. RP-Sev Q6 

7.7 KI.-5-2M Motor and VFD - Proper voltage at equipment served 

MATRIX REFERENCE - line 14,15,26,27 & 74 




" Kl-5-2M 

* Kl-5-2 VFD 




rating for the motor and VED. Breakers and other circuit protection devices function. 



EupetSerial # Calibration Due 

Equipment K3 A I Date: 

Vo kF-C'fr,- " -clir~ 1R ~ is~ I /l& I 

7.7.2 RECORD all initial VED settings in table FAT 7.7. 



Kl-HV-001 Inlet Plenum to Filter Train A Closed e 

KI-H{V-002 Inlet Plenum to Filter Train B Open C/( 

KI-HV-003 Inlet Plenum to Filter Train C Open C/c 

Kl-HV-010 F ilter A To Switch Plenum Closed 10( 

46 Premier Technology, Inc. 006765.O.OOO-FAT-OO1-1 (Rev 5)


Page B-1 5 


WRPS - 242-A Evaporator K1 Exhaust Co.ac 40161 

()~ech ologv~ nc Ventilation SystemNo 

RPPSPEC.62 


Kl-HV-017 Filter B To Switch Plenum Closed C/( 

Kl-HV-024 Filter C To Switch Plenum Closed c 

KI-MOV-001 Plenum to Fan isolation Damper (North) (Closed) C 

KI-MOV-002 Plenum to Fan Isolation Damper (South) A(Closed) CU 

KI-DMPR-001 Fan to Stack Isolation Damper (North) Open < 

Kl-DMPR-002 Fan to Stack Isolation Damper (South) Open C/ 


7.7.5 MEASURE voltage on the VFD Supply side and record value in table 


continuing. 

7.7.6 CONNECT amps meter to the Phase A of the K1 -5-2-M. 

7.7.7 SET the VFD speed to 10 Hz (17%) 



7.7.9 MEASURE voltage at terminal 22 to neutral of relays K1 -K-005 inside Kl -ENCL- 

300, there should be 120 VAC at this terminal. (If not, this could indicate that there is 

a high Radiation alarm or that the control circuit fuse is blown resolve issue as 

needed.) 

7.7.10 MEASURE voltage at terminal 21 to neutral of relays Kl -K-005 inside KI-ENCL- 


fan K 1 -5 -3 interlock. 

7.7.11 MEASURE resistance between terminals 7 ant 8 on TB36 in Kl -ENCL-300 (should 

be > 1 00k.Q) Note: this checks initial condition for supply fan interlock relay K1 -5-1 

7.7.12 OPEN the K1-EIV-017 and K1-HV-024 dampers to 10% 

7.7.13 START the motor and record the peak amperage as the motor winds up (should be 

less than 6X Name plate FLA rating). Note that the KI -K-005 Relay changed stats. 

7.7.14 VERIFY KI -MOV-001I is open. 




Page B-16 

PREMjIER TECHINOLOGY, INC. ProjectNo. 006765.0.000 

WRMPS - 242-,A Evaporator 1(1 Exhaust Contract 40167 

P M E Ventilation System No. 

& nc. -Tflchnoogy, 

pp-SPIEC-36062 


7.7.15 MEASURE voltage at terminal 2Zto neutral of relays Kl-K-005 inside K1-ENCL- 



7.7.16 mASURE resistance between terminals 7 ant 8 on TB6 in Kl -ENCL-300 (should 

be 0 M~) Note: this verifies that the fan interlock relay Kl -5-1 is working properly. 

-\7.7.17 RECORD the amps on all three phases once the motor has come to steady-state 

operation. 

7.7.18 INCREASE the VFD set point to 60 Hz 

7.7.19 VERIFY that the amp distribution across all phases is withbin 2% of each other. 

7.7.20 OPEN slowly the K1-HV-017 and K1-HV-024 to 50% 


operation. 

7.7.22 OPEN slowly the K1-HV-017 and K1-IIV-024 to 100% 


operation. 

Fat 7.7 VFD Output FLA Kl-5-2 Initials 

Voltage Fan voltage Fan Test QA 

RlyTerminal 

ed Rssnnn Director Inspector 

RaySto 

KI-K-005 21 110 C) 

Kl-K-005- 22 Z 0 

Resistance Check 

vEDF Hz (10(1%) 

OHMS OMS Initials 

Damer Vot A-%PDamer I h Damper @ 100% TestiA 

PhA Ph-ts H -C P-zh 

P - Ph-A Ph-B Ph-C D rco n p co 

sa .4J 

.iY 5 ?q1 1f 62g 

am s amS amps amps ams sinms ama sams am 


@6 

O06765..000-FAT-001-1 (Rev 5)



Page B-17 

WE7PS - 242-A Evaporator Ki Exh'aust Contract 40167 

\±~~jio~oy; i~Ventilation 

System 

No. 

FACTORY ACCEPTANCE TEST PLAN Spec No. RPPSev 30 6 

7ni7.27 RECOD alfinl VF settings.etinc 

P ARe -I _ R1I 

Tes Dieco Sinaur 

7..3 QA Inp x Cto I Y test is coplte 

Datet 

I ~~ I .. Re C/I P 

Fnpco QA iGntr Date 

T. K~% TaI GdMtr-Va~iYs 

MATDG REEENE-lie847&4 

(~ilUnSsel 

4 Prme b ehfOOV nc O 7 5O.0FTOb Rv5 

o


Page B-1 8 







7.11. 10 REMOVE temporary power from terminals 13 and 14 on TB-6. 





7.12 VKbS-3M Motor and V.FD - Proper voltage at equipment Served 

MATRIXK REFERENCE - line 14,15,26, 27 & 74 




0Kl-5-3 Fan and VFD 




rating for the motor and VFD. Breakers and other circuit protection devices function. 




V +I~i&,'~ 4~ S~ _____Date1. 

57 Premier Technology, Inc. 006765.0.O00-FAT-0O1-1 (Rev 5)

., EIRNo 

,rVentilation 


Page B-19 



SystemNo 

FACTORY ACCEPTANCE TEST PLAN SpecNo' RPPPE-30 6 

7.12.2 RECORD initial VED settings in table FAT 7.12 



KI-H-001 Inlet Plenum to Filter Train A Open 

KI-HV-002 Inlet Plenum to Filter Train B Open C 

K1-HV-003 Inlet Plenum to Filter Train C Closed ( 

K1-HV- 10 Filter A To Switch Plenum Closed C( 

KI-HV-017 Filter B To Switch Plenum Closed 

Kl-HV-024 Filter C To Switch Plenum Closed ( 

KI-MOV-001 Plenum to Fan Isolation Damper (North) (Closed) / 

Kl-MOV-002 Plenum to Fan Isolation Damper (South) (Closed) ( 


Kl-DMPR-002 Fan to Stack Isolation Damper (South) Open r(4" 

7.12.4 VERFY power to both VD's is on. 

7.12.5 MEASURE voltage on the VFD Supply side and record value in table 


continuing. 

7.12.6 CONNECT amp meter to Phase A of the K1 -5-3-M. 

7.12.7 SET the VFD speed to 10 Hz (17%) 



7.12.9 MEASURE voltage at terminal 22 to neutral of relays K1 -K-006 inside K1 -ENCL- 

300, there should be 120 VAC at this terminal. (If riot, this could indicate that there is 

a high Radiation alarm or that the control circuit fuse is blown resolve issue as 

needed.)


WRpS - 242-A Evaporator 1( xast Contract 40167 

\/' e C noog A! . Ventilation System 

FACT ORY ACCEPTANCE TEST PLAN Spec No. Rev 0 


Page B-20 

RpSE-66 

7.12.10 MEASURE voltage at terminal 21 to neutral of relays K1 -K-00 6 inside Kl -ENCL- 


fan K1l-5 -2 interlock. 

7.12.11 MEASURE resistance between terminals 23 ant 24 on '[36 in Kl1-ENCL-3 

(should be> 1 00K?2) Note: this checks initial condition for supply fan interlock relay 

Kl-5-1 

7.12.12 OPEN the Ki-I-O01 and KI-IW-017 dampers to 10% 

7.12.13 START the motor and record the peak amperage as the motor winds UP (should be 

less tan 6X Name plate FLA rating). Note that the K1-K-006 Relay changed states. 

7.12.14 VERIFY KI-MOVO00 2 is open LK~ ll sK K06isd I-NL 

7.12.15 MEASURE voltage at terminal 21'to neutral of relays I--0 nieK-NL 



7.12.16 MEASURE resistance between terminals 23 ant 24 on TB6 in K1-ENGL- 

(should be 0 k Q) Note: this test is to verify supply fan interlock for KI -5-1 is 

working properly. 


operation. 

7.12.18 INCREASE the VIFD set point to 60 Hz 

7.12.19 VERIFY that the amnp distribution across all phases is within 2% of each other. 

7.12.20 OPEN slowly the K1-lIV-010 and KI-HV-01 7 to 50% 


operation. 

7.12.22 OPEN slowly the K1-IFV-010 and K1-HV-017 to 100% 


operation. 


0 0 

3 0 0 

0 0 6 7 6 5.0.000FAT-0I 1 (Rev 5)

PREMIER TECHNOLOGY, INC- Project No. 006165.0.000 

/~~2N~ fJ{ WRPS - 242-A Evaporator K1 Exhaust .zontract 40167 

Ventilation System. No. ppc-62 


Page B-21 

FACTORY ACCEPTANCE TEST PLAN Spec No. RPPSev -6 

Fa 712vFD output FLA KI-5-2~ ^ Initials 

Relay 

Temial 

Temnlt9 

voltage Fan IVoltage Fan 

ed Runnin 

T est 

Dirctor 

Q 

in ector 

21 

0 

KI-K-006 

K1-K-006 22 1 0 : Ck 

Resistance check 

Resistance between ternuinals 23 and 24 0 . 

Name Plate Data 

FLA Volts Hz 

Daprs12.2 

OHMS OHMS initials 

VFD @ 10 Hz (17%) 

E:D-P: 

0 

IN Volts A-Phase Inrush Dmes@0% Direc~ npco 

Ph -A Ph-B Ph-C 

a ms a 

DEO tmpra a po e from termnal 13- an 1 o T - 

7.12.27~ina fSnlttinsttigs ECOR 

i. itial CON tII tne acetncFrtriLaebenm t 

60~ Prme ecoogy In. 0 6 7 5000FT0 1 Rv 

6

7.12.29 TestOLGY Dircto VERIFYt test is6complete. 

7.23 QA setrVR FY tes is2- cvaoplto1E. hut Cnrc 06 

7A 153 n Mtr-Vniration Sst~m irumSse Lo) 

MARXR FAECEOR ACETAC 8LN TEne ISe o e 

TACKROUDire rior ttakigtevbainaueets D tefashllboprtdt 

the.3 norAl opeatgspeed RFor atru in copeoftimeni.hebaigeahasal 

eQuiiru tepeatre atwicionteepature noaoner ie -- vr1 


Page B-22 

KT5- minutes s test Mto isd dtrmn t vibration ofsth fain nd mor uneSiuystemLos 


prior to the Fan Performance/Airflow Capacity test. ASME AG-i TA-3533 - Vibration 



When the bearing housing is not accessible the frame of the component may be used if it 


COMPONENTS BEIN G TESTED: 

0 Kl-5-3 Fan and Motor 


* Vibration: Measured in all three planes. The criteria for low horsepower, industrial 

process or petrochemnical applications, Fan Application Category AIVCA 204 BV-3, 



7.13.1 CONFIRM new clean filters are installed in filter housings A, B, and C. 


~i ~ ~ ~006765 ,0.000-FAT-001-I (Rev 5)

FMIER 

T,. 


Page B-23 


WRS - 242-A Evaporator K1 Exhaust 


Technk)VInc.RPP-SPEC-36062 

Contract 

o 

40167 

IFACTORY ACCEPTANCE TEST PLAN Spec No. Rev 0 

7.17.3 MEASURE the differential pressure between PDIT location KI-PDIT-314 


7.17.4 RECORD PDIT to Stack differential pressure inH 2O 

7.17.5 RECORD motor input frequency, differential pressure at PD1T location K1-PDIT- 

306, differential pressure at PDIT location K1 -PDIT-309, flow at, stack sampling, 






7.17.9 REMOVE temporary power from terminals 13 and 14 onTB-6. 



7.17.11 QA Inspector VERIEFY test is complete. 


7.18 Filter Train A - Airflow Distibution (Full System) 

Date 

Date 

MATRIX REFERENCE - line 42 AOIJ q",/j ( ' iI / 


pre-filter, and HIEPA filter banks. Acceptance tests shall be conducted with pre-filter and 

ITEPA filter banks installed. (ASME AG-l TA-4632 Airflow Distribution Test) With the 

system operating at design flow rate (18,000 scfm; 19,500 max) the airflow distribution shall 

be measured downstream of each pre-filter, and IfEPA filter bank. 



* inlet 

* Outlet 

S,-,v. ~nnr7rt hI Ofin-VAT-n(f11-1 (Rev


Page B-24 


WRPS - 242-A Evaporator K1 Exhaust Contrac 

Ventilation System N o. 406 

FACTORY ACCEPTAN4CE TEST PLAN Spec No. Rev 0 


" Isolation valves 


" Flexible metal connector 

* Ductwork 

Sp 


ACCEPTANCE CRITERIA -Velocity measurements across the HiEPA filter banks shall 




Valve/Damper Description Position I nitials 

KI-HEV-001 Inlet Plenum to Filter Train A Closed 

Kl-HV-002 Inlet Plenum to Filter Train B Closed 

Kl-HV-003 Inlet Plenum to Filter Train C ClIosed 

KI-H-010 Filter A To Switch Plenum Open C K 

Kl-HV-017 Filter B To Switch Plenum Open 11 

KI-HV-024 Filter C To Switch Plenum Closed %fr 

K1-MO4V-001 Plenum to Fan Isolation Damper (North) (Closed) ~ K 

KI-MOV-002 Plenum to Fan Isolation Damper (South) (Closed) K 

KI-DMPR-001 Fan to Stack Isolation Damper (North) Open ( 

KI-DMPR-002 Fan to Stack Isolation Damper (South) Oe 

7.18.2 VERIFY power to the VED is on. 

7.18.3 CONSULT and IMPLEATENT any additional safety precautions as required by 


7.18.4 SET the VFD speed to the required Hz to achieve 18,000 scfmn+10% (use 

Attachment 7.18 information) 



7.18.6 OPEN KI -11V-001 and KI-HIV-002 

6ig Premier Tech nologv. Inc. 006765..000-FAT-01-l (Rev 5)

7.18.7 START Kl-5-3 fan 


Page B-25 

PREMIER TECHNOLOGY, INC. Project No. 006765.0-000 

WVRPS - 242-A Evaporator K1 Exhaust Contract 40167 



7.18.8 RUN NUCOM procedure 12-101 rev 7 (Attachment 7.18) 




/J 

Date 

7.18.11 QA Inpecto7 VRIFY test is complete. 

- Ak / 


Date 

SCC' 1-(S4 

00Cdh1 

7.18.12 CONTINUE to 7.19 Filter Train B - Airflow Distribution (Full System) 

7.19 Filter Train B - Airflow Distribution (Full System) 

O2~c 3/22i/ 5c frs exer( Ck)}/ 2/11 

MATRIX REFERENCE - line 42 A&D , ji4it 


pre-filter and IJEPA filter banks. Acceptance tests shall be conducted with clean pre-filter 

and HEPA filter banks installed. (ASME AG- I TA-4632 Airflow Distribution Test) With 

the system operating at design flow rate (18,000 cfm; 19,500 max), the airflow distribution 

shall be measured downstream of each pre-filter, and HEPA filter bank. 

COMP'ONENTS BEING TESTED: 

*Filter Train 

* Inlet 

* Outlet 


* Isolation valves 


* Flexible metal connector 

* Ductwork 

ACCEPTANCE CRITERIA - Velocity measurements across the ITEPA filter banks shall 


No.

F 


Page B-26 


(~ Ei il R WRPS - 242-A Evaporator K1 Exhaust Contract 40167 

olg; fC Ventilation System No. 

V RPP-SPEC-36062 



7.19.1 RUN NUCON procedure 12-101 rev 7 (Attachment 7.18) 

7.19.2 CONFIRM the acceptance criterion has been met for each damper. 



7.19.4 QAins tector VERITY test is complete. 

Date 

7.19.5 ~AInspector Signature Date 

!rce'A crm dO2 6.CkAt3/I t'i lz~ff XCA('f"' 6o . 

7.19.6 CONTINUE to 7.20 ilter Train C - Airflow Distribution (Full System)21 

7.20 Filter Train C - Airflow Distribution (Full System) 

MATRIX REFERENCE - line 42 AM) -V 143-- 1 I. 


pre-filter and HLEPA filter banks. Acceptance tests shall be conducted with clean pre-filter 

and HEPA filter banks installed. (ASME AG-i TA-4632 Airflow Distribution Test) With 

the system operating at design flow rate (18,000 cfin; 19,500 max), the airflow distribution 

shall be measured downstream of each pre-filter, and HEPA filter bank. 



* inlet 

* outlet 


* Isolation valves 


* Flexible metal connector 

* Ductwork 

ACCEPTANCE CRITERIA - Velocity measurements across the HEPA filter banks shall 


'71 Vr-mipr Technonnv. Inc. 006765.0.000-FATOOI4- (Rev 5)


Page B-27 



P/T E MhIokg.J Ventilation System No. 417 

& ,fne h n ol g -y, h 

ic .R PP-SPE C -36062 



7.20.1 OPEN K1-HV-003 and K1-H{V-024 

7.20.2 CLOSE Kl-HV-001 and Kl-HV-010 

7.20.3 RUN NIJCOM procedure 1 2-101 rev 7 (Attachment 7.18) 

7.20.4 CONFMIR the acceptance criterion has been met for each damper. 


R _ 

l Ir 1 1 


7.20.6 Q IneorVERIFY test is complete. 


tSJ 1 Ce(fST'1 602 .Ch'31 ol t,5, Scc ks CI1' o 1(22/I/ 

Sccf + 

7.20.7 CONTINUE to 7.21 Stack samp] ig ocation - Angular or Cyclonic flow 

7.21. Stack Sampling location - Aug I rCyclonic -flow ' 

MATRIX REFERENCE-Iline 56Z FID2. r0i; 76(1~c 

BACKGROUND - This test is to show the angular or cyclonic flow at the stack sampling 

location. An appropriate method for determining if a proposed location meets this criterion 

is described in 40 CFR 60, Appendix A, Method 1, Section 2.4.' 

2.4 Verification of Absence of Cyclonic Flow. In most stationary sources, the direction of 

stack gas flow is essentially parallel to the stack walls. However, cyclonic flow may exist (1) 

after such devices as cyclones and inertial demnisters following venture scrubbers, or (2) in 

stacks having tangential inlets or other duct configurations which tend to induce swirling; in 

these instances, the presence or absence of cyclonic flow at the sampling location must be 

determined. The following techniques are acceptable for this determination. Level and zero 

the manometer. Connect a Type S pitot tube to the manometer. Position the Type S pitot 

tube at each traverse point, in succession, so that the planes of the face openings of the pitot 

tube are perpendicular to the stack cross-sectional plane; when the Type S pitot tube is in 

this position, it is at "0 deg. reference." Note the differential pressure (DELTAp) reading at 

each traverse point. If a null (zero) pitot reading is obtained at 0 deg. reference at a given 

traverse point, an acceptable flow condition exists at that point. If the pitot reading is not 

72 Premier Technolozy, Inc. 006765.0.O00-FAT-001-1 (Rev 5)

17' 


Page B-28 



,lory ~ Ventilation SystemNo 




zero at 0 deg. reference, rotate the pitot tube (up to + /-90 deg. yaw angle), until a null 

reading is obtained. Carefully determine and record the value of the rotation angle (alpha) to 

the nearest degree. After the null technique has been applied at each traverse point, calculate 

the average of the absolute values of alpha: assign alpha values of 0 degrees to those points 

for which no rotation was required, and include these in the overall average. If the average 

value of alpha is greater than 20 degrees, the overall flow condition in the stack is 

unacceptable and alternative methodology, subject to the approval of the Administrator, 

must be used to perform accurate sample and velocity traverses. 

COMPONENTS BEIN4G TESTED: 

a Stack Sampling System 

ACCEPTANCE CRITERIA - The average flow angle shall not exceed 200 relative to the 

longitudinal axis of the stack. Tracer gas coefficient of variation (COV) shall be less than or 

equal to 20% across an area that encompasses at least the center two-thirds of the crosssectional 

area of the stack. The COV of stack gas velocity shall be with + 20% across the 




concentration COY shall not exceed 20% over the center region of the stack that 


2 2' 

7.21.1 MEASURE the pressure at each point using an S Type pitot tube. 

7.21.2 RECORD pressure and yaw angle. 

m'flO76z;fi_00lFAT_01_1 

0 

(Rev I;)


pXEMTR TECHNOLOGY, INC. Project No. o06765.0.000 


Page B-29 

WRIS - 242-A Evaporator Ki Exhaust Contract 40167 

1or .Ventilation n 

System N . R PS E 66 


Angular or Cyclonlic flow 

initials 

Test QA 

MesuemntUn- 

MesuemntSatisfied satisfied Director inspector 

Location Pressure Yaw An le 

2 

3ihs 

Loes 

Avrg5 

7.13CN6Mteacpac rtro a enmt 

7.14CNIEto72Stcsapiglcto-CntniatnCocnrtoan 

TeDDre tor Sn ar aife aife et I co 

QAslt 

7.2. CONEt 2 Stack San'MiP 

Velcit Proile 

7.2A5TRIt DreFtrERICE 

74~ Prmer~~ni;y:;z 

~ esrc~ 

lingiO1 lotatna 

tes line cop7te 

DnsectrcSgnaur 

- Cotmntion Conetatonand 

0 6 6 .D00AT01(Rv5


Page B-30 


WVipS - 242-A Evaporator K1 Exhaust Contract 40167 

I . RVentilation SystemNo 

BACKGROUND -This 

0 6 

FACTORY ACCEPTANCE TEST PLAN Spec No. RPSev 6 

test is to show the velocity and concentration profiles o 

Concentration of 10 + 1 Rim AD tracer aerosol (e.g. helium, sulfur hexafluoride) at the stack 

sampling location. 


0 Stack Sampling System 

ACCEPTANCE CRITERIA _ Tracer gas coefficient of variation (COY) shall be less than 

or equal to 20% across an area that encompasses at least the center two-thirds of the crosssectional 

area of the stack. The COY of stack gas velocity shall be with + 20% across the 




concentration COY shall not exceed 20% over the center region of the stack that 



7.22.1 INJECT tracer gas after ITEPA filters in Filter Train C. 

7.22.2 MEASURE concentration of tracer gas at each location. 

7.22.3 RECORD concentration ofptactical. 

1.~~ 

r~nA,7(I 0f0iAT-001-1 CW~ov


Page B-31 

PREMIER TECHNOLOGY, INC. Project No. 00676.00 

e 

WVRPS - 242-A Evaporator K0 Exhaust 

RVentilat-ion I 

Cnrc 06 

SystemNo 

& T c-mloyIn. FACTORY ACCEPTANCE TEST PLAN Spec No. Rev 

K2/iIiil 


1Wia yuscfuv 

Mesre aisid Un- Test QA 

Location fieta tton, Stsfe satisfied Director Inspector 

Re2 t 

Avrg 

2aaSm ayStsfeaife7irco 

n co 

7.4 VRF httae a aito sls hn2%ars h rao h tc 

7.5 CNIMteacpac rtro aenmt 

7.6 SO oo n lo tt oetet 

7.2. 

EOEtmoaypwrfo 

7.8 TetDietr2EY et scmpee 

9/ 

emnl 3ad1 nTB6 

QAI inpe t Sgnare aife - TQ 

AveageI 

76~~~~~~~~~ ehooy n.O66..OFTO- 0rme 

X 4d ~ ,tC#- 

Rv5

Equipment for 7.22 

Equipment Model # Serial # Dte 



Page B-32 

73-~' N6-sI F--/_Ooo-HLn e

,12 

RPP.RPT-49670 Rev 0 

Page B-33 

PrMIER TECHNOLOGY, INC- Project No. 006765.0.000 

W 7 -22AEaporator 1(1 Exhaust Contract 40161 

emNo. 

Venilaio System 

& -technoogy Inc Syt , ESTRPP-SPEC-3 


pVentilation 

logyE 

FAT 7.22 4~~An yzzac lo Initials 

Location 

3vrg 

Measured Stsid Un- Test QA 

Concenratio 

satisfied Director inspector 

DaaSmayDretr 

7.4 VRF httae a aito sls n2%ars h rao h tc 

7.5 C 2-IMte cetne rtroha enmt 

7.6 STO moo6n llwi ocoetet 

7.7 REOV teprr0 oe3fo emnl 3 n 4o B 

7.21 Q Inpco IFYtss opee 

QA InspetorcSorntarepDat 

7.2. VRIthat tae a aito sls hn2%ars h rao htc 

7.22.5 ~ th ~ acetac ~ crteio4hs CONIR ~ (~ eeamt 

Isc 

60 6 2

Equipment for 7.22 

Equipment Model #Serial #Date: 


C, '9 3/of 0747 250/ 

kh~b"~ ~ 

cK~33/( 


Page B-34

) 

Test~ 


(This pape may be reproduced as necessey) 

nme:Tst 

ete exception number~ 

Description: b0 r-,t d-c.4ff 

61W-ao 

(oflM- Jt>4 F'l~ rl ' -3 -- 

Director 

aeTest 


Page C-2 

cit 

~ / ir~ -- 7 rsf 

DateEnie


(Mhs page may be reproduced as necessary) 

Te~pl1~~T) j'~ Z.0 Testexepfhio1Iube* ova 

Descriptfin -TC l1?( ~ -~ o 0 

efebk2I4 32 Cns 

921 

" ,A 

oiiato4 Tet ircor D 

RM ~ t su 


Page C-3


(This page may be reproduced as necessary) 

Tes se~ ume. Test exep,~ number c103ts~ 

DTescription: 

OrgntrTest 

Director 

32q11 


Page C-4 

Holdon fo eslton Ts. 

Retes Required46 

~Dt 

Dnesrip etion a cp ed Fiareoltonacepe 

fDate 

estie~ Dt nmeef' Date 

Qu tyAssur cDt 

alAsr"Date


(This pagre may be reproduced as necessary) 

Test step number: 7 /If 7AC 7 20 Test exception number:06 

Des cription: Al 

-~-P 

I(rc- 1/a kicd disbj-0 


Page C-5 

Lam' 55,&4% & /K 

(~~~ I-Hld for Resolution: nuet 

_____,_14f73L2- 

Originator Date Test Director Date 

Description- A- ASw4rV& P1%L-X 0 

Test~~~ DiecorDae 

Dnerip etion acpe:Fnlreouinacpe 

Tsiretr4ginee 

Ineimrslto cetd 

DateDate 

r~gi~ 

Date 

ialrslto cetd 

at 

iL

ITEM: 

Oty. Rejected: 3 sets 

Re 11-168Date: 

rtNO.: 

Flanders pr-filters 

Contract, Code/Standard or Specification Violated: 

systems Factory Acceptance Test Rev 5. 

Technology, Inc. a2.' 

32401 

Job No.: 66 


Page C-6 

Serial No.l Filter Housing A,' FitrHusing B, Filter Housing C 

FAT test 242-A Evaporator KI Exhaust Ventilation 

Desciptin ofNoncnfority: Sections 7.18, 7.19, and 7.2 ofu th state F requires that a distribution 

tesrbetdon tonsur eoity:rs each of the filters is limited to 20% of the average. When testing the pre-filters It was 

discovered that they did not meet this requirement. See attached reports.- 

Ientified By: Caleb Killian 

Cause: 

Flanders design of the transition. 

Date: 312411 

01

FT-1 6 (Rev. 5. 11105) - Date: z. 

NUCON Internationa,,Inc. Project g 

Z[AIRFLOW CAPACITY AND i OR DISTRIBuTION TEST REPORT 

client/I Plant: ~ 


Page C-7 

Unit: Ox Q s-s' C 7 -IT reL Test No:____ 

Test Type: Capacity_____ and/or. Distribution____ 

Test Location: Duct 7< or Filter Face______ 

CAPACITY DISTRIBUTION 

Flow Rats: Face Velocity 

Specfie IS ooo -!:-d1 MCFM, ACFM, o SCF Total ki-2-e-2- FPM: 

Speciied one) SJFAverage Lt1-. .5-- FPM 

Measured [ -4itg MCFM, ACFM, o CF Obtained Readings 

(circle on) Ma~dmum I L-1- FPM 

%of~sl~n~z.%Minimum - 4-2-4 FPM 

ofgh Design 

Mesue 

of DI Dsign xOOHDeviation from Average., 

____ ___ ____ ____ ___ ____ ___Low- - iq % 

Fan Stability Check. __~ ((crn-~ 

____Unsat. (-~n tpaKkX1m] 

Acceptance Criteria Met? 'Yes 'No 

tpIComments: 15-.1. J.C. 

Test Personnel Signature(s): NUCON International, Inc, 

Client Review

5T.21 (Rev, 3 11105) 

NUCON Internatioali Inc. 

S client 1 Plant 

1 nstrument(s) ID: 

RAW DATA GRID 


Page C-8 

Dt:z.. i T 

Prolect- 

Bank IdentifitatiOM 

Type of Test Airflow Capa d~ wiltle sa pi g - - t e , - 

Notes I comments: 

Airflow DjstbtibUf.& Air/Aeosol 

A 

4~ %igh + 

%/Lovv- 

~ Pcr~fflf~ 1 s ,rnfRtur(s); NUCON International, Inc- 

"Test__________________________ 

Velocity or ConCentration 

(d4rte one) 

DealO30ro Average 

-'w ~ 

OIoflwcpct 

T

FT-IS6 (Rev. 5, 11/05) Date: 7~- c, 

PN NUCON Iriternationcd, Inc. Project -ljf &.- L 

[-LOW A CAPACITY AND I OR DISTRIBUTION TEST RPR 


Page C-9 

client IPlant: _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 

Unit: C-KIA bl-4z C--t- t3 Test No: ___ 

Test Type: Capacity___ and/or Distribution_______ 

Test Location-. Duct____ or Filter Face___________ 

Flow Rt:Face 

CAPACITYDISTRIBUTION 

Velocity 

Specified MOFM ACE or SCFM 

Total ~Is--- 

Average_~.( 

-FPM 

FPM 

- Measured ~ ' FM, ACEM, or SCFMObiedRaig 

(droe one) Maximum I~d FPM 

%of Deign_ %Minimum -7- FPM 

Deviation from Average: 

%of~s~gn xiO IHigh + %*- 

LOW- -5-~ % 

fan Stability Check: Sat Mcn.-o1r1 

U-Jnsat oan 

Acceptanice Criteria Met? ____Yes V-'No 

* Notes I Commentst se " hA ~e- 

Test Personnel Signature(s): NUCON International, Inc. 


FT-21 (Rev. 3 11105) 

NUCON lnternctiof l Inc. 

Client I Plant\_*& 

Uni ''p - 5 

RAW DATA GRID 

~Test 

Poet 

Poet 

iTa- 


Page C-10 

NO '.- 

"S_~~ 

Bank Identification: 

T ofT p t: AirfloW CapaiY Multiple Sa plin -- - ot e 

T Of"et p 

Airflow DIsa fy -n -6; AirIAero sol Distributionl~- ~ t e . . 

r.. 

Average 

(drcie onea) 

~ 

%/Deviatiofl from Average 

+ l2S f 

~-%High %Low 

iirZ 1 ~~a~j.. 

-_____ 

a.Devion~f 

jK~)-comsonent Area 

CoP 

~~~~~=t ~~~ ~ ~ FniiUe(t ~ *o of~~ff~ 

UO lttltsfaiIc 

-

FT-1 6(Rev.5, 11/V05) Date, ---. -- 


Page C-1 1 

NUCON Internationotl, Inc. Project: c;ic* 

E~ AIRFLOW CAPACITY AND!I OR DISTRIBUTION TEST REPOR 

~Client/Plant: 

Unit" Test No, ____ 

Test Type: Capacity________ and/or Distribution____ 

Test Location: Duct___ or Filter Face_______ 

CAPACITY 

DISTRIBUTION 

Total LL q t- FPM 

Spectfled ______MFM, ACF SCFM Average 4R 7 FPM 

(circle one) 

Measured _______ M, ACFM, orSCFMObiedRans 

I aid one) Maximum i3'.3 FPM 

% of Design- 

Minimum -~= FPM 

Deviation from Average:. 

%fDsg=Measured X10High + (-;-I 

Design Low- .f. % 

Fan Stability Check- ___sat. /V~c=(xrn-v 

___Unsat. 

,, 

'Acceptance Criteria Met? ___Ys X: No 

Notes I Comments: "(JtCc '-& 

t c 

Test Personnel Signature(s): NUCON international, ]nc. 

Client Review 

.c..

F=T-21 (Rev. 3 11105)Daz-.'--Tme.- 

NCNItroiniInc. 

clen ln 

I 

Project 


Page C-12 

Clien a~ lantTest No:..t_ 

unit i' 11E. TE 

Bank identification:. 

~ 

Ty eo t Alirflow Capacity* Multiple Sa pi g - Oh r - 

Tirpl Ofst 

Aet ir/Aerosol Dist-lbutio fl...O he- 

Li i3~'? ~,obtained ~ 

-r-. P~rmr'nn~ 

te-e 

'1 

Commneflts 

; 1n~tUre(s)* WucON International. Inc. 

Readings 

%Deviatiof rom Average 

~~%H + .12LAZ- 

%Low 

of 

-A(g. w1


Page C-1 3 

1. Submmtal No. 

Washington River Protection 

SUPPLIER SUBMITTAL406NASB29 

9 

4 l7N~U0 

Solutions LLC (WRPS) 

2. To3. From 

z.aTon lr Paul M~cBride (PTI) 

4 .h r o c ne l a r k 

9 . D a t e 

04/04/2011 

242A Evaporator KI Exhaust Ventilat .ion System 

5PON.6. Project No. 7. Ton Farm/Tank No. .Aallg.No. 18. Review Distibutionl 

N/A 

242A Evaporator VT Donigan, R.3-26 

NITIP52 

- TFP ENG Review 

40167, Release NA Premier Technology, Inc.REle,125 -HVAC SME Revie;W 

'12.j Pre-Pturchass Evaluation Approval Data ~IIV1 information/Record TO Kaiser, S5-08 

- 

13. Paragraph 14.. Section 16. SOW/specffiC~If 

Sys Eng Review 

5.9.3 RPP-SPEC-360 6 2 WL Adams, R3-26 

-QA Revi ew 

17, Special Instructions: 

Resubml R Additfional Info. . Substitution 

19. Submittal propoaes DeviationsC from contract documents? LJ Yeas No 

20. Z Approved Not Approved [] Approved with Comments 10 Resubmit El lnfofrnatiofl/Record. 

21. Comments: 

WRPS concurs iwith the proposed use-as-is' disposition 'with the following justification 

discussion: 

In order to test airflow distribution across the pre-filters, Premier contracted NUCON who 

implements a cover over the access ports which provide access to the air space for taking 

velocity measurements. Because of the lack of clearance around the pre-filters, this method 

did not allow the velocity measurement readings to be taken with the pre-filterS installed. 

Therefore, the velocities were measured without the pre-filters installed at the estimated 

center point of each vacant filter space. it is these readinga. that did not fall. within the 

acceptabl 'e 20% range. These readings that did not meet the acceptance criteria can be 

accepted for 'the following. reasons: 

1.) Because the pre-filters were not installed-during testing, no resistance was present in 

the'air space that would have assisted in the function of equally distributing the inlet air 

to the 9 vacant spaces in each housing unit. 

.2.) The inlet Air was introduced through a 36" diameter opening exposed to wind and 

turbulence. Actual facility conditions will not be subject to such a condition. 

3.) The center point location of the pre-filters was an estimate only., 

4. ) The ist and 2nd Stage HEPA filter banks were tested with the pre-f ilters installed and 

both passed the distribution test and met the acceptance criteria. 

Page I of 2 

A-6003-219 (REVI 2)

1Sumta] No. 


Page C-14 

Washington River Protection SUPPLIER SUBMITTAL (continued) 4 01671- NA - S;4 o~ C4 

Solutions, LL-C (WRPS) 

22. Changes Required to Contract Documents? Yes Z No 7 : 2:DTt 

23. Signa~e2.Dt 

Page 2of 2 

A-500321D(REV 2)

SUPPLIER SUBMITTAL 

1. Submittal NO. 

Washington River Protection 

Solutions (WRPS)3.Fo 

3. From 4. Sheet 101of2 

2. To 

Sharon Clark 

6. project Title 

Pn 

Paul ~-rd 

Dcartd 

14.4Dat 

a. 

242-A Eva Orator KI Exhaust Ventilation S stem21ReiwDsrbto 

PO No. 7. Project No. 8. Tank FaIn/ank No. 9. Arealaldg. No,. 1 eiwDitiuif 

ucnrc 4i o n ees c 12. Subontractor or Supplier 

Pmmier Technologync 

13.0Pre~Purchass Evaluation 

14.3 rga1. 

Approval Date 

Section 

5.1.2 

0 i nformatlonRecotd 

16. specification 

Rpp.SpEC-3606 2 

17. Descriptionl of Item Submitted 

18, special instructions 0Resubmit CAdditional Into. 177 SubsIttion 2.FiaDspito 

Dimensional Drawings 

Equipment Weights 

Specifallo-t~l 

Material Descriptioni 

Performance Data 

- OrcJContral Diagram 

Date Sheets 

operate. InatruclJOras 

maint Instructions 

illusrativ Cuontrol stamps 


Page 0-1 5 

28. Changes Required-to Contract Document$? Yes [No 

29. Slgnatlure A-6003-219 (01-02)


Page C-16 

A-600 3 - 2 1 9 (01-02)

* 

*EchnO gy, Inc. 

44onodifformanlce Re Poft 


Page -17 

Re rt-No.: 

ITEM: 

11-168 

Fianders pre-tilters 

QtyRejcte 3 etsSerat 

Date: 3/24/2011 

JoCo; 88 

No. Filter Housing A, Filter HousingS, Fter HousingC 

* onrtColtfdrdoSpeoification Violated: 

systems Factory Acceptance, Teat Rev S. 

FAT.... .... test 2,2_A Evaporato r KI =Exha ust Vent ation 

Decito of.........~ll Sect11ionS 71B,7.19., and 7.20 of the state FArquire that a distribution. 

test be dlone to ensure velocity across each of the tlhers is limited to2%oftevra.Whnesigher-ilrsIws 

discovered that they did not meet this requirement. See attached reports. 

Identified BY. CaeG hha 

Flander desi n of the transition. 

Quality Assurance acceptance 

Disposito:(hOkoe Use-As-IS ~ Repair 

No action required 

Date: 3124111 

ffrgineeringfloieCL Manager acceptance 

Reectork- 

The flanders fiter housing does not facliltate airflow distribution tasting on the preifters without the pretilters, removed. This test was 

Cilient Approval Required (if no, prvd refpalT1Iafl 

N 

Yes

FT-16 (Rev. 5, '106) 

Date, -.. ~ z-'1 

4 IE!j 

C NUCON InternationaQI, Inc, O*project 

AAIT M DISTRIBUTION TEST REPORT 

EZ ~ ~ ~ ~~V OR~LW 

Unit, 


Page C-1 8 

aeI Plant________________________ 

Test Type; Capaty.... and/or. Distribution 

V 

TatCo 

Test Location: Duct 7< or. miter Face________ 

IFlow RatFace 

Spealfied 8, I 

CAPACITY 

tdO MCPM, ACFM, ) SCF 

DISTRIBUTION' 

Velocity, 

Total_ - 4 . FPM 

kverage . F4 PM 

Measuredrd on'~1e )CM CP .o C Obtained Readings 

(*de qle Ma~dmum It~-1,11 FPM 

a.of Design I iiu '~- P 

- Deviation from Average: 

Fan tablIty Check: 

No 

%of ~ g LeOgW '1{~ 9/ 

U(____________E5_______ 

t itent RiC 

met 

A. 

sit 

Acceptance Criterlia Met? ___-Yes-

NUCON InternotionaL~ 

CII 

instrumaentka) ID: 

InC. 

RAW DATA GRID 

C n t I P l a n t1 T e t N o : .J . . . 

' 

Type of Test Airflow CaPacity*_......~ pfiitpis sarping.- 

Airflow DistributiOn ArIVAerosol Distribution - te- - 

+33L) 4 10 

Total___ 

Average >- 


Page C-1 9 

%DevlaIofl 'from Average 

* %High +- " - 

%Lofiw ________l 

Notes ~ ~ ~ ~ ~ ~ ~~~o of Comet Wants__________________ 

"r-+ P- nnl-I A~ Shrnsture(s) NUCON international, Inc.- 

6r~ct

FT-i 6 (Rev. 6, 11105) D ate: L-4- ME~ 

NUCON Internton.i, Inc. PrWot :trz 

AIFLOW APACITY AND I OR DISTRIBUTION TEST RPR 

Client IPl-ant 

Unit C-11 bowi -m'-- zTest -. No: .. L 

Test Type- Capacity . and/or Dlsibuton_____ 

Test Location: Duct~.. or Filter Face_______ 

CAPACITY 

DISTRIBUTION 

Face Velocity 

PlwRate:1 

Totaed ~ FP 

Specified MCFMK ACF ,r SCFM Average _S *FPM 

(*old on 

Measured ~ ' FM, AoFM, or SCFMObandRunS 

e one-)Maximum 1-52 ' FPM 

-/ of Design 

M%~u ~c5 P 

Deviation fromn kVerage: 

%of Desig l -)dO H-igh + % 

Far.tablt.h : _ -at. 

Aiocepitnoe Criteria Met? __Yes Vi _o 

*Notes I Comments.-4:.$& "'~ - --- 

Test Personnel Slgnature(s): NUCON Internationa, Ino. 



Page C-20

FT-21 (Rev. 3 iiIOS5) 

t)keM,2t_-Tm. 

NUCON Internationai, Inc. Projsct Lik 

FRAWDATA GRID 

OllecuntI Plant\ 

*Uni~t &i- Test No-L 

instrument(s) QD: 

Bank Identillcaflofl 

0- e'k-: 

ell-~--- 


Page C-21 

* Typep TesBt~ Airflow Capaoity MUltiple Sarnpllng _ 

Airflow Distibutio%; Air/Arosol Distibution - Othr_____ 

( At Obtained Readings 

Notes I Comments' 

uI.DeviatioI from Average 

ic~iI~ ( 1 1~ ~%High + _122.Y 

____________________________ 

7T. Parmrnnfli A Srin~atLJe(S): NUCON International, Inc. 

ff required for.

F-rA 6 (Rev. 5, 11105) 

! NIJCON internotonlc, Inc. rjc 

Date '. -~- 

__________ 

Al FjLOW CApACIT'( AND I OR DISRBTO ETRPR 

Test Type: capa*fl.- 

Test Location- Dut..- 

and/or Dltbt~_:_ 

Or Filter P-ace_________ 

Test No, 

CAPACITYDisTRiBUTION 

CAPACTY -ace Velocity 

spelledMCFMI ACF SCFM kv g 

Notes I Comments: 

Measred _________ , ACWIor SFM 

~ ~r AGeO ne) 

btaIlned Readings 

Mam rfl 133 FPM 

minimumFP 

of Deign Deviation from Average, 

Measured 

.of Desig= ~~Xloo 

j-lih 1 

+-____ 

Unsat 

'Acceptance Criteria Met? __Yes. ____ 

Test Personne Signature(s): NUCON international, mop. 


'' 

(Ir)A 1 


Page C-22

FT-2.1 (Rev.3 '11105) 

NUCON Intornatioflcil, Inc. 

LIZ 

S client / Plant __4______________________________ 

Unit Pviz-- -'-ThtNo2- 

instrument(S) WD: 

Bank idenifteiOnl' 

RW DAA GRID 

cs-- 

___________ 


Page C-23 

Time,--_ 

Type of Test. A110iW C~padW Multipla Sanplg.. 

Airflow Disttbuflon V7 Air/Aerol Distribution-Ohe______ 

(Speff) 

0: /3~ ~ .. ~Obtained Readings 

%Deviationl tram Average 

%Low - 

Notasi~ ~ ~ ~ ~ ~ ~ ~ ComnsF__________________________ 

~~~~A 

r=~~~~~~~~~~+~I 

Irtreab UONItraioaI 

required~ f 

(3



Test step numbe: , q ITest exception number: (( 

Desciption: Nme ~ , 1Ih 002- Ltk~ cnodt t6 

2 11133C-S Ilkk r, 

-F 

PlL~P~ r" 

Testt Director 

Derip etion acpe:Fnlrslto 

Q 

'CA 

cetd 


Page C-24 

uet igin r Daze ,zi Date 

Asssur Dt aity 

ae 

t 

Date

Test step number 



' I.2 Test exception number: O 

Description: Prr m -cr ks rocedrc rif "ic a 

(ILY 1/- 17/1 

_________ // 

Hold for Resolution: ne t 

Originator Date iecoDt 

Interim resolution accepted: 

Final resoluion accepted* 


Page C-25 

~ni ~Date nginer Date 

A/L , 

ua Assumance Date ssurance Date

IWETechngy, Inc. 

Report No. 11-171 Date: 3/20111 

ITEM: 242-A Evaporator KI Job No.: 67e5 


Page C-26 

Qty. Rejected: 4 tests Serial No. NDE report #s: 

___________________________________11-1512, 11-1538,11-1539, 11-1540 

Contract Code/Standard or Specification Violated: Premier Bubble Leak Test procedure TP-1 .7 REV 5 

Description of Nonconformity: Premier procedure TP-1 .7 REV 5 requires a surface temperature between 

50 and 125 deg. F during testing. The actual surface temperature taken during testing on all four tests was below 50 deg. R. Test 

reports have been attached for specific temperatures. 

Identified By: Caleb Killian -rate: 3/30111 

Cause: Test was performed outside. Temperature of the entire assembly could not be controlled. 

Disposition: (check one) Use-As-Is fJ Repair flRework EJ Reject.E 

Instruction/Corrective Action: 

No further action required 

Engineering Justification, End condition: 

Premier uses Swagelok Snoop liquid leak detector which will work to temperatures as low as 27 degree F. (See attached) 

The lowest temperature recorded in the attached test reports Is 42.5 DEG F. 

Client Approval Required (if no, provide brief explanation): LI No Ld Yes 

Part 21 Reportable: ID No DYes 

P roecManagerEngineer SignaturelI Date Quality Assurance Manager I Date 

All Signature I Date (if required) 1Ciis1mer IDat (frequ~d 

NCR CLOSURE VERIFICATION 

Disposition as stated above has been satisfactorily completed and accepted by the Quaity Control Department 

Items listed above now conform to the requirements as outlined in the stated disposition. Production is authorized 

to proceed with fabrication or processing activities. D 

Al or 3rd Paty (if appocabe Date Quality Control Department -Date 

QA-15.1-1, Revision 2,11113/08


Page C-27 

Thohnoogy. ~Test 

#- 11-1:538 

Pro-ect Description: 

Bubble Leak Test Report -Io 

W on River Protection Solutions 242-A By I tV Ki 

Pressuire Gaenl, SeIc. Prmbe: 

Nopesr7a6e5e.Pesuewsstad anandb 

Commens : N/A~~l-11 

Dats tes satiste 1h eqieensofse07/11i esaedFT 

procedure Numbe 

Rev;~oi 

.a-nd 

0,31.6/EV


Page C-28 

Teoho~og~ 

b ~Tet#: 11-1539 

Bubble Leak Test Report 

Pro-ect Desc' ~tiou Wasbingdon Rivier Protetion Solutions 242-A Ev 

Pmer Teclinology, Inc. Pro' eat #. 6765 

Client PO #: 

N/A 

Date of Test: 

3/30/11 

?Z1gl 

rto ( 

Test pefformed By & Cort. Level: Caleb ilian. Level II Z d& 4',e t 

Wtessed B:Pu 

crd 

Item ilD or Serial Number: 242-jA Ev oqratorK1 

S3~~etc~ ord th ubdyelw 

eeho 

maintaiqed 

Ths stifeshe es uiemnl f, t 719502 anMped er10.3 in stt on vein 

FomTP .7-], nion 

360

TIeoly.IC 

TeTMehoo Teci iet 

Test#: 1.1-1540 

Bubble Leak Test Re 

6LO5 

CommenPOs: 1 3S/3011117 

Tethefomd 38t ert tisfie Cleb lnLevel ofHs71. n753jsaeFT 


Page C-29 

1 0V 

ear Numbe andI 1.7 REVRev.sol 

0,


Page C-30 

O TechnooyM Ic 

Te st#: 11-1512 

Pro. ect s ion: 


P g I of 1 

'Wasbig ORvrotc~timl Solutons; 242 = -A Evaorator K1 

Wiofnest B:2/1 

Procedure, Number and Rev: 'I? 1.7 REV -5 

Test Method or Technique: 

FLOW 

item ID or Serial Number, 

242-A Evaporator Ki 

Pressure Gan e Serial Number: PTI-378 

Cal Date and Due Date: 6/14/10-6/14/11 

Pressure CauE e: 0-3OnHGz -M 

Pressure Gauge Manufacturer DWYER 

Pressure GauvModel: DPGW-00 

Test Pressure: 

*24.2 IN H20 

Desi Pressure: 18.96 IN H20 

Trace G"s used: 

AIR 

Leak Solution ManUUcture IBrand Swagelock/ Snoop/ MS-SNOOP-GAL 

Name / Part Number 

Ten erature GaSe Serial Numaber: PTI-584 

Resut of Test: Ac taoble LjUn-Ace tble lanBelow 

Comiments-, *Pressujre mandated by step 7.29.3. 

**See NCR 11-171. FT 

This test satisfies the meats of stp7.29.4 in the stated FT 

-Farm TP-1.7-1, Revision 0, 3/6/09

2- Leak Detectors, Lubricants, and Sealants$Q 

Liquid Leak Veterctors 

Snoop and Real Cool Snoop liquid leak detectors detect gas leaks in hard-to-reach areas. 

Features 

" Sustained bubble action works even on very small leaks and vertical surfaces. 

* Flexible snooper tube extends for hard-to-reach areas. 

" Noncorrosive, nonflammable formula does not contain chlorine. 

11 Contains corrosion Inhibitor for added protection. 

8 Formula dries clean, without staining. 

Ordering Information 


Page C-31 

~ i~~ 

noop Liquid Leak Detector 

U Specifications:~ Meets the 

U Notoxi forulaperformance requirements ... 

* 

of: 

MIL-PRF-25567 Leak Detector 

Technical Informationi 

Compound, Oxygen Systems, 

* Compostiol: Deionized water and a Type I, 1 to 701C (33 to 158*F). 

surfactant. ~.NFPA 52 Section 6-12.2 Leak 

U Temperature rating- Can be used 

Testing Compressed Natural Gas 

o.er a temperature range of 27 to Vehicular Fuel System 

2000 F (- o90) P at60, Appendix A, 

Method 21, Section 4.3.3 

IZ 

Alternative Screening Procedures 

Using Soap Solutions. 

Ul ASTM G18B6-05, Standard Test 

Method for Determining Whether 

Gae-Leak-Datector Fluid Solutions 

Can Cause Stress Corrosion 

Cracking of Brass Alloys. 

Realicool Snoop 

K Specifications:. Meets the 

Liquid Leak Detector 

performance requirements of: 

U Works at temperatures as low as . i MIL-PRF-25567 Leak Detector 

(-54C) even on very small Compound, Oxygen Systems, 

-~-85*F 

leaks and vertical surf aces. 

Type 11, -54 to 100 (-65 to 33*F). 

t-* NFPA 52 Section 6-12.2 Leak 

Technical Information 


isS4 ~ . a Composition, Deionized water, a Vehicular Fuel System. 

, s~~"' urfactant, and ethylene glycol to EPA Par 60, Appendix A. 

prevent freezing at low temperatures. Method 21, Section 4.3.3 

0 Temperature rating- Can be used Alternative Screening Procedures 

&over a temperature range of -65 to Using Soap Solutions. 

- ~ 200 -4t 30.r:AT G186-05, Standard Test 


Gas-Leak-etctr Fluid Solutions 


cracking of Brass Alloys. 

A? Warning: Usb Snoop and Real 

Cool Snoop liquid leak detectors 

- nodnrn only on external surfaces. 

. p 

2 toz 11 (59 mi. 1 IM$. SNOP-2OZ: .' 6 in. 060fcm) 

S 11 OZ (236 m1L) I S.,SNOOP-BOZ7- 12 In. (so cm) 

I gal (s.$ l) M-NOPGL0 

P 

8 f1 oz Ps5 mL) TMS-RC-SNOOP--0Z: 12 In. (~3O cm) MaeilSafety Data Sheets are available from your 

1 al(381 Sl--O-G - fauthorized Swagelo k representative or at swagelokOorm


Page 0-32 

11/02/2010 13:07 2082388425 BISO PO30ATELLO (\A(G.. atI3 

PoebW FOX Note .7W7 

PoTLO ID 

No., Peet NumberA 

I M-6NOOP-AL 4w - 

I ~ ~ I ~ sO~Rd d 

440.51*AWT fox 

4ONVIF"PpLY 

mirao n ontinbd itat. bove m rdmh~ 

,ppriowst) orf t owcson am for eftramim pqpoefl a*l. 

rssponswbMt4. for t t=ncy or reiabKt afuicbbkxnwml 

swegobproduobemw ,mnb'*red undffrionGwfltttl -we 

been ued fin puducb of y=Ur der end no UK="a baring 

meinztc*jit aemmwy,ntesng In wici, a VIrarTsKw5Im0*-n 

@WDSOI eopIsnuuls florn JIUWW ndud in 

and SPA P.rt±6O App3SIIZ A, mfffud 21. $NdO-A tS 0nooP 

am ua rmut 

ICOIrIWWanr 

mmu~y No NMzvy boo 

or~te equlpinenthhv 

%fibw*vt L PRF 2858, MMP 

tave dtft 15 yesm 

"te 

take 

compoflflb hivm 

Used bn Moir 

melon 8-12-2 

Nto agbastm or ab~s*WdSUw~wr oOrOrfttgflf URsai 

TeSngaoit produss eedfd sho u am ru lor ums In 

reiot .deetDemer in, On. WsqakcoflyamYIS ~fIa 800 

*~ (I)MH- 

~ ~~O 

/Dwp M~ 

grgqcfiannSmmp 

Q& ar 9 Af 7 Joehmwew 

Ant~d I 

At~~~zro T-.k 1 ferj&P r .. e6tA 

P=140235 pae:s I of 1I10221


Page C-33 

Washington Rivpr Protection 

Solutions LLC (WRPS). 

SUPPLIER SUBMITTAL 

1. Subm~tal 0;~ 

4 Q 7-NA-SUB-023. . 

I.. 

2. To 

From.om 

Sharon'Clark 

Paul McBride (PTI) 

4.Poect Tis 

*242A Evaporator 1(1 Exhaust Ventilation System 

5. PO No. 6. Project No. 7. Tank FarmdTank No. 8. Aralldg. No. 

N/A TlPS2 N/A 242A Evaporator 

9. Date 

04/21/2010 

18.RevieW Distrdbution 

WT Donigan, R3-26 

*10. SubcontratNo.arid Release. No. 

40167, Release NA 

I i. Subcontractor or Suppier 

Premier technology, Inc. 

-TFly .en, Revie8 

E.yeR25 

-HyAC SME Review 

12..~ Pre-Purchase Evaluation 

13. Paragraph . ~ 

APProva Data 

14. Section 

Table 5-1 

\I Information/Rasoard 

15. SOW I Sppoication 


WL Adam, R3-26 

-QA Review 

-S Gingrich, stan..' 

Te. escipton f itm Sbmitedgingrich~urs-com~ 

Premier NCR 11-171 * .NDE 

Auth Review 

17. Speciel lnstrudtiona: jResqbml E Additional lnfo . 0 Substtution 

19. Suibmtalproposes OeVlatblS from contact documewnts? E] Yes N o 

20. S Approved j~Not Approved [] Approved whh Comnments flResubmit flWncMIofl/Racord 

21. Comments: 

WRPS concurs with Premi~er's proposed "Use-as-is" dispositionto NCR .11-171. WRPS has 

reviewed the applicable codes and standards for this contract and was unable* to identify a 

reguieement to maixrtain the surface temperatl~re above 50 degrees F. The ductile -to-brittle 

tra:6aitidn- point for 300 series stainless steel is in the range of -200 degrees F. The 

stack was designed -in accordance with ASbIE STS-1 and the other components. to ASME AG-1. and 

were confirmed by ptructural analysis for wind, seismic, and temperature to the applicable 

zone. ASME AG-1 Sections SA-4540 and TA-4300 and TA-III74300 do not specify a minimum 

temperature for testing. Each test run passed the pressure test at an airflow range of 

19i516 scfm -' 19, 850 scfm. As such, the components tested meet the leak test requir~enents 

of ASME AG-i-. 

22- Chenges Required to Contract Documents? Yea S.No 

23. Signature 

Page I of I 

4 Date 

A-6003-219 (REV 2)

* Washington River Protecionl 

-Solutions (ViIRPIS 

ShO 

* 

SUPPLIER SUBMrTTAL 

~~3. 


Page C-34 

Frm45e~t 

Pault Mc d Da2 4,i of 

a. 

242-A 

o. 

8.~~~1 PP~c ~l 

rtrK 1 Exhaust Ventilation 

PPr No. No .Taen Far/Taink No. 19. Area/Bldg. No. 

21* Re4iew-Disrbto 

Reiw _,4_ itibt 

40167 

11. Subonact No. ad etNo. I2. Sutiiractoror supplier 

Premier Technology Inc. 

13. [l pre-purhase Evaiualion Approval Data El vi E3 trrformationlReord 

4. Paragrapl' 18. Section 18. Speclication 

5.1.2RPP-SPEC-36062 

7. Desipfin of Item Submitted 

PTI-35.6 RO NCR 11 -171 Rev. 0 

* 1. istrctons Se~i 

lJ Resubmit ElAdditional info. alsbtiuln 22. Final Disposition 

1.24. 

D1 stion 

Date 20. Datla Descripion. N ItDale Appd. PJ Not Reaub. 

* Dirnenbjlonal Drawings 

EquIlpment Weights 

* Spacliftins 

* Material Descriptioni 

Periormance Data ---- ---- 7 1 1 

Circ./Oofllmi Diagram 

Date Sheet4.CntutinDcmn 

I 

illustrative Cuts 

install Instruclone 

. 3ConstrulctaDm en 

* operate. instructionls 

Meit. Instruollons, 

Spare Parts Usi 

28. Submitiall proposes Deviations from contract documents? El yes 0 No 

*Premier has completed a constructablilty review of the attached documents 

28. Changes Required to Contract Documnts? E Yes No 

- 29.1Signatur 

A-150034219 (01.02)


Page C-35 

A-6003-219 (01.02)

TchnologY, Inc. 

Rt tNo:7 1-7 

Date: 31301201 

ITEM: 242-A Evaporator KI Job No.: 6785 


Page C-36 

KCIIAVl 

5 4 . tstsSerial Rejet~d 

No. NDE report t: 

Oty 411-1512, Rjeced 

1,141538, 11-1539,11-54 

Contract U -de/Standard or Spectfication Viola-td: 

Premriler Bubble Leak-Test procedure TP-1.7 RV 5 

Desripti-on of Noncofiformlty Premier proc-edure TP-1 .7 REV 5 requires a surface temperature between 

50 and 12 deg. F during teat. The actual surface temperature taken during teting on all four tests was below 50 deg. F. Test 

reports have been attached for specific temperatuires. 

Identife By: Calb Klin 

Cause., 

ale; M1011 

Test was perforrried outside. Tempeature of the entire assemblyouyld not be controlled. 

uality Assurance acceptance, 

Englneerlh Jsloation, I End condition: 

Promie uses Swagelok Snoop liquid leak detector which will. 

he lowest: ternereturn recorded in the attached test reports Is 42.5 DEG'F. 

Eneringirplect Manager acceptance 

lEng.1P3M 

otr eun slws2 ere Wol ee atch 

Clen Approval Required (Nf no, provide brief explanation): ONLIO Ilyes 

Part 21 Reporabie: 21 No [jYes 

nagrlnglier ~gntuef Date 

QualitY ASSurance Manager I Date 

AlSinaur IDae(if required) CU, mr D~ate (if required) 

NCR CLOSPRE VERIFICATION 

Disposition as stated above has been satisfaictoily completed and accepted by the Quailty Control Department 

Items listed above now conformh to the requirements as outlined in the stated disposition. Production is authorized 

to proceed with fabrication or processing activities. 

Alor3r (f Prt ppicbl)Date Quality Control Department Date 

QA-1 5.1-1, Revision 2j 11113108

Teobnlogy.Inc.Test#- 

TMt eior+ By & CwL Level: Caleb Kiflisxi Level HI 

MehdoIT ': F 

pIcd NForm and3 Re-I. Tio 1.7 REVO5 

Tes 

11-1538 

W River protectoi Solutions 242-A B oZao 1 


Page 0-37 

It Do eilNIw 4-.xao e ni b

Technology. Inc. Te~t#: 11-1539 

Bubble Leak Test Re ort. 

Bmtm Rtem oKI Prote)o Souton 24i1Nimb) -42A 

p* za Tear =s1 091 b: PI - Pesr /.AcnlSF 95 

Dsi Psife 18.6N11A 

ar of Test 

3/30/1 

T qtr Tuna CatLvlPaeMYljr 2&0 LvlI 

Avt Pre Pawt *46.5De. 

Co mens and NRv 11-.171. 

Tsm dorThi tet teOWrmYso FLse t .02an .03i ttdFT 

item~~or iD- o7-r .22- Serial~ Eapraor 

Numn 


Page C-38 

o

Teohnoogy. 

nc. Tes-t# 4 

Bubble Leak Test Re: Or 


Page C-39 

J~~~~~ tern~~24 

-A 

l M E 

rSiJNu 

4- 

br 

~ Pressure Ia FaT .ii~n Rver oao ProtecSltionous 22A~pr~l 

Raesu of Test: Ac tale/3A0/11ai B~o 

Tet the lmetd o&Crt eel.Iqae LeelUow:wUr 

Item.For MJ- o7r1 Seiso 0* 

Nube;I5/08 

FV rAM 

Prsue ewa ub opesr ag s&Is'a n oitndb

Tec'61-lyTestc#: 

1141512 

proeot 


n ia Prtto Solution 242-A 

Pg I ofIl 

toair Ki 

I I eichn 1130yin Poiect#: 6765 

Cljet PO#: 

NIA 

Date of Test 

U/28f1 

Test Per0reBY & cart. Lee: Caleb 1(llan LeI II 

Wiftne eB. 

paw Mobide 

proceclir Numbei and Rv TP 1.7 RERV 5 

Test Meth1od oTwhi 

FLOW 

ltmir ID or Seial Numbe. 242-A Eva ror KI 

1'resrare iaNutber.' W 

PTI-378 

Cal Dateand Due Date. 6/14/10-6/14/11 

* PresaireG(o e .0-30IN HO 

Pressue auc . D'WYER 

preamire Gine Model' DPGWAA 

Name / Part Nmber':5P 

Date nd 11 Dte 11/21-1/21 

T This st tef there Aase ants f 72. ntesaeA 


Page C-40 

FOrrp-i .7-j,Rzvision 0,3/6/0S

2 Leak Deors, Lubricants, and Sesants 

Liquid Leak Detectors 

Snoop and Real Cool Snoop lliid leak detectors detct gas leaks In hard-to-reach areas- 

Feetures 

lz Sustained bubble action workcs even on very s"Il leaks and vertical surfaces. 

9 Flexible snooper tube extends for hard-to-rach areas. 

dos rit contain chlorine. 

N NonoorrOslV9, nonflammableformua 

19 contains corrosion inhibitor for added protection.' 

n Formula dries clean, withotstaining, 


Page C-41 

Vop Liquid Leak Deatecr 

n Wnod fruamiL-PRr-25667 

\ Speoffltoflsos Meet the 

promnerequirements Oft 

Leak Detector 

* 

-- ~~ . 

Technical Information Compound, Oxygen Systemls. 

Ucompositl qlr DeionIzed water and a TpeIIo7C(3to5F) 

s, po jnt NFPA 52 section 6-12.2 Leak 

Tmertre ~ ~~ ratlngt Can beue Testing Compressed Natural Gas 

over a tamperature range of127 of to t.Vehicular Fuel System. 

\ 200*F (-2 to .93*0). 

k. EPA Pr 0 pedXA 

Method 21, Section 4.3.3 

ScreenIng Procedures 

-SnootAlternative 

N No-c&ASTM E W 

-~ - 

Using soap Solutions. 

GIS$B-o5. Standard Test 


Gas -Leak.Detot Fluid Solutions 


Cracking of Bras Alloys 

- Real COol Snoop g UspeofficatihSw. Meets the 

* Liquid Loak Detector performance requirements oft' 

* ~ ~ ~ ~ ~ Work attmeaue.slwa 

. MIL-PRF-26W8 Leak Detector 

111 ork at5C) ve n onverylo ams compound, Oxygen systems. 

:4 .- leaks and venal vsrfaces. l T yo. 11 -54 to 1 '0 -6 to 33S'F). 

le k n v ri a NFPA 52 Section 6-12 2 Leak 

Technical InforIMation 


5-'.a Compositifl. Deionized water. a Vehicular Fuel System. 

X&S 

wsoatant, and ethylene glycol to. 

prevent freezing at I-W temperatures. 

z Temperature rating- Can be ueed 

over a temperature range of -65 to 

~20G-F (-54 to 93-0). 

. K EpA pan 60, Appndx A, 

Method 21, Section 4-3-8 

Alernative screening Procedures 

Sa Solton.des 

,sn 

V SMG160 n hte 

method for Determin~n hte 

Bgas-Leak-Detator Fluid Solutions 

Can Cause Stress Corrosion' 

Cracking Of Brass Alloys- 

.A Warrng ueb Snoop and Real 

orderIng Infor .mation Snoop liquid leak detectOrG 

. ,..,Cool .. 

a r ubeonly 

on external surfaces. 

2 f! o (9 ML) M.SNO0P-20Z.. j -. 5 In. 05 Orl 

I gal~.5 O-SNOP-Cal. MS 

Sat D~ata Stmt a aillle from your.at 

or swagelok.00rrL


Page C-42 

111/82/20iO 13'87 2082388425 BIM FOCATV-.LO PAGE 01/91- 

posW tFax Nots. 7M7 

NO M-NOOPbL w 

-air,' 

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Vo*wnion ontidIn Ow Ib~ matm add~ns ( w~ Iea I pitdbr OS'72 Wur 

$ufco, omb1Iuf ousft i fowaomm ntw satoao 

and PA P6 Amn* Sod Z1, a=4A& 8ne 

me A A'' *~ contocasmi md 

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*W& a 'D ~ikpw t 

lasorwlhaldig 

P001026 11 Iof. 

_ie 

7 

euid



Test step number: 7/,Z Z/3 a 7 16 Vf63 ['est exception number: 007( 

Description: 

r)tl Arr~ "~ced-c6. 

i~'"~- 

Origirlator DTest Director Dt 

Descriotionfl 

Description:. c.Q.- 1-1-7 t&)M 

Retest Required: 

Test Director Date E ierDate 


ngi -Date nleeDate 

Final resolution accepted: 


Page C-43 

Reetntqired: 

~11:7 Ksurance Date Qua I ssu~rane Date 

a --



Test step number 'a. 7.2 & 7. Z -9 Test exception number: C>>( 

Description' VtOP 

biterimHol acetdRnlesol resluio 

OrigeatDaDae 


Page C-44 

ution: a C ontiueest 

STes airetor Date



Test step number: 7 7a~Test exception number:~ 


Page C-45 

7s 'O wFLAf# L-2 ice 0Yr L-&I 4 

Description: 

~jctj~ill. ~~44 ~Hold for Resof ution: Tet 

Oriinaor ate Test Director .Date 

Description: IV_. ~ 3r2 


Rtenote uied: 

Test Director Date Date 

Interim resolution accepted: Final resolution accepted ! 

alty Assura e Cae Q ty Assur



Test step number: 7Y 7.2f,6 I Test exception number: 010 

Description: 96 1-6 Ie f /-, 0 00 4-/ e-1'7 AI e 

is t de 91 (Oute g n 10 M re ~ AVC L07 A7 

0& 


Page C-46 

(o14 itf A A r, 

Hold for Res olution: i u es 

01 iginator ate Test Director Date 

Description 

SRetest 

Required: Retest not require 

Test Director -Date iner Date 



Date n, Dat 

MV Assurance, Date Q ,uality Asurance 

Dt


(Thiis page may be reproduced as necessary) 

Test step number: 7*' c ~ Test exception number: Cj- 

Description:~ 

~~I~oiutonI~ Continue. Test: 

g0inator Dae Test Director Dt 

Description: TF- ;R~fej-- p _p2 

~( '~~- ~ 1tqi( Retest Required: Rett ot equired: 

Test Diredtor Date ~ ier ~Date 



Date ?i/siDate 


Page C-47 

1 7Assurance Date Quality Assurance Date

REQUEST FOR INFORMATION 


Page -48 

Contract No.: 40161. Rel No.: NA RFI No. (ContrasctNo-ReI. Alo.-RFI-S eq. No. Rev. No,): 4016NAFI-039 RO 

Project Description. 242-A Evaporator K1l HVAC Exhaust Skid ----- 

RFI Title/DescriptiOnl 

RFI Initiated By: 

Noise levels 

Paul McBride 

Proped Cai e To D honCs)? Yesete No/1 

Repos 

De.cit of Request 4/5/11 dtlo 

Phone: 2087829195 FAX No. ________ 

Phone: 509-3739894. FAX No. ________ 

Section 3o3.10.1 sttes theato "The stack and mechanical equipment noise emis sions at the 

maximum flow rate condition shall not create noise levels equal to or greae htl8 

8-hour time weighted average, or equivalent nos oe . prme mased8-1BAt 

one meter away from the fan belt guard and under the Wye section of the, stack. Please 

provide guidance whether this is an acceptable level or if further evaluation is re \aired. 

Recommedationl: 

Requestor: Paul McBride 

Section 2 

Response to Request 

By: 

Date: 4/5/11 

Contract Change Required? Yes No Contract Change Request No.:______________ 

ECN/pCN Required? Yes No ECN/FCN No.:_________________ 

Enginese'ring Review Necessary? Z Yes F- No Date Sent to Engineering: ~// 

amYe W1J"~Az 

Clarification Only? 

Responder. 

Buyer's Technical 

ERepresentative (TR)C-'~I..~Dt 

Leti Irn/S~r 

Page I of I 

Date 1O.jA 

A-603417 (REV 1)

Response: 

40167-NA-RFI-039 RO 

Noise Levels 

Attachment 1: WRPS Response 

WRPS can accept the noise levels measured in two places at 89-91 dBA. 

Discussion:* 


Page C-49 

While it would be guaranteed -that an 8-hour time weighted average less than 85 d.BA would be achieved 

with noise readings less.than 85 dBA in all places, individual readings of 89-91 dBA do not necessarily 

exceed this 8-hour time weighted average for the following reasons: 

*Premier's facility conditions do not mimic the actual on-site conditions where this equipment 

will be installed. 

*All readings where facility work will be performed did not exceed 85 dBA. The readings that 

exceeded 85 dBA were in locations where an employee may pass by but will not slop or stand 

while per-forming normal work activities. 

* Normal work activities do not require workers to be in the vicinity of the fans (i.e. at those 

points with noise levels greater than 85 dBA) for lengthy periods of time, such that an individual 

reading is not representative of an 8-hour time weighted average for a worker. 

' Should the noise levels be deemed excessive in the immediate vicinity of the fans and stack at. 

the time of installation, warning signs can be posted advising workers of the hazards and 

providing PPE requirements (i.e. hearing protection) or other administrative controls as 

*appropriate. 

Changes to specification RPP-SPEC-36062: 

No changes to the specification are required as a result of this RFI 

Will Donigan 

WRPS Project Engineering 

April 8th, 2011 

Note: This, response has been coordinated with W. Adams and M. Cranston.



Test step number . Test exception numben 1. 

-- US I. ~ ~ - 

* Description: -o 

Hold for Resolutio : Continue Test 

Oriinaor te Test Director Date 

Dc.AJpil TVALefrL~ - f~(u - AcL we ,r'- q rm- 

it It-r AttEP-I-rcATM UE- ')jqAk-M 

TVSg5---x-A.-r- 


Page C-50

REQUEST FOR INFORmATION 


Page C-51 

Cotr1tNo: 72 R l No.-. NA RFI No. (conractNo.Re. No.-RFI-sq. No. Rev. No.): 4 0167 -NARFI-04o RO 

Project Descriptiom, 242-A Evprtr1( ACEhutSd 

RFI tltleIDescriptiofl 

Damnpers 

RFI Initiated By' Paul mcBride Phne 097894 FAX No. ________ 

FaxdlEM~led o: ho Clark Phone: 593384 FXN.________ 

proposed Change to Document(s)? yes []No 

Description of RequestJReCOmmlendation sae,"rsuedo ilb ihn1%O 

Premier's FAT section 6.3 acceptance criteria ilb ihn1%o 

sae,"rsuedo 

value used to size Ithe fan. Test data or manufacturer certification on damper style is 

acceptable.' This requirement was take from WRPS's TRMF however, the only requirement in 

our specification is AG-1, DA-5110 which requires the pressure drop to be 

calculated/tested in accordance with.AMCA 500. Premier wants to write a test exception to 

change the acceptance criteria to verify that the pressure drop testing/ calculations were 

in accordance with AG-l, DA-511O. 

Recommenldation 

*Contract Change Required? r- Yes No Contract Change Request No.: -------- __________ 

ECNIFCN Required? I] Yes Z No ECNIFCN No.:_________________ 

Engineering Review Necessary? Yes U No Date Sent to Engineering: 'I SA~I 

Clarification Only? 5 .Yes 41~TO leI o.f/ A 0/ 

Responder: 

Buyer's Technical 

Representative (BTR) 

VeSDte1 

A"c.W*e oADt 

Page I of I 

Date ________ 

______ 

11fI 

A-6003-41 7 (RiEV 1)

40167-NA-RFI-040 RO 

Dampers 



Page C-52 

Rpo ns: eie request to write a test exception to change the accep tance criteria in Section 6.3 

of the FAT Procedure to verify complianc ihAM GiD-10 

Discussion- 

While the Test Requirements Matrix (TRM) has been supplied to Premier, it has been done informnally 

for Premier's and WRPS' mutual benefit such that it is not a contractual document for Premier. premier 

is contractually obligated to comply with the procurement specification, RPP-SPEC-36O 6 2- This request 

aligns with the requirements included-in RPP-SPEC-36 062 (see section 3.3.2.8) for dampers. Line item 

18 of the TRM does reference ASMVE AG-i DA-51i10 as the basis for the test which is in accordance with 

the requirements of RPP-SPEC-36 062 ; however, the basis for the acceptance criter .ia is listed as 

engineering judgment. While WRPS does expect Premier to discuss differenc *es between vendor 

supplied data and design inputs used in calculations and analysis with thi engineering subcontractor, 

the system (including fans and dampers) have passed all functional and acceptance testing in 

accordance with the remainder of the Factory Acceptance Test (FAT) procedure such that any variances 

between the calculation and the values for the actual components implemented in the system have 

been proven to be of no effect. With the assurance that the dampers meet ASME AG-i requirements, 

the approval of this request does not affect form, fit, or function of the dampers, fans, other system 

components, or the system as a whole. 

Changes to the Test Requirement Matrix: 

The TRMV line item 18 will be revised as follows: 

Was: 

I Dampers Pressure ASMVE 

Drop AG-i, 

(meeting ASMVE Section 

AG-i) DA-5110 

Ki-MOV-00l 

KI-MO-002500. 

2 

Ki-OV-0 

FAT Pressure drop Pressure drop will 

data shall be be within 10% of 

based on tests value used to size 

performed in the fan. Test data 

accordance with or manufacturer 

AMCA Standard certification on 

The AMCA damper style is 

Standard acceptable. 

Good 

engineering 

practice. 

Kl-BDD-001 

K1-BD-002shall 

number used 

be stated 

Kl-DMPR001 

Kl-DMPR-00 2 

Ki-BD-002with 

the 

pressure drop 

data.

Is: 

40167-NA-RPI-040 RD 

Dampers 



Page C-53 

18DmesPressure 

19DmesDrop 

(meeting ASME 

AG-i) 

ASME 

AG-i, 

Section 

DA-5110 

FAT -Pressure drop Pressure drop shall 

data shall be be based on tests 

based on tests performed in 

performed In accordance, with 

accordance with AMCA Standard 

AMCA standard 500. Test data or 

ASME AG 

1, Section. 

DA-5110. 

K1-MV-O500,D 

KIMV01Standard. 

The AMCA manufacturer 

certification on 

KI-MOV-00 2 numb er used shall be stated 

damper style is 

acceptable. 

K1-BD-0O1with 

K1-BDD-002 

the 

pressure drop 

data. 

Kl DMPR-001 

K1-DMPR-002 

Will Donigan 

WRPS Project Engineering 

April 19th, 2011 

Note: This resp~onse has been coordinated with D. Gerken. 

2


(This page may be. reproduced as necessary) 

Test step number 4 Test exception number CA 

f:79 L 

- 

-t 

for Reo Continue Test 

originator Dae Test Director Date 

Description: 

q 


Retettrequired 


Page 0-54 

Test Director Dat Date 

Itrmrsolution accepted: 

Finral resolution accepted: 

Quality Assurance Date Quality Assurance Date 

Date 

Date



VAGE1Ofj..- 

1PWP~ o a ! 

OOz 3 1S/f Q o- r - 

3 203 I3.sj /c77 or ytjfce cv 

007 3l If PrrU- /i k csI.' lc# 

00c4: Tc2str- 


Page 0-55 

4 

e' X"4C ~riiS Lkn1~

Attachment 3, FAT Test log 


PAGE 1 of- 

DAIE~jP~E 2 ESORP~IO - -- INtIAL 

3tA 

Aner 7.3~ 

/7 4'7 i'i/ul , 

S #"f1, x f 

3 1/11 /:00 3 7 IV ~ cc ~02 0 

32311)O~oo 

1h~s~124 

. 

3 M6 C - - r 

3/2~~~~~~~v&A e, 

'Ibiies /cr-" (.J I~iY -i 

32q ~ ~ ~ if 7, f'of'! A,~~~s 

32, 14 e:on e 

3 i)J.OAfl o 1 PredL Vk3 its 7 17lk 

3 2Dh o~oh~~ PA 

2/ 

7,11~f~t' G; 

~'j' '31n1" OuA- Olo ' 1 $ ~ ~ ~ 19''3~~ 


Page C-56



PAGEZof 

oil~~it(c~ I&44diS 7/ 2~~' 

33/ lOO 11fr4rL1S 

331~~ ~ni 

4 23 

L(~ ~ ~ ~ ~ ~~1 

as 72o~j 


Page C-57 

:v~7&~J~~eiLc gr 

7 f 

TIAA


(This page may be reprodUced as neressarY) 

PAGE 

.- of 

..... 


Page C-58


Page C-59 

PREMIEh TECHNOLOGY, INC. Project No. 006,765.000 

(PZI PjIJR VWS -242-A Evaporator KI Exhaust Contmct 40167 

Inc. Ventilation System No. 

FACTORY ACCEPTANCE TEST PLAN Sper.No. RPY-SPEC-36062 

____ ___ ___ 

___ ___ ___ ____ ___ ___ ___Rev 0 

Attachment 6.1


Page C-60 

Baldor Test Report & Product Information Packet 

has been removed from this report and relocated in 

VI File 50676 (See Supplement 10)


Page C-61 

1 PREM'~IER TECHNOLOGY, INC. FrojtdNo. 006765.0.000 

(IVMJ R VWPS - 242-A Evaporator 1(1 Exhaust coatact 40167 

1c(),Ventilation System No. 

RPUP-SPEC-36062 

FACrORY ACCEPTANCE TEST PLAN Spec No. Re 0 

Attachment 6.2.

li0 

r 

4-4 

'0 . 

Qjj 

w :5 

w 0 Z 

*- 

0jj 4. ) 


Page C-62 

.j.%

ABZ Valves & Controls 

A GFT Company 

L P.O. Boxl157 - 113 West Main 

YA ~Madisoni, KS 66860 

website: 'www.abzvalve.com * e-mail: info@1bzvMveXo-m 

VA (620) 437-2440 * Fax (620) 437-2435 

Justification for AIBZ Valves & Controls 

ABZolute Series High Perfonnance Butterfly Valve Usage 

Per ASN{E 31.1 Power Piping 


Page 0-63 

:ASM B3 1.1 Power Piping provides the design basis for making new, repair or replacement of piping typically 

found in electric power generating stations, in industrial and institutional plants, geothermal heating systems, and 

central and district beatinig and cooling systems. 

Justification is provided below to validate compliance of the ABZ Valve and Controls ABZolute Series High 

Performance Butterfly Valve to ASME 3 1.1.Code. 

Code Sectioin 107 VALVES 

107.1 General 

(A) Valves complying with the standards and specifications listed in Table 126.1 shall be used within the specified 

pressure-temperature ratings. 

Just#1cation - The ABZoluto Series ffigh Performance Butterfly Valve is designed in accordance with AN~SI 

BI 6.34 and API 609 Category B. Both standards are. listed in Table 126.1. 

(B) Valves not complying with (A) above shl be of a design, or equal to the design, which the manufacturer 

recommends for the service as stipulated in paragraph 102.2.2. 

Justification - ABZolute Series complies with (A). 

(C) Some valves are capable of sealing simultaneously against a pressure diffemtial between. an internal cavity of 

the valve and the adjacent pipe in both directions. Where liquid is entrapped in such a valve and is, subsequently 

beated, a dangerous rise in pressure can result. Where this condition is possible, the Owner shall provide means 

in design, installation, and/or operation to asure that the pressure in the valve shall not exceed the rated 

pressure for the attained temperature. A relief device used solely for the over-pressure protection from such 

entrapped fluid end conforning to (A) or (B) above need not comply with the requikrments of paragraph 107.8. 

Any penetration of the pressure retaininig wall of the valve shall meet the requirements of this Code. 

Justification - Not applicable. 

(D) Only valves designed such that the valve stemn is retined from blow-out by an assembly which functions 

independently of the stem seal retaier shall be used. 

Justifica 

tion -Blowout proof stem retention system is de-signed per API 609 standards and is located above the 

packing area.

(E) Materials used for pressure retention for valves in flammable, combustible, or toxic fluid systems shall in 

addition conform to the requirements of paragraphs 122.7 and 122.8. 


Page C-64 

Justification - In addition to ANSI BI 6.34 and API 609 Category B, the ABZolute Series High Performance 

Butterfly Valve can be purchased meeting the requirements of API 607 / ISO 10497 Fire Test for Soft-seated 

Quarter-turn. Valve certification. 

107.2 Marking 

Each valve shall bear the manufacturer's name or trademark and reference symbol to indicate the service conditions 

for which the manufacturer guarantees the valve. The marking shall be in accordance with ASME BI 6.5 and 

B1 6.34. 

Justijfication - The AB3Zolute Series High Performance Butterfly Valve is identified in accordance with ANSI 

B 16.34 and API 609 Category B. 

107.3 Ends 

Valves may be used with flanged, threaded, butt welding, socket welding, or other ends in accordance with 

applicable standards as specified in paragraph 107.1(A). 

Justification - The ABZolute Series High Performance Butterfly Valve is designed in accordance with the 

applicable flange specification listed in Table 126.1. Specifically, ASMSE B16.5 & B16.47. 

107.4 Stem Threads 

Stem threads of valves may be internal or external with reference to the valve bonnet. Outside screw and yoke 

design shall be used for valves NPS 3 and larger for pressures above 600 psi (4150 kPa). 

Justification - Not applicable. The ABZolute Series has no stemn threads. 

107.5 Bonnet Joints 

Bonnet joints may be of flanged, welded, pressure seal, union type, or other design, except that screwed bonnet 

connections in which the seal depends on a steam tight threaded j oint shall not be per-mitted as source valves in 

steam service at pressures above 250 psi (1750 kPa). 

Just fication - Not applicable. The ABZolute Series has no bonnet joint 

107.6 Bypasses 

Sizes of bypasses shall be in accordance with MSS SP-45 as a minimum standard. Pipe for bypasses shall be at least 

schedule 80 seamless, and of a material of the same nominal chemical composition and physical properties as that 

used for the main line. Bypasses may be integral or attached. 

Justification - Not applicable. The ABZolute Series has no bypasses. 

107.8 Safety, Safety Relief, and Relief Valves 

107.8.1 General. Safety, safety reliect and relief valves shall conform to the requirements specified in this Code for 

flanges, valves, and fittings for the pressures and temperatures to which they may be subjected. 

Justification - Not applicable. The ABZolute Series is not designed as a safety, safety relief; and relief valve. 

*Summary: 

The ABZolute Series H1igh Performance Butterfly Valve satisfies the requirements of ASMB B3 1 .1 Power Piping 

* Code.

ABZ Valves & Controls 

A GFT Company 

P.O. Box157 - 113 West Main 

Madison, KS 66860 

website: www abzvalve.coin & e-mail-, info(~abzvalve.gom 

(620) 437-2440 a Fax (620) 437-24351 


Page 0-65 

Addendum: 

The ABZolute High Performaance Butterfly Valve Series 400 has been specified for a customer 

application requiring design parameters of -30 inH2O at an atmospheric temperature range of -250 

to 1150 F and a n internal temperature of 5 9' to 1150 F. Thie stated flowniedia is. air. 

Further customer specifications include meeting the material requirements of... 

Body 316 Stainless Steel 

Disc =316 Stainless Steel / ENP 

Stem =17-4 Stainless Steel 

Seat = UHMWPE (Ultra High Molecular Weiglat.Polyethylene.) 

The 'ABZolute Series 402 Class 150 lug valve meets the design requirements for its intended use 

within the above stated criterion. The body is, cast from: I 16*stainless steel specification ASTM 

,5 A3 1-CF8M. Per the valve design specification ASME B 10~4, this is a' Group 2. material. 

Table 2-2.2A for Group 2 materials of standard class valyes designates CF8M at 200'F to have. a 

max pressure of 235 psig. 

The limiting component of the valve trim is the UI1MWvE seat. The temperature range for this 

material is -70*F to max temperature of 1 75 0 F. The system temperature criterion is enicompassed 

within the range of the UHMfWPE material. 

Testing: 

The ABZolute Series is ain API 609 Category B valve and is tested in. accordance~w with API 598 

& ASME BI 6.34 specifications. Required tests include a hydrostatic shell test at 1.5 times the 

1 00*F body rating and a hydrostatic high-pressure closure test at 110% of the design differential 

pressure at the 1 00*F rating. 

ABZ Valves & Controls provides a Manufacturer's Test Certificate in association with Material 

Test Reports (MTfR). 'Upon manufacture and assigning valve serial numbers testing will be 

performed and logged with the MTK- 

Conclusion: 

The ABZ Valves & Controls ABZolute series valve encompasses the customer stated design 

requirements and is suitable for the application.


Page C-66 

ABZ ABZolute High Performance Butterfly Valve 

Drawing has been removed from this report and 

relocated in VI File 50676 (See Supplement 7, 

attachment to 40167-NA-RFI-021)


Page C-67 

PR~EMIER TECHNOLOGY, INC. ProjedtNoL 006765.0.000( 

(DPCPNJLR WRS - 242-A Evaporator 1(1 Exhaunst Conrt 401. 

Z"I I rc Ventilation System No.__ ______ 

FACTORY ACCEPTANCE TEST PLAN Spec N~O. nPP-)'EC36062 

Attachment 6.3

DOCUMENT #.246-QVD-021 

I 000060 

DOCUMENT NAME: QUAITY VERIFICATtON Doc UMENTATION 

REV.: 

Rev, 

= DATE: 2P161201I 

ffDUST~S 1 

340i Grand Avenue 

Pittsburgh, PA 15225 

Phone 41 a-777-5i01 

PWEl III Fax 412-771-53B2 Page l of 3 

DOCUMENT No.- 246-~QVD-0211000060 Rev.1 

Premier Tec-hnology, Inc. 

Purchase Order Number 92378 Change Order 2 

Job Number PP246 

Invoice Number IVPL-0211000060 


Page 0-68 

Prerecholokbe QCRgliisedib 

Maki#), D e~VeMi & A~CDTW h 

Appiwve Bp __hE Ufaikip 

2415-lVD-0210OIJBO Rav. I .doc

0 -mDATE' 

DOCUMENT #: 246-OVD-021100006D 

DOCUMENT NAME QUALITY VERIFICATION DOCUMENTATION 

REV.: 

Rev. I 

211612011 

- 

m~sJNC. 

3401 Grand Avenue 

Plttsburgh, PA 15225 

Phone 412-777-5101. 

Po~ ~VBIPax 412-771-5382 Page 2 of 3 

Tai o ntentsPacias2 

SSM Industries, Inc. Certificate of Conformance Pac-e 3 


Page C-69 

&1gimnt =VNral VoIffed MctvPr 

Nilkom& cdiNQA4/ IE SBI 1'~t.. 

246.-QVD.021 WOOSO Rv 1 cloc

DOCUMENT #: 

246-QVD-0211 000060 

DOCUMENT NAME: QUALITY VERF~iC)ATION DOUMENTATION 

REV: 


' !'= 19DATE:. 2116I2011 

3401 Grand Avenue 

IN~tSTRESINC. Pittsburgh, PA 15225 

Phonea 412-777-5101 

POWER DYSOFX427158Pae 

CERTIFICATE OF CONFORMANCE 

CUSTOMER: Premier Technology, Inc. 

MATERIAL.-DESCRIPTION: 

O Line Q Descri tion: 

11 Ea- 30' isolation Damper Ta Number KI-MOV-O01 Rev.0 

2 1 s 0IoinDerTa Number KI-M0V-002 Rev.0 

3 1 Ea. 35' x 20' Backdraft Damper Tag Number K1 -BDD)-001 

4 1~. 36E 0 a~rf DamTa Number KI-BDD-002 

5 1 Ea. 35" x 20' Isolation ar rTpNme 1DP-0 

6 1E Es. 36 x 2"IsoLation auTlNme IOP-0 

DOCUMENT #:246-QVDJ-021 

SHIPME~T #:0211000060 

'PURCHASE ORDER: 

.JOB #: 

3 of 3 

1000060 Rev. 1 

92378 Change Order 2 

PP246 


Page C-70 

SSM Industries, Inc. located at 3401 Grand Avenue, Pittsburgh, PA hereby certfes that the 

material and/or parts based on the Suppliers Information furnished conform to the terms 

outlined below, 

1 . Premier Technology, Inc- Purchase Order 92378 Change Order 2 dated 

10/2812010. 

2. ASME AG-I 2003 thrTu 2004 Addenda for the design, material, fabrication, a nd 

testing of the dampers. 

31 SSM Industries, Inc. Quality As~urance Program SSM-QAP-01 Rev. I1I Dated 

* 7/7/2009, which includes Rev. 6 of the SSM aA Manual. 

Calvin F. Shannon l~~l 

Qualit Assurance Represeftative/DatB 

pew 3~.==.DRL~ 

3 a-0-e 3$ 

2.46-QVD-21 100050 Rev I doe

SS~l 1A 

Industries Inc. 

LEAKAGE CLASS 0 & 1 DAMPERS 

(BUBBLE TIGHT) 

PRESSURE DROP CHART 

10.000 - _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 

1.000- 

AP 

in 

W.G. 

0.100- 


Page C-71 

0.010 - III I * 

I1000.0 Free Area Velocity FPM 10000.0

Attachment "B" to Report SSM-BD-LT IAP 

Taken f rom Report 001 -QSLJM-D0 Fle # (9-1)P12P 

S, AReport Numbers - Pml1 7spP~ Pml I , PM124SP, M" P 

Industries Inc- PM,3SSp, pM1 34j, pM140SpaTnd PM143P :2 

10.000 

1.000 

AP 

BACKD RATDAMPER 

PRESSURE DROP CHART 

0.100 

FD 

1000.0 FPMW 10000.0 


Page C-72 

100.


Page C-73 

-~PREYMR TECHNOLOGY, INC. Projcct No. 006765.0.000 

WRPS - 242-A Evaporator Ki )Exhaust Cotrc 406 

~~Ventilation ~~~ 

System No.__ ______ 

FACTORY ACCEPTANC E ST PLAN Spec No. RPPeC-30 

Attachment 6.4


Page C-74 

DOCUMENT#: 246-LKK&OP-BTBTO-A25-S-Ol 3401 Grand Ave. 

La v 1 "m REVISION: 0 Pittsburgh, PA 152.5-1507 

= = O#. 2378(412) 777-510D1 

PO #: 9237 Fax (412) 771-5382 

JOB #: PP246 AE1 F1 

DNDUSRUESINC. JOB NAME: PREMIER BT, BT o & BDPAE1OF6 

DATE: 021181201 1 

P W R DI-VISION TITLE: BUBBLE & O 'PERATIONAL TESTING 

PROCEDURE 

DESIGN TYPE: 02102A 

LOCATION: HANFORD 

Fle #1 -54- 

DATA SHEET 

BUBBLE METHOD LEAK TEST TEST# D I 

Job Name & Numben Premier BT, BTO & BD PP246 Data Sheet# Dl Page _1 of. _I 

Lab Name: SSM Industries, Inc. Date: 2/812011 

Device Tested: BD Type of Observation: Direct 

Tag Number. K1-BDD-0O1 SBrometric Pressure: N/A 

Device Model Number, SSM-BD-01 Supply Air Pressure N/A 

Device Size: 20" x 36x 8' Signal Air Pressure or Voltage N/A 

Temperature: (wet and/or dry as appflcable) N/A Required max Open I Close Time (sec.) NIA 

Added Test Description: N/A Min# of Cycles: 10 

Positioner Operaflon (Poe Op) Verification: N/A System Test Pressure : N/A 

Added Tes DI.9sc; Syste 

DtTest (LI( or 

Type 

lop) 

(Blade 

Cycle. 

Sel, 

Pas. Op. Frame. 

elo) in-~ 

Pres 

QC 

Ace/Rej 

lo ntiDate 

Comments 

(Any added test or test result Information to clarify test. & results 

Record actions taken in connection with any deviations noted) 

QC Retest 

AceRej 

lnthdata 

T OP Cycle N/A AC Cycled 10 Times wvith Smooth Operation 

2 

7 

101 -1 1 

Comments: 

Puli Test 3 LBS Continuous 

Engineering Review & Approval (mnt/Date) ag- -k 

Note: Form may vary due to computerization 

Z46-OP&LK-BTBT0-S25--0I rev0-I

---------------- 

D ODOCUMENT*# 246-LK&OP-BTBTO-A6SS01 


Page C-75 

3401 Grand Ave. 

Pittsburgh, PA 165-1507 

* __W REVISION: 0 (412) 777-51 01 

-30=PO#: 92378 Fax (412) 71-.5382 

JB #- PP4 PAGE 15 OF 16 

*NDUSTR1ESINC. JOB NAME: PREMIER BT, BT 0 &BD 

DATE: 021118/20111 

TITLE: BUB~i E & OPERATIONAL TESTING 

SPON PR6CEDURE 

DESIGN TYPE:~ 02102A 


DATA SHEET 

BUS13LE METHOD LEAK TEST 

TEST001ag 

Job Name & Number* Prem1I ier BT, BTo & 31) PP2t6 Data Sheet # 01 Pag 1 Of -I- 

Lab Mama: SSM industries, Inc. Date: Dir/201 

Device Tested: 51) 

Typeomtd ofsur- ObNvanIArc 

Ta iubr. K1-BIDD-002 

Brmti rsue / 

De e dl Number, SSM-BD-01 

Supply Air Presre N/A 

Deviqe Size: 20'x 38"x 8Signal 

Air Pressure or voltageN/A 

Temperature: (wet anid/or dry.. as .applicable) N/A 

RequIred max Open / Close Time (sac.) NIA 

Added Test Decription: N/A 

M ri Of Cycles: '10 

PoaltionerO Oeratlon (Pos Op Verifir tion: N/A Sse etrsue / 

2 

3- 

4 

5 

6 

7 

8 

10 

Added Test Ciso system 00 Comments, QC Retest 

Test Type (Siade Sea, Frame P a Acc/i'j Any added tes orlest resultinformatloflitoc clIf test results' Aco/Rel 

OPL c C prs.Pb In. Int/Date R ecorod awwt Io taken in! connetioni wvh a 'SeViatointd I W~ale 

i ~cycle N/A AO Cycle d 10 Times with Smooth Operation 

Pull Test 3 LBS Continus 

FEngineering Review &ADrylD tlae.~ ~'' 

Note: Form may vary due to computerization. 

24&OP&LKBTBT0-SZ-S-W fwev0A


Page C-76 

DOCUMENT #: 246-LK&0 P-BTBTO-A25-S-01 

~- ~- EV1SON --- 0Pittsburgh, 

am# 9237 

PO#-27 


PA 1525-1507 

(412) 777-510DI 

Fax (412) 771-5382 

INDUS~rES~NG. 

JOB #: PP246PAE1OF6 

JOB NAME: PREMIER ST, BT o & BD 

DATE: 02/1812011 

F1 

POWER DIVISION TITLE: BUBBLE & OPERATIONAL TESTING 

PROCEDURE 


LOCATION: HANIFORD 

File #1-54 

DATA SHEET 

BUBBLE METHOD LEAK TEST .TEST# 

01 

Job Name & Number, Premier BT, STO & BD/ PP246 Data Sheet # 01 Page I of I 

Lab Name: SS nutis n.Date: 

2J1 112011 

Device Tested: BT 

Type of Obsevation: Direct 

TagNumber: KI-DMVR-UUI 

Barometric Pressure: 30.13 

Deie Model Number, SSM-ET-01 Su Il Air Pressure NIA 

Device Size: 20" x 36" X B" 

Signal Air Pressure or Voltage -NIA 

Temperature: (wet arnd/or dry as applicable) W-38, D-47 Required max Open / Close Time (sec.) N/A 

Added Test Description: N/A 

Min# of Cycles: 10 

Posifloner Operation (Pas Op) Verification- N/A 

System Test Pressure: NfA 

Added Test Disc. System , CComments QC Retest 

Det ATest:Type (Slade Seat~ Frame, Pres AcclRq] : Any added test or test result inlormation to claritfy test & results Acc/Rel 

(LK or OP)Cce oOp etc) in.j wg nt)Oati. Record actions taken in connection with any deviations noted) lnt/datle 

I LK Blade Seal, 30" 1Zero Leakage ( No Bubbles) 

2* OP- Cycle N/A Cycled 10 imes with Smooth Operation 

4 

5 

6 

7- 

8 

10_______ 

Comments: 

*M&TE: QC-SP-01 

Seat Torque Test 0.21" wg Q~ 20 Ft Lbs. 

Engineering Review & Approval (nt/Date) ~ ~,!5c'"Yvl Gt: .v N \I~ - 

Note: Form may vary due to computerization.


Page C-77 

DOCUENT# -24-LKOP-BBTO-.26--013401 Grand Ave.. 

REOCUMEN : 04-K O-TBOA5S 

REVISIN: 0 

PO #:92378 

Pftsburgh, PA 162541507 

412) 777-51'01 

rax (412)771-6382- 

JOB #: PP246 PAUE 16 OF is 

M UsTIMsONG. JOB NAME: PREMIER BT, BT 0 & BD 

DATE: 02/18W011 

powER Iii TITLE: BUBBLE. & OPERATIONAL TESTING 

POWE DIVSIONPROCEDURE 



Flle#14 

DATA SHEET 

BUBBLE METHOD LEAK TEST 

TEST # 01 

Job Name & Number. Premier BT, BTO & BDl PP246 Data Sheet# 01 Page I1 of _I_ 

Lab Name: SS nutis n.Date: W172011 

Device Tested: BT 

Type of~ Observation: Direcot 

T ubr KI-DMPR-002 

Barometric Pressure. 29.98 

DceMdel Number: 5SSM-BT-01 

Suoply Air Pressure NIA 

Device Size: 20" x 36" x 8" 

Signal Air Pressure or Voltage N/A 

Temperature: (wet and/or dry a plabeW36, D-48 . Required max Open / Close Time (sec.) N/A 

Added Test Description: N/A 

Min # of Cycles :10 

Positloner Operation (Poe Op) yerlisln N/A 

System Test Pressure :.N/A 

Added Test Disc; System: .. !qc Comments ~ t9 - 

De . 

1 LK 

fise~pl.ram4, Prevs Aco/Re] 

Cyc~e; P6&, Op. eo 16Y IritlDate 

Blade Seal, 30' AC 

Any added test or test result Information to dlrl, tet.&iot.A 

Record actions taken in connection wllh any deviations itiotbI 

Zero Leakage ( No Bubbles) 

p OR........ 

t~ae n 

2 OP 

F~rame___ 

Cycle Ni/A Cycled, 10 Times with Smooth Operation 

4 

5 

6r 

7 

-Comments: 

M&TE: QC-SP-01 

Seat Torque Test 0.20' w 21 Ft Lbs. 

Engineering Review &Approval (It/Date). V1_:2t L4VA -y t. 7- 

Note: Form may vary due to computerizat~on. 

246-OP&LK-B1BT0S256*.1 ,Tv0-1


Page C-78 

DOCMET #84- -BTT-25S 

D O C U M Es lN : 2 4 -K0- T T - - 5 S 0 

ME : 9278(412) R PO 

PO#: 2378Fax 

JOB #: PP246PAE1OFi 


P itts b u rg h P A 1 5 2 5 -1 0 7 

777-5101 

(412) 771-53B2 

WIDUSTRIE&INC. JOB NAME: PREMIER BT, BT o & BDPAE5OF1 

DATE: 0211812011 

POWR ~V~sONTIT-LE: BUBBLE & OPERATIONAL TESTING' 

POWE DIVSIONPROCEDURE 

DESIGN TYPE: 02/02A 

LOCATION* HANFORD 

File #1 -54 

DATA SHEET 


TEST# 01 

Job Name & Number: Prmier BT. BT0 & BDI PP246 Data Sheet #01 Page 1- of I- 

Lab Name: SSM industrieS, inc. 

Date: 2111/2011 

Device Tested: BTO 

Type of Observation: Direct 

Tag Number: Kl-MOV-001 


Device Moe ubr -BT-DI Supply Air Pressure N/A 

Device Size: 30" x 9' Signal Air Pretsure or Voltage NIA 

Temperature: (wet and/or dry as applicable) W-35, D-44 Required max Openi I Close Time (sec.) N/A 

Added Test Description: N/A_ 

Min 9 of Cycles: 10 

Positioner Operation (Pos Op) Verification: NIA System Test Pressure: NIA 

TT Added 7est Disc system 

bet 0M 

(LK 

Tet~ 

or )Cce 

(Blade Sal, 

.,&o)~ 

Frame, Pres 

in. g 

QC 

AcrdRej 

lnhJDae 

Comments 

[Any added test or test result informetion to clarfy test & results 

Record a ctions taken In connecton iwith any deviations noted) 

ac Retest 

Acc/Rej 

intldate 

1 LK Blade Seal, 30" AC ~ Zero Leakage ( No Bubbles) 

2 

______ 

OP 

Frame 

Cycle N/A -AC Cycled 10 Times with Smooth Operation 

Comments: 


Seat Torque Test 0.475" wg t35 Ft Lbs. 

Engineering Review & Approval (Int/Date) Q) :l:-, ~ k,-%,, ~ 

Note: Form may vary due to compuiterization. 

24&;OP&LK-B=0-SS-S-01 rev0-I


Page C-79 

DOCUMENT *: 246-LK&OP-BTBTO-A26-S-0l 

REVISION: 0 

LlP0 #: 92378 

Jos 0: PP246 

NDUTDSIC JOB NAME: PREMIER 5T, BT 0 & BD 

DATE: 02M1812011 

POWER DIVISION TITLE: BUBBLE & OPERATIONAL TESTING 

PROCEDURE 

DESIGN TYPE: 02/02A 


Pitsburgh, PA 1 525-1507 

Pa (4'12).771-5382 

PG~oI 


DATA SHEET 


TEST#01 

Job Name & Number Premier ST, BTO & BDI PP246 Data Sheet # 01 Page j.of I 

-Lab Nomew SSM Industries, Inc, 

Date: 2/1012011 

Device Tested: BTO 

Type of Observation: Direc 

Tan NumbrKih-M-0102 


Device Model Number: SSm-sT-01 

Supply Air Pressure N/A 

Device Size: 30"x Ir 

Signal Air Pressure or Voltage N/A 

Temperature: (wet and/or dry as aPplicable) WV6 D4 Required max Open / Close Time (sec.) N/A 

Added Test Descrition: NIA, 

Mn #of Cycles: 10 

Positloner Operation (Pos Op6eilaln N/ 

ytem Tesl Pressure: NIA 

Added Test Pp Sstm C Comments QO Retest 

aet Tes 

Pye*8~d~~ 

roq Pr AwC/Fte (Any added~test or tpst result information to clarify test & rdsiq$ts AcfR~ 

i, lne,2s 1 w tiat Record actions talier in j6irnedfion with gpy devlations notid) 

I LK Blade Seal ZeroLeaKage (No BUbbles) 

Frame 

2 ~ Cce ~ ~ /ycled 4 OP 

10 imes w~th Smooth. Operation 

4 

.6 

7 

Comments. 


Seat Torque Test 0.475" wg c 40 Ft Lbs.. 

Engineering Review & Approyal (It/Date) f 

Note: Form may vary due to computerization 

246.OP&LK40BTT-$2-S rev0L-1 

rt

PREMIER TECHNOLOGY, IN4C. Project No. 006765.0.000 

U ~EAIIER WR2PS - 242-A Evaporator Ki Exhaust Contract 4W,6 

STee, Ventilation System No.___ 

FACTORY ACCEPTANCE TEST PLAN Spec No. 0 

Attachment 6.5 


Page 0-80

V R 


Page C-81 

Cu SOMER:. 

PREMIER TECHNOLOGY INC 

CUSTOMER ORDER NO.:. 

931077 

FCS 

NU0ERA 

CONTROL JOB NO.: 

6601O. 

HOUSINGS MODEL NO.: 

BF1-3HSW FILTRATION UNIT 

HOU0NG6ERAL-O. 

m 

Pim Initial Manometer Test Pressure Req'd -30 . 141IcesWG.A Total Test T1M-: 15 Min, 

TestMethd; RESSRE ECAY PE ANS/ASI9'JNSJ M 'od of Leak Detection: SOAP SUBBLE. PER Nl 510 

TIME START (ti) RDIN 76-21i TABL At = MAX. W ~ LEA O S THE P E AIED RAL E-E T D S A U 

MANOMETERE (POU S S 

50SSR (m)in. ii 2mi. 3 li 60li m i . Fna 

(Max.. Lea)___) 

STEP. STR FINISH~_______ 

ISF LES THAN7 MA.PRISILTEK, HOSN OR9. SYSTMICETBE 

MOMETER TEARL) @ - UTME ~CPE 

BAROMETRI 

( 1 I -1 9c 

e 

ThERMOMETER 

Is?.l / 

3; ? Y FIN45 ARLY Pm Customer 

~ ~ ~ ~ ~ ~ ~ inhe W.~ to 

1.~ ~ ~ P ~ ~ f(ovr ~ ~ rmP ~ ~ ~ ~ RA-5.-2ueemn ~ P ~ .0 ~~~~II f 07 

v5. YALY -.. 3 - ) FCCQ. Rviwdb


Page C-82 

. .. .. .. ..... R O R D E R N O .: F IC s C C O N T R O L JO B N O . : 

PRSTOIER TEHNOLOGY, INC 9071 1005601 

HOUSING MODEL NO.: BFI-1-H3W FILTRATION UNIT 1HO00N6SEIALNO. 

Pjm= Initial Manometer Test Pressure Req'd -30 Inches W.G.1 ATotal Test Time: 15 m. 

'4g( - ERDA 78-21, TABLE WHERE MAX- LEAK 

0.0005 CFM/FT 3 

' OF VOLUME RATE IS 0.1% OF HOUSING VOLUME OTHER SPECIFIED VALUE: 

SAV = 0.03 x V 

60min.60in 

SAV =0.03x 

___=_0001x_ 

SAV =0.002 x 569.513 

SV=CFM SAV= .0949 OFM 

(max Permissible Leak) (Max Permissible Leak) ___ 

a TIME START (t) FINISH (t) At =v t ELD JOI SHOP DWG. REPAIRED RTTEDSTATUS 

(Min.) 60a ' Li- ID No. No. BY BY 

FINISH 

TM.START 

(IF)+ 49.7= T,-22 1 3 + 459.7 =T 

___ 

7f __ 

MANOMETER (Ph,) I@ a 0 §. (PW __ 

PRESSURE (Pm) Initial 1 min. 2 mmn. 3 miri. 4 min. Final 

(inch~esW.G.) -3 '' 2v '-i -39ITesting Techlan-- Date Q-7 

BAROMETRI INITIAL =PB FINAL Pis 

PRESSURE (Pa) 

ell~4- 

.Customer 

39 

Witne3ssedo. By 

(inches Hg) 

2. D~terrnlne P 1 & Pr (Convert.from inches W.G. to IblFt 2 ): 

1. RA =53.35 

(Gas Constant P, = i +PEx 70.73 pr =f x 5.204 + Pis x 70.73 

for~ir) Pj&r -&~204 + xc3 70.73 p=.'/ x.204+ 0~3' x0.73 

3. CALCULATE AVERAGE LEAK RATE OF.HOUSING USING THE FOLLOWING EQUATION: (STEPS A - E 

Step A. j ,\ VStop~ B. /. &91/(-7 111. ic2L !53 5-13 

Q KT, T RA At (0.075) 5Sp O (53)E 005 

StepC. ~ - '~ ~ 5~/~Step D./ , \StE 

StpC- oo '.&4a9 &~/g7 - - ~ 2)i 2 e&9 99! CFM 

SAV 0,00949 CFM 

IF Q IS LESS THAN MAX. PERMISSIBLE LEAKAGE. HOUSING OR SYSTEM IS ACCEPTABLE.. 

p jESCRIPTION SERIAL No, FREQUENCY OF CA LAST DATE FICSC PROJECT FILE, ORIGINAL 

L42aMANOMETER 7 - DAILY. WHEN USE ., - CUSTOMER: CPE 

BAROMETER (11 ~- H US D 9- OTHER: 

=THERMOMETER 

YEARLY Ito -,P93 I/o FICSC Q.A Reviewed by: 

/

HOUSING MODEL NO,:HOSNSEILO. 


Page C-83 

-V =Volume of Houaing to be Pressurized (No dummy Ster) 509.518 cubIc feet 

$A -Surfae Ara pf Housing to be Pressurized (No dummy filter) 

square_________feet____ 

Phw miiInltal Manometer Teat Pressure Reqrd -30 Inchesl W.G.&t Total Teat Time: 15 M I. 

Test Method P1WPSSUBDMY, PEAANSIASMSNSJO0 Method of Leak Detection: SOAP BUBBLE, PER N 510 

SAV = 0.03_____xC 

V SAVe =0.004 X V CF 

(Max PermIssIble Leek) (Max PermilbLsa) 

TIME START t FINISH (tOA),- WLD Jo! SHOP OWO. REPAIRED RETESTED STATUS 

- -n, ID No.. No. BY BY, 

TEMP. START FINISH _______ 

(8F) 23 + 45e.7=T -7 + 459.7 T 1 _________ 

MANOMETER '(Pti TG a (Pw_ ___ __ 

PRESSURE (Pmn -In~lI mln. 2 mn. .3 min,,j 4 mlii. Final 

(_nb__W___) 07__ S c 9 1ci a Test Technician: Dqate .'-'// 

BAROMETRIC 

PRESSURE (P8 )i 

* (Inphag 

INITIAL 

3o. 

Pil FINAL =P 8 

-3a 

usoe 

Witneased By 

/ 

1. RA =53.835 ?2. Determine P1 & P, (Convert from Inches W.G. to lb/Ft 2) 

2 4 

(Gor itntr) P , ,D +L Pox.76.73 3P. q X70.73 P1, xj 5. FileQx + 

70.7 

(Gaa Aonr) n P, = 5. 07 204+ 3 

x 70.73 q 

P, x6 204 &P xt + 70.73 

(-/ & .c 07 (0 )+4(; I$ , RISA. P (-4)3 W ) +(-?/Si. e7sral 

$. CALCULATE AVERAGE LEAK RATE OF HOUSING USING THE FOLLOWING EQUATION: (STEPS-A -E) 

Stop A. PV 

T ( -T T- 

"tpO. ' ~ (3,.6 o-7 - 

RA At (0,076) 

,; NA 

Step B. 19l7A,2Sb4lc o -1 f 

0= \ 3 0 o S.7 

.f StopD. f \j \Se 

(ooS7 0-000)k') bc - "- 

/(53.35) ( iC ) (0.075) 

- 00 Q00o~ CFM 

SAV = 0.0090:9 .:CFM 

IF 0 IS LESS THAN MAX. PERMISSIBLE LEAKAGE, HOUSING OR SYSTEM IS ACCEPTABLE, 

DESCRIPTION SERIAL No. FREQUENCY OF CAL LAST DATE FICSC PROJECT FILE: ORIGINAL 

W'iV sMAOMETERWtfJ 307-g< -i WHEN USED - 9-/0 CUlSTOMER: CPE 

BAROMETER Fj-5~c-7 YEARLY .. o. OTHER: . 

ITHERMOMETER 3C oo0- YE-ARLY -1 -FICSO 

0 A.Re~ewed by:

Attach ment 6.6 


Page C-84

1 

(6 

Vi Exhauster Electrical Assembly Traveler REV2.xlsx 

Attachment C - Continuity 


Page C-85 

Page 1 of S 

-I' 

I -1242-A Evap 1( 

Exhaust Vent 

Jn ob Name; System NlST Instrument #: 3411t' / 9~7iI00 V ?c3 

Job #: 6765 Calibration Date: ///oO 7 3'/e~i 

Technician Signature(s): 7IL 7JA - 

H 

E Engine 'o-bserer e~~~ 

Test Date: 6 /p ________________ 

[] Purpose: 

H Procedure: 

~~" I ' ' ~~Jumper Resistance: . ~ ~ ,-' / 

1. To verify continuity from/to each point identified in Table 1 Below: 

2. To verify electrical isolation from ground 

1. Using an NIST Calibrated, certified inst'rument: 

A. Check for continuity between the listed wire ends as shown in Table 1 

Fl 

SJ -Nate: 

U 2 

- 

- 

B. Verify that the resistance from each conductor to ground is > 100K C2. 

Ensure ground conductors have good continuity before being landed 'on a grounded connection. 

Ground circuits should be checked before and after landing the grouniding/grounded conductors. 

2. Document the resistance reading for Steps 1A and Ig .inTablel:Ibelow 

3. Place your initials in the INI box next to each wire asit -is "checked 

TABLE 1 _ _ _ _ _ _ _ _ _ _ 

Tes Point Results (a INI 

F-rom (Point A) To (Point B) End to End (near 0 a2) Wire to Ground (> 100k 92) 

Li Kl-K-002 TERM-41 

Kl-ENCL300 TB-5-2 

Kl-K-006 TERM-22 

Kl-K-006 TERM-21 Am" 

'Kl-ENC1300 TB5-1 KI-K-002 TERM-44 . I g~ 

Li Kl-ENCL-300 TB-5-7 Kl-K-007 TERM Al ____________ 

Kl-ENCL-300 TB-5-8 Kl-K-007 TERM A2Z____________ 

1 Kl-ENCL-300 TB-5-9 Kl-MOV-001 TB-7 

Kl-ENCL-300 TB-5-10 Kl-MOV-00lT- 

Kl-ENCL-300 TB--li Kl-MOV-001 TB-10 ____________ 

KI-ENCL-300 TB-5-12 

Kl-MOV-001 TB-il11___________ 

KI-ENCL-300 TB-5-13 Kl-K-002 TERM-il .0 

KI-K-002 TERM-14 Kl-K-005 TERM-22 * 0 ___________ 

Kl-ENCL-300 TB-5-14 Kl-K-005 TERM-21 .1 

KI-ENCL-300 TB-5-15 Kl-K-004 TERM-il112 

KlENCL-300 TB-5-i6 K-K-004 TERM-14 

KIENCL-300 TB-5-17 Kl-K-006 TERM-Al 

_ _ _ TB5-8zl-z06 

_ _ _ __30 

KENCL-300 TB-5-19 K1-K-006 TERM-Al 

I 

AMI 

zz-A 

KlENCL-300 TB-5-20 lKl-K-008 TERM A2 z z ~ z z~

-~ 

Attachm ent C - CofltflI ty 

Exhauster Electrical Assembly Traveler REV2.xlsx 

Resul s (LI 


Page C-86 

Fro (PintA)To (Point B) End to End (near 0 El) Wire to Ground (> look n2) 

Kl-ENCL-300 TB-5- 2 1 

Kl-ENCL-300 TB--2 

Kl-MOV-002 TB-B 

Ii-M-002 TB-8 

r1 K-ENC 300 TB5243 K-O-0B1 

~ l -ENCL-300on TB--24 K-MO-2 TB-11+ 

r 1 K-ENCL-300 Tb-t,-6 

K-ENCL-300 TB--i 

K-ENCL-300 TB-6-3B 

KlI-ENCL-300 TB-6-40 

KiI-ENCL-300 TB-6-51 

SHL5--VD T- 

Kl-5--VFD TB-Ol 

Kl5--VD T- 

Kl-5--VFD TB-S2+ 

K-5--VFD TB-S3 

I K-ENCL-300 TB-6-23 

L.ii K-EC-30 B6-4 

K HL-KO6TR-4 

Kl-K-00 TERM-il 

Ki-ENCL-300 TB-6-6 

i-ENCL-300 TB-6-7 

B2 

Ki-K-004 TERM-1 

I K-ENCL-300 TB-6-9 Kl -AF TB--i) 

KI-ENCL-300 TB-6-0 KI-AF TB--2L 

KiENCL-300 TB-6-1 

L Kl-ENCL300TB-6-2 

I Bl-A TBR--7 

B-A0 TBR--B 

I KiENCL-300TB-63 KiJBA li 

KI-ENCL-300 TB-6-4 

KJB-ATB-l#A1 

K-ENCL-300 TB-6-7 1 B-A-F TB-i-i5 

I -ENCL-300 TB-6-8 

Kl-ENCL-300 TB-6-9 

KlB-BF TB-2-l 

IA -BTB2- 

K-ENCL-300 TB-6-2 

KI-ENCL-300 TB-6-iI 

SLABBT--D 

Bl-B-F TB-20 

0F 

aim 

I53VF 

A

~ttachment C - Continuity 

T est PollintIN 

Exhauster Electrical Assembly Traveler REV2.xIsx 


Page C-87 

prm PontA)To (Point B) End to End (near 0 LI) Wire to Groun (> 100k P 

Kl-ENCL-30 0 TB-6-42 J- T-- 

Kl-ENCL-30 0 TB-6-43 J- T-- 

Kl-ENCL-30 0 TB-6-449J- T--. 

SI Kl-ENCL-30 0 TB-6-452 IBTB21 

KENLOOTB-6-6 

UJB- TB--15 

SKl-ENCL-30 0 TB6-7/ 

Kl-ENCL-300 TB6-48 

K-ENCL-30 

Kl-ENCL- TB-3- 

Kl-CL- TB-3-3 

0 TB--5 

Kl-ENCL-3 

IJ-ECL4TB-34 

0 0 TB-6-0 

IJ-ECL4TB-3-5 

KlENCL-300 TB--6 Kl-CL- TB-3-8 6 

* K-ENCL-300 TB-6-2 Kl-C-4TB-3-B 



K-ENCL-300 TB-6-69 

K-ENCL-300 TB-6-0, 

Kl-ENCL-300 TB6-72 

K-$L0 TB-6-7 

KlENCL-0 TB6-7 

K-ENCL-300 TB-6-9 


KlIENCL-30 B6 +iBA5B-- 

)K- DC13T--3 - 

K1-CL- TB-3- 

IJ-CL0TB-3-1 

IJ-CL4TB-3-1 

K-ENCL-400 TB-3-5 

Kl-ENCL-400 TB--3 

KlENCL-40TB-3 

KlEC-0TB4O 

Kl-ENCL-40 0 TB-47 

Kl-ENCL-40 0 TB-4-8I 

i-EBC-A TB--8 

KI-ENCL-30 T hdiB-A-5 K-EC-0 TB--10 

Kl-ENCL-30 66 K UBNC-A0 TB--111 

PDIT-KCL-307- B-6B71B--16 

Page 3 of 5

F 



Page 0-88 

,,ttachment C - ContinuityPae4f 

Test Point 

Results (fl)N 

From (Point A) To (Point B) End to End (near 0 £0) Wire to Ground (> 100k a) N 

PDIT-Kl-307 shid IJB-ATB-1-9 74,L 

PD[T-K-308 + 

PDIT-Kl-308 - 

PDIT-Kl-308 shId 

IJB-A TB114 

Ii B-A TB-1-13 

UJB-A TB-1-15 

_____________q_ 

______________ 

I I PDIT-Kl-309 + 

iJPDIT-KI-309 - 

vi 

PDIT-K1-30)9 shid 

PDIT-Kl-310 + 

IJ B-BTB-21 

_________TB-2-2 

1.1B-B3 TB-2-3 

I.1B-B3 TB-2-7 

_ 

A___________ 

I~04 

PDlt-K1-310 - 1.11-13 TB-2-8 4s____________ 

PDIT-K1-310 shid IJB-B TB-2-9 j(~- . 

PDIT-(1-31 + 

lB-B TB-2-13 

PDIT-K1-311 -1131 

B21 

PDIT-Kl-311 shid 

PDIT-K1-312.+ 

Ii B-B TB-2-15 

IJB-CTB-3- 12 

PDIT-KI-312.,-.. 

ADT K1-3.12 shid. 

IJB-CTB-32 

~ T:IB-B33 

PDIT-K1 313-IiCT38 

P IT-K 1-3 13 shi 1J- 

PITK-3 13 + 

PDITK1314 +IJB-CTB-3143_ 

IJB-C TB-3-7 

_ _313_ IJ-C B-- 

TB390_ 

J-Ts31 

_____________ 

________ 

___________ 

____________ _ _ _ _ _ _ _ _ _ _ 

_ _ _ _ _ _ _ _ _ 

____________ 

PDIT-Kl-314 shid 

Kl-MOV-001 TB-TERM 2 

IJB-CTB-315 

K1-K-007 TERM-14 1 

K1-MOV-001 TB-TERM 3 

KI-MOV-001 TB-TERM 6 


K1-MOV-002 TB-TERM 3 


K1-K-007 TERM-12 

K1-K7 TEM-il 

K1-I(-008 TERM I Z 

K1-K-008 TERM..- 11 

K1-K-008 TERM-li 

A 

10 

'1 

Jo ,~ 

J( E IL ------- C

.tachment C - ContinuitY 

Test Point 

Exhauster Electrical Assembly Traveler REV2.xIsx 


Page C-89 

Frm o n t EdOpen 

Wire to Ground 

Landed 

~60 

-Ci 

.1r e- 1bo-. 

jV 

Pg~f 

N 

INI



Page C-90


p ~ Ji -,7 v,- Page C-91 


ctachment D - Loop CheckPaeIo7 

242-A Evaporator KI 

Job Name: Exhaust Ventilation 

System 

Job # 6765 

Tes Dte 1/NIST 

NIST Loop Calibrator#i: 3 

~Calibration Date: 45, 

Pressure Pump/Guage Mif: k 

4V/ 

E ngner: 

observer: 

Technician Signature(s): 

Purpose: Verification of appropriate 4-20 mA signal when a known pressure is applied to the transmitter 

Procedure: 1. Break the inktrument loop and insert a calibrated 4-20 instrument calibrator 

2. Attach the pressure pump/guage to the pressure transducer 

3.. Pump up the pressure to the first test point 

4. Record the m4 reading from the calibrator in Table 1 Below 

5. Adjust the 0 and/or span if needed to obtain the proper reading 

6. Place your initials in the INI Column 

7. Repeat Steps I toG for each pressure setpoiflt you wish to test 

l-PlDT-306 

K1--PIDT-30B 

K1I-PIDT-310 - $ 

K1-PIDT-312 

9 Kl-PIDT-314 

-, 

- 

d 

___ressuna,-,; 

7017 

3. 

-A I lie. 

f 

, 

00

PRpKRTECNOLOGY, IC. projectNo. 006765.0.000 

-&A EMIEBR Vextlation System No. 

WRPS - 242-A Evaporator K]. Exhatust Contract 40167 

FACTORY ACCEPTANCE TEST PLAN SpecNo. RevSPC 3 

0 



Page C-92


Page C-93 

'Ai1KMONITOR. A~ W~ifCorporate offices 

P.O. Box Bs 

Santa Rosa, CA 95408 

C ORTel: (707) 544-2708 

AnoN Fax. (707) 528-2825 

FACTORY ACCEPTANCE TEST PROCEDURE 

OF 

242-A EXHAUSTER SAMPLING SYSTEM 


* P-O, No.. 90788 

AMC W.O. No. 71566 

3) IRevision 1, 2f4111 

Table of Contenft 

u Section 1: introduction 

a section 2: Preliminary Calibration 

.1 Section 3: Hardware Testing 

in Section 4: System Performance/ 

Operation Check 

N Section .5: Data Sheets 

Prepared By: __ _ __ _ _ __ _ _ Date: ~,2 -ef-// 

Reviewed By: Date . t- 

Witnessed By:. {LVJ Date: Q 0-

Factory Acceptance Test Procedur 

2of 13 

SECTION 1.0 - introduc-tion 

The subsequent sections of this procedure outline the various tasks required to verify that the 242-A 

Exhauster Samping System Is operating In accordance with design requirements. 


Page C-94 

1.1 Equipment Requirements: Equipment I Instrumepntation used in this procedure for verification 

of accuracy shall be currently calibrated to NIST. They shall include as necessary, electronic 

manometers, dligital multi-meters, signal generator, thermometer, and low pressure air source. 

Record serial number, calibration date and due date of equipment used on data sheet 

1.2 Personnel: Persons performing this procedure shall -have sufficienft knowledge [ training to 

understand the requirements and interpret results. 

1.3 Data Recording: Where requested during the performance of this procedure, data shall be 

recorded an appropriate data sheets. 

Persons performing tests and recording data shall enter their signatures and date at the end of 

the applicable section. 

1.4 Appicable revision to the following drawings shall be available during the test VV71558AA, 

W71558AC, W7156BAE, W7ISSBAF, W7156SAG, W71568AH, W7156SAJ and, W71586AK( 

SECTION 2.0 - Preliminary Calibration 

Q 2.1 Calibration: To calibrate components to design requirements prior to Installation in system. 

2.2.1 MASS-tron 11 mass flow tranarmitters; / controllers (FIT-I, FITC-2, FITC-B) shall be calibrated in 

arccordance with Factory Set-up Information Sheet (FSU) prior to Installing in Instrumentation 

enclosure. Record serial numbers on Data Sheet and attach FSU to this procedure when 

complete. 

2.2.2 VEL-trol 11 pressure transmitter! qontroller (PITC-4) shall be calibrated in accordance With 

Factory Set-up Information Sheet (FSU prior to installing in instrumentation enclosure: Record 

serial number on Data Sheet and attach FSU to this procedure when complete. 

Z.2.3 Temperature transmitters (TT-I, TT-2 & TT-3) shall be programmed and verified in accordance 

with span calculaton heet prior to installing in instrumentation enclosure. Record serial number 

on Data Sheet and attach set-up sheet to this procedure when complete. 

SECTION 3.0 - Hardware Testing 

3.1 Leak Testing: To verify physical integrity of sample transport tubing. 

3.1.1 Sample transport tubing in the Instrumentation enclosure shall be leak tested according to the 

following: 

a) DISConnect electrical power by positioning PDAI to the OFF position and locing out for the 

duration of the leek test.

Factory Acceptance Test Procedure 


Page C-95 

b) Remove flexible tubing at BETA CAM's in-line head AMS-4-1 & sea[ end'of tubing. -Note:" 

BETA CAM's In-fine head AWa-4-1, MASS-trans and VEL-trol dannot be positively 

pressurized, therefore It must be omitted from this leak test. 

) Close Isolation valves HV-5 thru HV-1 1. 

d) Open Isolation valves HV-3 end HV-4. 

e) Seal Record Sample inlet (Connection Code B) an top of enclosure. 

f) Seal sample exhaust (Oonneoflon Code G) fitting at boftom right of enclosure. 

g) Remove vacuum relief valves VRV-1 VRV-2 and sea( openings. 

h) Remove vacuum gauge P1 and seal opening. 

I)Remove signaI lines at P 8-1 & PS!2 and seal 

j)Position sample flow control valves FCV-I FCV-2 to 100% open by manually disengaging 

clutch and turning. handle. 

k) Position PCV-i to 60% open by manually disengaging clutch and turning handle. 

I)Pos~ton ICV-I and lCV-2 to pump P-1 by manually disengaging clutch andi turning harldle., 

mn) Remove make-up air-fiftar FL-I. on the left side of enclosure and connect source of. 

instrument air with regulator and shut-off Valve Tee in a 0-20 pslg gauge near inlet 

q) Open shut-off valve and adjust pressure regulator (as read on gauge). to 6 psig. 

o) Listen for any audible leeks and repair as necessary. 

p), Apply liquid leak detector to alJoints and conneutions frr sample transport piping betwveen 

Record Sample Inlet B and. sample exhausi(excluding pump. P-1). Repair any leaks 

detected.. 

ti) Manually position Isolation valves ICV-1 and IGV-2 to route pressure through pump P-2. 

r) Apply liquid leak detector to all Joinds and'conneotioris between ICV1 & ICV-2 on pump P-2 

side (excluding pump P-2). Repair any leaks detected. 

a) Disconnect test equipment, remove seals on connections and reconnect items previously 

removed. 

Performed 13. K 1 Date: A~ /i /f'. 

S.2 VOLU-probellSS shall be leak tested according SOP U.,'

jeaotory AOceptaflce Test Praredure 

4 Of 13 

3.4 power and functionalt cher.c To verify proper distribution of electical power and' 

functionality of coMPOfleflts- 

- 

- 

04 - 

-b) 

a) Verify isolation valves KV-3 thru HV-I I are open. 

RPP-RPTF-49670 Rev 0 

Page C-96 

Verify incoming power at PDAI is 240 VAC. Positonpower disconn'ect PD-A In the ON 

position. (:2 C, - lZ4O VAC) ~ ./));i 

c) Position C ircuit Breaker GB-I to the ON position and verify displays on transmitters 

FIT-i? FITC-2, FrrC-3 & PM0C4 are on. 

-6f d) Verify that temperature transmiltrs TT7-1, TT-2 & TT-3, totalizers TOT-I & TOT-2 and 

alarm* module AM-I are on, AA'v 4,gAt ~ (_ r ~rSIC~~ / 

- 

r4\ ) Verify that flow control valves FCV-I and FCV-2 position themselves in the open ~/0/i 

-_ 

-1) 

-n) 

position. Verif that pressure control valve Pcv-i positions itself in the full vacuum 

(0% make-up air) position. 

t)Turn on both power switches of the AMS-4 beta monitor RM-I and verify display comes 

on. 

g) Position circuit breaker CE?-2 to the OAF position and verify enclosure ight LT-i 

*comes on. 

h) Positionl Circuit Breaker CS-4 to the ON position and varfy fans in heaters i-T-i & NT- 

2 come on. 

) Adjust thermostat on heaters HT-i & HT-2 below ambient temperature and verify the 

1) Adjust thermfostat on air conditioner ACAI above ambient temperature and verify it. begins 

to cool. 

Position Circuit Breaker C13-3 to the ON position. 

mn) Position "HeadOff-AaJt~'switch SW-I to Auto, verify pump P-1 Is in lead by visual 

verification, and momentarily depress "Pump Start I Stop" pushbutton P13-3. 

Verify that after approximately 30 seconds pump P-I starts running and "pump #1 

On"' light L-6 comes on. 

o____ ) Verify vacuum gauge P1I indicates a vacuum. 

p) Momentarily depr-ess Pump LeibdILag"; pushbutton PB-& and verfy that pump P-I 

stops and "Pump f On" fight L-6 goes out. 

q) Verify isolation valves ICV-I and ICV-2 b egin to repositio n themselves to pump P-2, 

_____r) 

~ 

Verify that after approximnately 30 seconds pump P-:2 starts running and "Pump -02 

On" light L-7 comoes on. 

* 'o 

-s) Verify vacuum gauge PI1 indicates a vacuum. 

4 ~t) Momentarly depress "Pump Start I Stop" pushbutton PB-3 and- verify that pump P-2 

stops and "Pump 02 On" light L-7 goes out.

Factory Acsptanne Test Pracedura 

O 5cf13 


Page C-97 

A U) Position Cbwit Breaker CB-S to the ON position and veify Voltage between terminals 

LI and 12 of ternral blockTIB-71Is 240 Vac. (2c -*#' V,a) 0j, OArIII 

rk( v) Verify that heat trace controllers HTC-1, -2 & -3 are on and power Is available at their 

output terminals- 

_____w) Position power disconnect PP-A in the OFF posltin and verify all components go off.- 

_____ x) Position power disconnect PDAI in the ON posItion and verify all components come on. 

&y) Reposition Circuit Breaker CS-5 to the OAF position 

Perfored'1Y. ______________ ate e of 

SECTON 4,D -Systarm Performance/I Operation Check 

4.1 Scope: To operate the system anid check It a erall performance and operation of lts-Intagral 

components as a system, 

This section Is to be performed onlly aftsie Sectis 2.0 and 3.0 have been successfully 

completed. 

D 4.2 Sample Flow Control Loop: To verify sample flow controllers are rmintalinng constant volume 

42.1 Start pump P-I. 

42.2 Verify stack flow as read on FIT-I Is 0 SCFM. 

4.2.3 Aftr several mdnutes, the sample flows, as Oispiayed on FITC-2 & FITC-3 should stabilize at 

approxriately 2.00 SC$M. Record these flows. 

42.4 For the sample flows (recorded In 4.2.3), calculate the percent deviation from the Idea[ sample 

flow of 2.00 SCFM. These dieviations should be . 5%. 

% Devadon = DMraed SCFM - 2.00 SCFMx 100 

2. 00 SCFM. 

42.5 Monitor and record the Ifollowing output slgnvals (4 - 20'mnAdr.) atTB-3: 

Beta sample flow at terminals 3 & 4. 

Record sample flow at terminels; 5 & 6. 

Calculate and record devlatIonifrom Ideal output of 18.55 mAdc for each sample.. 

4.2.6 Verif each sample flow control valve (FCV-I & FCV-2) is open between 35 to 85% by recording 

controller output as dlrsplayad on tine 4 of FITC-1 & FlTC 2: 

4.2.7 Simulate a stack flow of I 9,k0Q SCFM. 

4.2.8 Verify that sample flows are not effected by changes in stack flow by repeating steps 4.2.3 

through 42.0.

Factory Acceptance Test Prcoedure 


Page C-98 

4,3 Sample Low Flow Alarms* To verlfy low Beta and Record sample flow alarms are functioning 

properly. 

4-3.1 Allow sufficienlt time for FCV-1 & lFCV-2 to bring samples undercontrol at 2.0D SCFM. 

4.3.2 Change Beta sample flow set-polnt to 1.50 SCFM (internal to the FITC-2). 

4.3.3 Once Beta sample flow drops below 1.70 SCFM, begin timing via stopwatch and verify after 30 

seconds the following alarm conditions: 

- Continuity does not exist across terminals I and 2 of TB-4 (remote alarm contacts). 

- OLow Beta Sample Fow' light L1 comes on. 

- Cabinet strobe light LT-2 comes on. 

4-3.4 Return set-point for Be9ta sample to 2.00 SCFM. Aftr Beta sample flow is above 1.70 SDFM 

alarm conditions remain. 

Momentanly depress "Alarm Reset" pushbutton PB3-8 and verify the following: 

- Continuity across terminals 'I and 2 of 71B-4. 

- "Low Beta Sample.Flow" light LA1 is off. 

- Cabinet strobe light LT-2 is off. 

4.3.5 Change Record sample flow set-point to 1.50 SUFM (internal to the FrlTC-3). 

4.3-6 Once Record sample flow dropi below 1.70 SCFM, begin timing via stopwatch and verify after 

30 seconds the following alarm conditions: 

-Continuity does not exist across terminals 3 and 4 of TB-4 (remote, alarm contacts). 

uLojw Record Sample Flouwv light L-2 comes on. 

-Cabinet strobe light L-T-2 comes. on. 

4.3.7 Return set-point for Record sample to 2.00 SCFM. After Beta sample fHow Is above 1.70 SCFM 

alarm conditions remain. 

Momnentaily depress "Alarm Reset" pushbutton PD-6 and verify the follovWng: 

-Continuity across terminals 3Sand 4 of TB-4. 

-"Low Record Sample flow" light L-2 is off. 

-Cabinet strobe light LT-2 is off. 

4.4 Sample Flow Totalizers: To verify low Beta and Record sample flow totalizers are functioning 

proparly. 

4.4-1 With both Beta and Record sample flows stable at 2.00 SCFM, record each totalizer value as 

indicated on display. Start stop watch. 

4.4.2 After 50 minutes record b*oth Beta and Record sample totalizer values as indicated on display. 

4.4.3 For both Beta'and Record samples, calculate each sample volumes for the 50 minute period -by 

subtracting the values recorded in step 4.4.1 from values recorded in step 4.4.2. 

Verify each volume Is 10 +/- I SCF. 

4.5 Stack Flow: To verify stack flow transmitter Is functioning properly. 

4.5.1 Simulate a pressure input of approximately 40% full scale (8,580 SCFM) to stack mass-flow 

'0 transmitter FIT-I.


7 Of is 


Page C-99 

4.5.2 Monitor arnd record 4 -20 mAdrc signal o f stack flow at terminals 1 & 2 of T13-3. Verify that' 

output is 10.40 4-1- 0.05 r'nAdc. 

4.5.3 Repeat step 4,5.2 for following stack flows: 

So% full scale (12,870 SOFM), 13.60 +1- 0. 05 rAda 

80%Y full scale (17,160 SON~), 15.80 +1- 0.05 mAda 

I100% full scals. (21.450 SCFM), 20.00+1 0.05 mAdc, 

4.6 Radiation Monitor alarms: To verify radiation alarms are functioning properly. 

4.6.1 Simulate a high radiation alarm from RM..1 and verify the tollowirig alarm conditions: 

- Continuity does not exist across terminals B and 6 of T13-4 (remote alarm .contacts). 

- Continuity does not exist acrss terminals 7 and 8 of TB-.4 (exhaust fan interlock contacts). 

-"Bet High Radiationff light L-3 comei an. 

-Bell BL-1 sounds. 

-Cabinet strobe light LT-2 comes on. 

4,6.2 Depress 'Alarm Mute" pushbutton MB-4 and Verify, that-bell BL-1 Is silenced and PBA is 

illuminated. 

4.6.3 Correct high radiation alarm from R-.Aamc~dif8rrah 

Momentarily depress "Alarmo Reset" pushboutton P13-6 arnd verfythe following-. 

Continuity across terminals 5 and 8 of TB-4. 

-Continuity across terminals 7 and 5 of T5-4. 

-Wata High Radiaton" light L-3 is off, 

-Cabinet stobe light LT-2 is1 olT. 

*4.8.4 Depress "Alarm Mate" pushbutto.1 PB-4 and verify that bell-BL-1 does not sound and 13141is 

not illuminated. 

kwe~ nr*Amotd&.c\ 

4.6 Simulate a radiation detector failure alarm from RMd-1 and verify the following alanm conditions:.. 

*-Continuity does not exist across terminals 9 -and 10 of T!34.(remnots, alarm contacts). 

'Beta Monitor Pailure" light L.A comes on. - 

-Cabinet 

strobe light LT-2 comes on. 

4.6.6 Correct a radiation) d etector failure alarm from RM-1. Alarm conditions reimain. 

Momentarily depress "Alarm Reset" pushbutton P13-6 and verify the following: 

Continuity across terminals 9 and 10 of T134. 

'"Befa Monitor Feilure" light L-4 Is off. 

-Cabinet 

strobe light LT-2 is off. 

4.7 Cabinst Temperature alarm: To verify cabinet temperature alarm is funotioning properly. 

4.7.1 Simulate a high cabinet temrperature using heat gun on teMperature sensor TE-3 arnd verfy the 

following alarm conditons 

- Continuity does not exist across terminals 11.and 12 of T13-4 (remote alarm contacts). 

- "Hi/L Cabinet Twmperiature" light L-5 comes on. 

-Cabine t strobe light UT-2 comes on.


8 Of Is 

K4.7.2. Correct cabinet high temperature condifti. Alarm conditions remain. 

Momentarily depress "Alaim Resut" pushbutton PB-6 and verify the followng: 

- Continuity across terminals I1I and 12 of TB-4. 

- "HI!f Lo Cabinet Temperature"v light L-5 is off. 

- Cabinet strobe light LT-2 Is Off. 

4.7.3 Simulate a low cabinet temperature using ice pack on temperature sensor TE-3 and verify the 

following alarm conditions: 

- Continuity does not exist across terminals I I and 12 of TB-4 (remote alarm contacts). 

-HiILC) Cabinet Temparmture"'light L-5 comes on. 

- Cabinet strobe light LT-2 comes oni. 

4.7.4 Correct cabinet low temperature condition. Alarm conditions remain. 

Momentarily depress "Alarm Reset" pushbutton 131-8 and verify the following: 

- Continuity across terminals 11 and 12 of TB-4. 

- "Hi / Lo Cabinet Temperature" light L.-5 Is off . 

- Cabinet strobe light LT-2 is off. 


Page C-100 

4.8 'Auto Pump Control: To verify that upon failure of one pump, the othar pump will automatically 

start to maintain sampling system operation, and that failure alarms are workdig. 

(D ____4.8.2 

____4.8.1 

____4.5.3 

____4.8.4 

Start system with pump P-1 in lead. After pump P-I has started running, simulate Its 

failure by removing signal line to PS-I. Verify pump PAI stops, -Pump #1 On" right L- 

5 goes off and 'Pump @1 Failure' light 1.-B comes on. 

Verify isolation valves iGV-1 and ICV-2 begin to reposition themselves to p ump P-2. 

Verify that after approximately 30 seconds pump P-2 starts running and "Pump ;92 

On " light L-7 comes on. 

Momentarily depress "Pump Lead/ Lag" pushbutton PB-5 and verify nothing 

happens. 

S 4-8.5 Reconnect signal line to PS-I. 

_____4.8.8' Momentarily depress "Alarm Reset" pushbutton PB-6 and verfy "Pump 01 Failure" 

light 1.-B is off. 

X L 4.8.7 Simulate a failure of pump P-2 by removing signal lihe to PS-2. Verify pump P-2 

stops and "Pump #2 On" ight L-7 goes off and "Pump 112 Failure" light L-9 comes 

on. 

V ~4.8.8 Verify isolation valves ]CV-1 and ICV-2 begin to reposition themselves to pump P-1. 

_____4.8.10 

4.13.9 Verify that after approximately 30 seconds pump P-1 starts running-andi "Pump #f 

On" light L-8 comes on. 

Momeintarily depress 'Pumpj LearLeg" pushbutton PB-S and verify nothing changes 

happens. 

S 4.811 Reconnect signal line to PS-2.

Fac~tory Acceptance Test Procedure 

,of Is 


Page C-101 

K~~) ______4.8.12 Momentarfly depress "Alarm Reset" pushbutton PB-S and vertfy "Pump *I4falre* 

Performed BY: _____________Date: 

4.9 Remote Pump Control.. To verify that pumps can be started and'swapped via remote 

commands. 

____4.9.1 

_____4.9.2 

Position "I-anct Oft'Arito" switch SW- to Auto. Simulate a remote pump start 

command by jumping terminals IS~ and 14 of TB.-4, Verify isolation valves iOV-1 and 

IGV-2 begin to reposition themselves to pump% P-1. 

Verify that after approximately $0 seconds pump P-1 start runnin g and "Pump Of 

On" right L-6 comes on. 

.9.3 Simulaig a remote pump swap command Iby jumping terminals 15 and IS of TB-4. 

and veriy that pump P-1 stops and "Pump,#1 On" lg! -6. goes out. 

-.. 4,.a.4 Verify Isolation. valves IGV-I and iCV-2 begi to raposltlcn thaessh to puipp P-2. 

4.9.5 Verify that after approximately 30 seconds pump P-2 starts running and "Pump 42 

O On" light L-7 comed on. 

4.9.6 Remove jumper at terminals 13 and 14 of TB-4. Verify pump P-2 stops and "Pumnp 

#2 On". light L_7 is off. 

'

* Faotory Aorpc est Procdure 

10 Of 13SEOTION 5.0 - DATA SHEETS 

1. 'Test Equipment 

Declf~/oe 

I! flJ - S/N: _ g A406- Cal: I!-86-ic Due G-R-L 

DacpinMdl V- .R.4rA SIN: _cr 0 Cal: 01~-'it Due.. G 2.iZ L 

Desciptiol/Moel- M-4V1 ea; /: 9- Cal: G~-)-1 Dua: G - 'I: 

DesriplflIondet SIN: ______Cal: _____ Due:-___ 

1. Drawings Used: WI5'-A* AZ7 C.7t+ A AK 

2.2.1 MASS-tron 11 MVass Flow TransmiftrslCoflfrollers: 

FIT-I SIN: 1 fo oA 

F17TQ,2 S/N: '7.IGGiJr, 

SIN: _____ 

FITC-3 

0 -7-2 VEL-Itrol 11 Static; Pressure TransmttrCoftroller. 

PITG-4 S/N: UCGJ 

2-2.3 Temperature Transmitters: 

TTI1 SIN: I Z q4,r7G 

1T-2 S/N: V1 

Tr-3 S/N: q-9,5 11 I 

22.4 Temperature Controllers: 

IITC-1 

S/N: _______ 

HTC-2 SIN:___ ____ 

HTC-3 

SIN: _______ 


Page C-102


11 Of 1 

4.2 Sample Flow Control - 0 SCFM Stack Flow 


Page C-1 03 

4.2.3 Beta Sample Flow (FITC-2 display): _ SCFM 

4.2.3 Record Sample Flow (FITC-3 display): ________SCFM 

4_2A4 % Deviation between actual and ideal Record sample flow %~% 

4.2.4 % Deviation between actual and ideal Beta sample flow (

Factory Accept ance Test Procedure 

12 of 13 

4.3.6 Continuity at terminals 3 & 4, T8-4 (ye's or no):_________ 

State of "L~ow Record Sample Rlow" light L-2 (on or oft): 

4.3.7 Continuity at termninals; 3 & 4, TB-4 (yes or no): 

State of 'If-ow Record Sample Rlow" light L-2 (on or of): 

Performed By: ______ ______Date: - 

Y £ 


Page C-104 

44 Sample Flow Totalizers 

4.4.1 Beta sample totalizer value at start 10SciF 

4.4.1 Record sample totalizervalue attt sr 

4.4.2 Beta sample totalizer value at start?\H ? C 

4.4.2 Record sample totalizer value at 

4,4.3 Beta sample totalizer volume :3SGF 

4.4.3 Record sample totalizer volume: 

Performed By: _____________ 

4.5 Stack Flow 

ii3 

Date.:- 

4 

________SCF 

9SCF 

4.5.2 40% Stack flow at terminals 1 & 2 I-m~ d o 

4-5.2 80% Stack flow at terminals I & 2 l359 mAdc 

4.5.2 80% Stack flow at terminals I & 2 

4.5.2 100% Stack flow at terminals 1 2 

Performed By: ________ ______Date: ~' 

4.5 Radiation MonitorAlarms; 

4.6.1 Continuity at terminals 5 & 8, TB-4 (yes or no): AC 

Continuity at terminals 7 & 8, TB-4 (Ves or no):VV 

State of "Bata High Radlatfon" light L-3 (on or off): 

State of bell BL-1 (on or oft): 

State of cabinet strobe right LT-2 (on or off): 

C_________ 

-SCF 

-OC>O rAdc.


13 Of 13 

4.9 6.2 State of bell EL-.1 (on or oft): 

State of PS-4 (on or offl: 

4.5.3* Con~tinuity at termkIals 5 & 6, T134 "ys or nio): ________ 

Continuity at tearminals 7 & 8, TD4 (yes or no): 

State of "Setaffligh Radiaton" light L-3 (on or ofl):________ 

State of cabinestrombe light LT-2 (on or off):_________ 

4.6.4 State of bell SW- (on or oft): 

State Of P13-4 (on or oft: 

4.8.5 Continuity at terminals 9 & 10, TE3-4 (yes or no): 

State of "Sat Mantor Failure ' light L-4 (on or oft): 

State.-Of cabinet strobe light LT-2 (on or oft):0 \ 

4.8.6 Continuity at terminals 9 & 16, 113-4 (Yes o no): ~e 

Stats of "Beta Mapftor~aII a" light L-4 (6n orof) - 

State- of cabinet strobe light LT-2 (on or off): 

Performed By:.-" Date: -. '~~ 

4.71 Cabinet Tearhiperature, Alarm 

4.7.1 Continuity at termilnals I1I & 12, 11-4 (yes or no): AO~ 

State of 'HIlLo Cabinet Temperature"' light L- (on oroft): 

State of cabinet strobe fight LT-2 (on or oft): . I ~ L 

4.7.2 Continuity at termInals 11 & 12, TB-4 (ye or no): 

State of "Hi/Lo Cabinet TemperatureO light 4-5 (on or 0ff: _________ 

State of cabinet strobe light LT-2 (on or of): 

4.7.3 Continuity at terminals I1I & 12, TB-4 (yes or no):;A. 

State of "OHi/Lo Cabinet Temperature' light L-5 (on or offl: _________ 

State of cabinet strobe light LT-2 (on or oft):'V 

4.7.4 Continuity at terminals I1I & 12, TB-4 (yes or no): 

State of vHi/Lo Cabinet Temperature" light Lr5 (on or oft): 

State of cab~net strobe light LT-2 (on or oft: ________ 

Performed By:-, ____________ Date:.__________ 


Page C-1 05


(IPM ER WRPS - 242-A1 Evaporator 1(1 Exhaust contraot406 

\/i~~ioog~.~ -Ventilation 

System N o. 406 


Page C-106 

FACTORY ACCEPTANCE TEST PLAN SpecNlo. Rev 0LC366 

Attachment 6.18

Am MONITOR 

SHOP TRAVELER 

for 

Instrumpntatiofl and Control EnlOosurs 

Project 242-A Exhauster Samping SYstem Unit No I Quantity: None I Qt I 

Purchaser Premier Technology, ]no contract No: 90786 


Page C-1 07 

pge Iof - 

AMC W.O. No: 71566 Reference Dwgv: W71 566AA,AC.ADAEAFAG 

AH.AJ.AK.aL& B 

A. FAB3RIdATION 

* Release enclosure to Production, "Inspected By: 2 ~ 

Veiycret enclosure part number adn h'ia 

damage. 

Locate and punch holes In enclosure. 

.Name 

By:rformed-By: 

Inspection Hold oint 

Verify all dimensions of penetration locations, Inspected By: ~-L Ic 

~'mount components to back plate. Performed By: .tr- L~L z) 

verify proper component orientation and installat~on lnspected 13y: .J 4d /2 - 

*PJumb sample piping, valving & LO0-flo's. Performed BY: IAI,., 

verify proper Iplumbing configuration. Inspected By: ~, 

* Install transmitters and control circuitry. Performed By: }/ X 2 )-', 

Verify correct installation, Inspected By' Z L 

*Wire 

components. 

Data 

Performed By: ~ . ~ z i 

Verify wiring Is correct per schematic and point-to-point Inspected By: I r't 

drawings. 

1050 Hopyper Avenue * PO a658 Saxita Rosa,'CA -05406 (707) 544-2706 * (7M7 526-2825 Itax 

Form 9-1, 

Rev. 4/92

SHOP TRAVELER 

for 

instrumentation and Control Enclosure 

AMC W.0. NO: 71566 Unit ID No: None 


Page 0-1 08 

*Install tubing. Performed By: /-/., 

Verify correct tubing connections. 

B, TESTING!I FINAL INSPECTION 

Inspected By: 

Page.2Lof 3 

Perform Leak Test of system piping per FAT for W71 566. Performed By, ;~-'-/ 

Verify results of leak testing are acceptable. Reviewed By -1 2-b 10~ 

*Perform Factory Acceptance Test per F.A.T. WV71566. Performed BY: P- Z V' 

Verify results of F.A.T. are acceptable. Reviewed By:Z 6-i 

Fia npcinof completed Instrumentaio and Control InspectdBy:__ 

enclosure. PEAAIN ~ B 

*Seal enclosure penetrations with tape/plugs. Performed By: J. 

Inspected By: f 

*Secure enalosure I access6ries In shipping crate. Performed By. _____ 

L 

Inspected By: z_________ 

*Include all markings I documentation with shipment. Performed By, Luw 11-A914/ 

Form 9-1, 

Rev. 4192 

Inspected By: 

10-50 Hlopper A-vexnue *PO o658 Santa Rosa, CA 95406 * (707) 544-2706 (707 526-2825 Fax 

-2(

SHOP TRAVELER 

for 

lnstrumehittlofl and Control Enclosure 

AMC W.0. NO: 715_6 Unit ID No: None 

sH-IPMENT 

Date of Shipmenit 

Carier __________________ 

Bill of Lading: 

Form 9-1. 

Rev. 42 


Page C-1 09 

page 3 .of3 

105 HoporAveue p.. D 638 *Sats Rosa, C& 95406 *C707):544-2706 *(70) 526-2825 Fax

AJRMNONITOR 


Page C-1 10 

Corporate Offices 

1050 Hopper Averni 

Santa Rosa CA 95403 

Tel: (707) 544-2706 

CORPO ATIONFax: (707) 526-2825 

CERTIFICATE OF CALIBRATION 

Air Monitor Corporation hereby certifies that ths instrument meets or exceeds all published 

AMC W.O. No. 71666 

specifications and has been calibrated using standards whose accuracy's are traceable to the 

National Institute of Standards and Technology within the limitations of the Institute's calibration 

services, or have been derived from acceptable values of natural physical constants, or have been 

derived by the ratio type of self-calibration techniques. 

Ct. Description Serial Number l.D.ITan No. 

1 MASS-tron 11 71566A EXHAUST STACK (FIT-I) 

Operating Span: 0 to 0.8077 In w.c. 

Output #1: 0.00 to 10.00 Vdc (Flow) 

Output #2: 0.00 to 10.00 Vdc (Temperature) 

Output #3: 0.00 to 10.00 Vdc (Absolute Pressure) 

Output #4: 0.00 to 10.00 Vdc (Differential Pressure) 

Display Line #1: 0 to 21,450 SCFM 

Display Line #2: 0 to I 50*1F 

Display Line #3: 26.00 to 34.00 In Hg 

Display Line #4: 0 to 0.8077 In w.c. 

Display Line #5: EXHAUST STACK (FIT-I) 

Power~ 24 Vacldc 

kJ~r--,- - 'r 

Calibrated By 

Date 

Q'r*AssuacMnge 

Date


Page C-Ill1 

rM M 

A ITORSanta m M O 


1050 Hopper Avenue 

Rosa, CA 95403 

Tel: (707) 544-2706 

CORPO ATIONFax: (707) 526-2825 


AMC W.O. No. 71566 

Air Monitor Corporation hereby certifies that this instrument meets or exceeds all published 



services, or have been derived from acceptable values of natural physical constants, or have been 

derived by the ratio type of self-calibration technirq!ues.- 

M. Description Serial Number ... l.D./Taci No., 

1 MASS-tron I1 71 566B BETA SAMPLE (FITC-2) 

Operating Span: 0 to 0.1482 In w.c. 


Output #2: 2.00 to 10.00 Vdc (Controller Output) 

Output #3: 0. 00 to 10.00 Vdc (Absolute Pressure) 

Output #4: 0.00 to 10.00 Vdc (Differentia Pressure) 

Low Alarm Setpoint 1.70 SCFM 

Display Line #1: 0 to 2.20 SCFM 

Display Line #2: 0 to 150'F 

Display Line #3-.16.00 to 34.00 In Hg 

Display Line #4: 2.00 SUFM (Controller Setpoint) 

Display Line #5: BETA SAMPLE (FITC-2) 

Power: 24 Vacfdc 

Calibrated By Date 

00KfAssurneMng Date


Page 0-1 12 



Santa pRsCA 95403 

AIRMONITOR 

CORPO ATIONTel: (707) 544-2706 

(707) 526-2825 

71=n COPORAIONFax 


AMC W.O. No. 7166 

Air monitor corporation hereby certifies that this instrument meets or exceeds all published 


National Institute of Standards and Technology within the limitations of the Instituters calibration 

services-or have been derived from acceptable values of natural physical constants, or have been 


Qt. Description Serial Number I.D./Taci No 

1 MASS-tron 11 715660 REC. SAMPLE (FITC-3) 

Operating Span: 0 to 0.1482 In w.c.. 


Output #2: 2.00 to 10.00 Vdc (Controller OutputY 

Output #3: 0.00 to 10.00 Vdc (Absolute Pressure) 

Output #4: 0.00 to 10.00 Vdc (Differential Pressure) 

Low Alarm Setpoint: 1.70 SCFM 

Display Line #1: 0 to 2.20 SCFM 

Display Line #2: 0 to I 50*F 

Display Line #3:16.00 to 34.00 In Hg 

Display Line #4: 2.00 SCFM (Controller Setpoint) 

Display Line #5: REC. SAMPLE (FITC-3) 

Power 24 Vacldc 

Calibrated By 

Quiffty Assurance Manaor 

Date 

Date

AIR ITOR MIO 

AmMONITORSanta 

COR IONFax ORA 



Page C-1 13 




Tel: (707) 544-2706 

(707) 526-2825 

AMC W-O. No. 71566 

Air Monitor corporation hereby certifies that this instrument meets or exceeds all published 



services, or have been derived from acceptable values of natural physical constants1 -or have. been 


Oy 'Description Serial Number I D.ITaca No. - 

1 E-rlI 71560D MAN. VACUUM (PITC-4) 

Operating Span: 0 to 11.033 In Hg (150" wc) 

Output #1: 4.00 to 20.00 mAdc. (Flow) 

Output #2: 2.00 to 10.00 Vdc (Controller Output). 

Display Line #1: 0Oto 7.000 In Hg 

Display Line #2: 2.00 SCFM (Controller Setpoint) 

Power 24 Vacldc 

Calibrated By 

Quality Assurance Manag& 

Date 

Date


Page C-1 14 

lk rCorporate AIR iTOR1050 M ~ 

A ITORSanta m MO 

Offices 

Hopper Avenue 


CORPOATION 

Tel: (707) 544-2706 

Fax: (707) 526-2825 


AMC W.O. No. 71566 

Air Monitor corporation hereby certifies that this instrument meets or exceeds all published 



services, or have-been derived from acceptable values of natural physical constants, or havebeen 

derived by, the ratio type -of self-calibration techniques. 

_h Desddption Serial Number -DIaiNo~ 

3. Moore Industries. Temperature 2129375 iT-I 

Transmitter, Model CPT 2129376 TT-2 

Input 0 to 150'F,.100 Ohm RTD 2129377 TT-3 

Output 0.00 to 10.00 Vdc 

\\~~-At7u . - ~- 

Calibrated By 

Date 

Z ityAsssuraneMn r Date

PREMIER TECHNOLOGY, IC. Project No. 006765.0.000 

W7- iRPS - 242-A Evaporator KU Exhaus Co 0167 

Ventlato Stm L No. 

FACTORY ACCEPTANCE TEST PLAN Spec No P-P306 

Attach ment 6.21 


Page C-1 15

* .~ 

* Ftauelsrgo 

7013 RT. 92B 

BATA~ NC 27808 

TEL. 252-923-2911 

FAXC 212-923-6931 

1LANDMJO8CSC 3N ]atUS ORDER No. 503 

CONTMPLON DATE: Id44t8 

Set" and docee± masn ment for~i sytw nfigimtinn for t10 test sectfoM/BBA filter bousiV 

UNL 

TIS R rSTRMOG PLATE WAS UN~ ON THE 

Figur 1.K 

. mesuremiits(Note-, Doumen 

Drawing not to scale) 

2.. ~ 8 2 

FlandersCSC model no. of tast sectios: 

Combination TSC-1H2W-0-04TM 

Otlet TSO-1H2W430G-304-Dl 

Flanders/CSC drawng no. and revision for inzm comb~ination, and outlet teat s.. tion 

Combination TS-01 7 Ra 

Outiet M023 Rev, 

FlandersICSC model no. of filter housings 

lst. Bank 31-12W-OGF-304-D1 

2nd. Bank BrGI-lH2M-c16ji-3o4lyi 

Pagel I 


Page C-1 16

Fk&a lSl 

7013 XT. 99' 

BATHI, NC 27808 

TEL 252-923-29l11 

FAX: 252-923-6931 

planders/MS drawing no. andrevision forfimter housings 

Ms Bank B-26 &eM I 

2ad. Bak ROAM EmL 

Document measuremefliS 

21~ 

a B. 

Setup and document measureents for the convenltional single wide HEPA systemn 

AIR~ FLOW STATION~ 

W&, ULTRATEC14. INC. 

29. a F~LEX DUCT BaE 

A/ I! HL 

Figure 2 

(Note: Drawing not to scale) 

Flanlders/CSC model no. of fjlter housing 33QxllHl-W--QQE3k4- 

Flanders/CSC drawing no. and revisicn Q-07 key 

Install prefitecs in inlet test section 

A. Size of prefilter .24~x2"X= 

Efficienzy of prefiter 3TI% 

C. Prefilter manufacturer Flianders Air Pure 

D. preflter nmanufacturer model no. FAP 3 

Page 2 

IN CENTER 


Page C-1 17

7013 VT. 92B 

BATE, NC 27808 

TEL, 252-92J-2911 

FAX 252-923-6931 

Install HEPA fUit n thme rst (no. 1) BEPA filter housing 

A. Sim of HEPA filIarno. I 24""xAI1IX 

B. liBPA no.1I manufacturer Yaler 

C. Manufacturer model no. of HEPA no.1 I -007-W-08-03-111-l -00-GG-FU5 

D. Efficiency of'HBA no.1I 22S22% 

E. Pressure drop fIEPA no. I D.2r w.g. at I=Q CFM 

X. Serial no. of WA no.I 1O717 

6. Size of HEPA filter no.2 2!",c2Alx la 

H. IIEPA no. 2 manufacturr Plod rFilter 

-1 Manfeotermodelno. ofMWEA no.2E-0--O.0-U11-0G-I 

I. Efficiency ofMHPA no. 2 22M22% 

IC. Pressure drop HEPA no. 2' DL24w.g. at1M CFM 

L. Serial no. of EWA no.2, J.170Q. 

Install EWA filters in the 2nd HEPA filter honu& 

A. Size aiEVA filterio. '2A*n2H1I 

B. HEPA no. I mamiffct=e Flandr.Elters 

C. Manuflattirermodelno. ofEPA no.l 1 000-W-OR-03-TGIEJ-00--GGnFU5 

D. Efficiency ofEWA no'. 1 92.998 % 

H. Press=r drop of BEPA no. I D w.g. at=~ CFM 

F. Serial no. of HEPA wo. 11XQ7590 

0. Size ofHEWA no.2 24"xWX~iU(2 

K. EPA no. 2 manufacturer =WFitr 

L Manufaoturer model no. of HEPA noc. 2 6-007-W-08-03-IT-1 1-90G-S 

3. Efficiency ofIHBPA no. 2 99,99 % 

9- Pressure, drop EPA no. 2 UL7'wg. at1IOM CPM 

L. Serial no. of HEA no.2 108718 

Objective 1 

Perfunn seal aurhwc and a complete pressure boundry leak test on the test seotion/fflter housing system per 

ASME NSIO-1989 (see attacimnent no. 1, objective no. Iafr results). 


Page 0-1 18 

Objective 2 

Poxform, seal surface and a complete pressure b~oundary leok test on the conventional single wide filter housing 

systemper ASviE N510-1 989 (see attachment no. 2, objective no,.2 for results). 

Objective 3 HP nuta ilt adok eto 

at5fori rcpacittest on the single wide B A it Ier system per, Init etlt an dbo eton9 

at CF 5D pr fltr.Diameter of ductwork is 12 inches. Refer to figure no. 2 & 11g=rno. 3for location of 

airflow sample in. the duct 

Page 3.

7013 XT. 923 

BATH, NC 27808 

TEL: 252-923-2911 

FAX 252-923-6931 

Airflow tolerance per ANSIASME N510-1980 and ASMM N510-1999 equals +/- 10% of flowrat 

Document readings on chart 

Vertical velocity 

readip(itfeetper 

mmi.) 

ffodzoatal velocity 

readinp fipfat per 

mlii.) 

Z000 

1910 

1 2 2 

2000 

I2025 - 

31415.16 

I 

1990 1 90D 

2050 1950 

M92 

2000 

1900 

1900 

7 

1700 

1900 

8 

1650, 

1100 

9 

1625 

1500 

10 

1600 

1.300 

Mean Velocity equals scm of velocity/ # readings 

XMQ/2=E261PM 

AV AD=2 f? 1 x 1826fpm =IAU CFM 

where Q=volume of flow (CFM) 

A - rea of duct (ft 2 ) 

V - velocity (PM 

is actual CPM within +/- 10% -X-Yes -no 

Test equipment TIM MODEL 1650 AZR VELOCIYMEl1 

*Serial no.: 707A 

TeSt teChniiE ______________ 

Date of test, : 


Page C-1 19 

Objective 4 

* Qualify conventional downstream sample port on the single wide HEPA filter system at 1500 OEM per filter, 

per ASMEA N509-1989. The numiber of sample points shatl be in accordance with Section 9 of the lndustrial 

Ventilation Handbook. 

Tolerance requires that any single point sample shall be. witin +1- 5% of the calculated average concentration. 

Page 4

PORT 

Figure 3 

(Not. Dra int to scale) 

fliareetaiof ductwork Is 12 inches 

BAThI, NC 278 

TEL: 252-923-2911 

FAX: 252-M2-6931 

Test rslsi ioogrmws per Ittar 

Verlicea con kation readings IBorizonta1 concentation readings 

(1) 8 (6)?7 (1) 7 (6) 7 

(2)7 (7) 7_______ (2) 7 (7) 7 

(3) 7 (8) 7 (3)7. (8) 7 

(Q)8 (9) 7 (4) 7 (9) 7 

Required CFM at test MD 

Aotu4 GEM at test "n~ 

Phiotometer n. AUl 

Photometer model no. 

Photomneter serial no. 22 

Aerosol generator modelno.If&5 

Aerosol type Pb-Aq:Qpi 

Approx aize of hole in filter 0,125 hbg 


Page C-120 

NOTES: A HEPA filter was installed in the single filter bank housing. The BEPA filter had a hole in the 

center of the filter Aerosol was injected upstream of the H~EM filter. A downstream sample wax thn takent 

through the downstreamnsamplo port in accordance withi Section. 9 of the Indlustrial Ventlation Ha~udbook (see 

fgur no,.2 for actual location of port), 

Page 5

* 

* 

Ftwtau~5 4 

7013 RT. 92E 

BATH, NC 278 

TEL: 252-923-2911 

PAX 252-923-6931 

Tot,a cn ,,I atralneadings divided bytIe inmbe of readings. 

laI 12Q = mean concentration 

Allowable tolerances equals mean +1- 5%. 

* typperlimit 7 4 concentration 

Lower limit fi3. concenitration 

Single point concentration, taken from the center of the duct tough ihe downstream samnple Port 

(see figure; no. 3)2 concenration. 

is the single point concentration 

Test technician 

Date of test 2MM12 

1 wiitin +15% of iffe mnean concentration? 

X.Yes _____A 


Page 0-121 

Objetive 5 

Perform air capacity test on the teat jieciou/filter housing HEPA filter system per, Industrial Ventflii 

Handbook, Section 9 at 1500 CM per filter. Dimater of ductwork where sample is taken is 12 inches, Refer 

to figure no.1I & figuse no. 3 for location of airflorw samTpl in the duct. 

Aitow toleranceper ANSI/ABIENS 10- 9 80 and ASUM X510198 9 equals +/-- 10% Of flow rate.- 

1 2 

Document -readings on chart 

3 4 5 6 7 8 9 10 

Vertical velocity 

readings (in feet par 

min.) 

3775 3500 3700 3750 3900 3900 3675 3600 3550 3500 

oraiznta ( veloetyr 3 5 3900 3900 350 3900 3800 3650 3500 2950 2700 

W 

Mean Velocity equals surm of velocity/ # readings 

72850 / Q 3421 FPM 

Q7- AV I= ftI! x I6IU fpm = 2M2 CFM (both filters) 

where Qvolume of flow (CFM) 

A. area of duct (ft 2 ) 

V -velocity (FPM) 

Is actual CpM wffo&nI 10% Xyes _no 

Test equipment S oe 15 i elct ee 

Serial no.: 

Test technician. 

Dat of test NU2LIA 

Page 6

F6", /am 

7013 RT. 92B 

BATE, NC 27808 

TB: 252-923-2911 

TAX 252-923-6931 


Page C-122 

Objective 5 (continued) 

PeiffornPrewmD~ drop test on the Wellt test section. binmibfl test setion, and oulet-lust sectionat 1500 

CFM Per ifiter witha maxircm pressure drop across each test section in the,"test" mode of 1. 10 inches water 

gage. 

Required CFMQQQ (both filters) 

Actual test CFM 2L5 (both filters) 

Air capacity test t0Mole Mc is +-10% Per AMVIASM NSIO-1980 & ASME N510-1989Q 

Maximumn pressure drop tolerance is 1.10 at 1500 CFM per olter in the "teat" mode for. Wnet combination, and 

* outlet test section 

Actual pressure drop of inlet tea section at 1500 CFM per filtet ,B4 inches Water gag. 

Actual presur drop of combin.Ation test section. at 1500 a~mper filter SAinches water gage. 

Actua pressure drop of outlet test section at 1500 CPM per fiter2 inches water gage. 

Are reading. accptble? Xyes = n 

Instrument used to measure pressure drop hridyA DfMutne. 

Serial number M935UA 

Test techiia 

Date of test 9t10198 

Objective 6 

Perform pressure drop test on the inet testsecton, cunblntlontent section, anld Outlet test section at 1500 . - 

CFM per filter with a mium pressure drop'across ea test section in the "Operating' mode of 0.05 inches 

water gage. 

Requird CFM 300 (both. filters) 

Actual test CFM 2Z2 (both filt=r) 

Air capacity testtulerance is +1- 10% per ANSI/ASMGN510 4980 & AgMENSl(O-I989 

Maxhrmn pressure drop tolerance, is 0.05 at 1500 CPM p r filter in the "operatig mode for inlet, 

combination, and outlt test secton. 

Actual presur drop of inlet test section at 1500 CPM per filter inches water gage. 

Actual pressure drop of combination tes setion, at 1500 CFM per flter ~LA inches water gage. 

Actual pressure drop of outlet test section at 1500 CFM per flter DJU inches water gage. 

Are readings acceptable? X-yes -__no 

Page 7

F~ I~u 

7013 R.T. 923 

BATN, NC 27808 

TEL: 252-923-2911 

FAY- 252-923-6931 

Instrument used to measure presanr drop ShrrdeArDt 

- 

Seriainuber M354 

Test technician__________ 

Date of tvst 910/98 

Objective 7 

Perform air aerosol uniformity teet on Ist HEPA filter bank (upstream) at 1500 CFM per fflter, per ASME 

N510-1989 with the inlet, combination, and outlet test sections in the "test" mode. 

Air aerosol tolerance per ASlvM N510-1999 equals +/- 20%. 

- Document percenst concentration readings on chart 

Required CFM at test =QQ (both filters) 

Actual CFM at test 2M~ (bath filters) 

Photometer mnfr. Anl 

Photometer model no. IQ&2l 

Photometer serial no. 2M2 

Aerosol generator model no. I12&.5Ak 

Aerosol type Po~y--AlpJ%lekin 


Page C-123 

742d% 77 % 0 0 

R 

Bottom 

* NOTES: Aerosol was. injected into the aerosol injection ports on the inlet test section. The inlet, combination, 

* and outtWs sections were in the "test mode. Aerosol readings were taken through test ports located on the 

1stEPAiffIter housingupstream of the ifiters. All upsiream concentration readings were taken using the, 

100%/ scale on the photometer. 

Total all concentration readings divided by the number of readings. 

2~ = 2k mean % concentration. 

Upper limit .21 % concentration 

Lower Eimit 11 %h concentration 

.Are the allowable limits within +1- 20% of the mean? 2L-yes__n 

Page 8 

D

Date oftst325/98 'C' 

f7 013 RIM 92 

BATI, NC 27808 

TEL* 252-923-2911 

FA]t.: 252-923-6931 

Objectdve 7 (continued) 

Peform air aerosol uniformity test on Ist HEPA fiter bank (upstream) at 1500 CFM per filter, per 

ANSXIASIVf N510-1980 with inlet combialit and Outlet test sectIOn, In the "test* made. 

Air aerosol toleranc per ANSI/ASME N510-1980 +/-20 0 A. 

Document percent eoacentration readings on chart 


Page C-1 24 

86% 76% 73% 65% 70% 81% 8 5% 91%Y 

88% 80% 740p 67% 68% 7 8% 8 5 /% 94% D 

0 

994 2% 71% 71%/a !161k 70%~ g91/o 93% 0 

89% 80% 79%Y- 69%y 72% 80% 89+% 92% 

Required CFMat t (bothfiltets)- 

Aztua CPM at test ZM~ (Oth filters) 

Photometer mfr. AUl 

Photomnewe model no.I&2 

Photometer aerial no, IM2 

Aerosol generator model no. TD-& 

Aeosol type Mny-A Ie ffin 

*Bottom 

NOMES Aerosol was isujerWe into the aerosol injection ports oni the inlet test section. Inlet combination, and 

outlet test seotions were in the "testmodeP, Aerosolireadings were taken throughi test ports located on the 1st 

BEPA filter housing, upstream of the fiters. -All upstream. conceutrationreadings were taken using the 100% 

scale on t photometer+. 

Total. all concentration readings divided by the nmber of readings. 

i~/f" Mxean % concentration 

upper liita % Concetration 

Lower limit 64 % concentration 

Are, the allowable limits wltiu +1 20% of the mean? L..yes --- o 

Date of test M ML2 

Page 9

* W 

Fknuu I L 

7013 PCT. 92E 

BATHL NC 27808 

TEL: 252-923-2911 

FAXM 252-923-6931 

objective 7 (continued) 

perform air aerosol unifocrmity test on 2nd REPA filter bank (downstream) at 1500 CFM per fite-r, Per ASME 

NS510-1989 with the inlet, combination, and outlet test sections in the "test!' mode, 

Air aerosol tolerance per ASM N510-1989 equals +-20%. 

Required CM at test 3Q (both filters) 

Actual CFM at test 2M (both filters) 

Photometer mfr. Al 

Photometer model no. TA2 


Aerosol generatorodel no. IDA-5A 

Aerosol type D-~f 

Document percent concentration readings on chart 

TOP 

Bottom 


Page C-125 

NOTES: Aerosol was injected into the aerosol injection ports on the combination test section lnlet, 

combination, and outlet test sections were in the -,test mode,. Aerosolireadings were take thlrough test Ports 

located on the 2nd BEPA filt~er housing, Upstream of the filters. All upstream concentration readings Were 

taken using the 100% scale on the photometer. 

Total all concentration readings divied bynumhe of readinlgs. 

L- Bi2j £mean % concentration 

Upper limi~t Ml % concentration 

Lower limit b2 % cancentration 

Are the allowable limits withxin -F/- 20%A of the mean? X.ye5 .... nmo 

Test tehica 

Date of test 8125198R 


Peform air aerosol uniformity test on 2ud HEPA filter bank (dow~nstream) at 1500 CFM per tilter, per 

ANSI/ASME N510-1980 with inlet, combination, and outlet test section in the "test" mode. 

Air aerosol tolerance per ANSVASME N510-1980 +/-20%. 

Page 10 

D 

0

70131M. 92B 

BA7th NC 27808 

TEL: 252-923-2911 

PAX, 252-923-6931 

Docmentperoln concentration readings on chart 


Page C-126 

-87% 8% 79% 78 % 92%V 100% O/ 9% 92% 

* 87% 84-% 82% 81F%. 89% -92% 24% 22% D' 

0 

78% 80%Y 82% 82% 91% 96% 94% 90%0 

8% -1 85% al7Y 97% _28%/ 98% 89% 

Required CFM at test3Dfl (bot filters) 

Actual CFM at test 2M~ (both filtmr) 

Photometer iofr. Anl 

Photometer model no. Il2 

Photometer aerial no. 17 

5 Aerosol generator model no. TD-S 

Aerosol tp bA b~a 

Bottom 

NOTES: Aerosol was fjorted into the aerosol injection ports on the combination test-section. Inlet; 

combination, and outlet test sections were in the "~test mode". Aerosol readings ware taken through teat ports 

located on the 2nd HHPA filter housing, upstream, of the filters. All upstreami concentration readings wore 

taken using the 100/c, scale onl the photometer. 

Total all concentration readings dividedby the imunber of readings. 

Me1t M3~ maean % concentration 

Upper limit JM~%cocnrtn 

* Lower limit 7Q % concentration 

* Are the allowable limits within +-20% of the mean? Xyea --- o 

Testtehiin___________ _ 

Date of test 8125/98 

ObJective 8 

Perform air distribution test on IdtlIEA ffiter bank-(upstreani) at 1500 CFM per filter, per ABMB NS 10-1989 

with the inlet, combination, and outlet Wet sections in the "operating" mode. 

S Air disribution tolerance per ASME X51O-4989 equals +/- 20%. 

Page 11

7013 XT. 92E 

RATH, NC 27808 

TEL: 252-923-2911 

FAX- 252-923-6931 

Document velocity readings on chait 


Page C-127 

58fl.pm 57-~ 0 0 

R 

Bottom 

RezquiredCPM at test 3 (bothfilters) 

Actual CFM at test 2M~ (both filters) 

Velocity instrument 'rSI 1650 ArVelocity MIdeir 

Serial number 4707AA 

NOTES- Air distribution readings were td=ce with the inlet combination, and outlet test sections in the 

UoperatiWg. All readings were taken through sample parts locatd downstream of the 1st EHPA filter bank on 

t HEPA filter housing. Readings are recorded as feet per minute (fpm). 

Total all velocity readings divided by the number of readings 

IM / 2= 5M pm(mean) 

Mean M +1- 20% 

Upper limit Mfptn 

Lower limit _4fi fpm, 

Are all readings within the allowable limit? X-yes ---- n 

Test technician______________ 

Dat of test L1082 

ObjectiveS8 (continued) 

Perform air distribution test on 1st H1PA filter bank (upstream) at 1500 CFM perffilter 1 per ANSI/ASIM 

N510-1980 with the inlet, combination, and outlet test sections in the "operating "mode. 

Air distributiontolerance per ANSI/ASMbI N5IO-1980 equals +/- 201/. 

Document velocityr readings in feet per minute (PPM) on chart 

TOP 

590 570 600 550 D 

580 570 0 

570 570 570 550 

Bottom 

Page 12 

D

Namte,~ fE 

7013 RT. 92E 

BAIZ NC 27808 

S TEL: 2S2-929-2911 

FAX 252,923-6931 

Required crM at test (b~f oth filters) 

Actual CPM at toot 2M~ (both Maltrs) 

Velocity inst meat -TS 165Q Air Velo ft Meter' 

Seriai mnber 4707AA 


Page C-128 

NOTES: Air distribution readings were taken with the inet combination, and outlet test sections in the 

"4operating" Ali readingswere taken tfi~ug sample ports locatedi downstram of~ the lot EMA filter bank on 

theIIEPAfflterbousing. Readings are recorded as foot per minute (fpm). 


I=~ 1/1 IQ z fpm (mean) 

Mean M2 +1. 20% 

Uplimitm-ipmm 

Lower limit 4~Rfp)In. 

Axe alireadingswithinthe allo~wable limit X-Yas _U 

Test technician -j 

Date of test 9/14L129 


Performa alrdistribution test on 2nd REPA fitr bank (downstream) at 1500 CFM per fiter, per ASUEN5 10- 

1989 with toe inlet, combination, sa outlet test sections in the "operating "mode, 

Air distibution tolerance per ASNIE N5 10- 1989 equals 4--20%/. 

R~equired CFMv at test NMD~bothi filters) 

Actual CFM at test 2W (bolh fiters) 

Velocity ustrWnent TST 1650 Air Velocid Me 

Serial number 4707A 

Docnxnent velocity readings on chart 

TOP 

Bottom 

NOTES-. Air distribution readings were taken with the inlet, combination, audoutlet test seotiLns in the 

"operating". Allireadings were taken through sample ports located downstream of the 2nd EPA f~lter bank 

on the I{BPA filter housing. Readings ame recorded as feet per minute (fpm). 

Page 13 

D

703RT. 973 

BATH. NC 27808 

TBL.: 252-923-2911 

FAML 252-923-6931 

Total a V loct -readings divided by the mmibar of ieadigs 

i2Qim 2Qpm.(me=n) 

Tipper limit 22.Q fP= 

Lower limit 4801 im 

Aie all readings witIn the allowable limit? Xyes _no 

Test 

Date Of test 911AL 


perform air dimibutioa test on 2nrIHEpA finter hank (downstream) at 1500 CFM per Nlter, per ANS/ASIM 

1451671980 with the ilet combination, and outlet test sections inx the "operating " mod& 

Air distribution toleanoe per ) ~sIIASN3 NSIO-1980 equals +/9- 20 0 h. 

Docun2±velocitY readings in feet Per minrute (F~bM on chart 

600 590 610 590 D 0 

600 600 0 

60D 610 650 600 

Required, CFM at test 3M (both Miters) 

Actual CFM at test 2(both 11tex4) 

Velocity instrument S160ArVlntMer 

Senal monnber 4707A 


Page C-129 

"operating. All reading$ -were taken through sample Ports located do wtream of the 2nd H~pA filter bank on 

c mbiain ( f n ultes et01 z 

NOTouSn .A' 

the IMI A ffiter hosig.Radings are -recorded as fefctpr iluty ib 

page 14

7D13 RT. 92B 

13ATH, NC 27808 

TEL: 252-923-2911 

FAX 2.52-923-6931 


fi 1 fpmn (mnean) 

Mean AU +1- 20% 

Upper limit 2M~ fpM 

Lower limit 484 fpmn 

Are all readings within tke allowable limit? Xyes _ _no 

Test technician______________ 

Date of test9148 


Page C-130 

Objective 9 

Fince aMHBA fiterin a single Wide HrA filter housing that has been setup for a conventional aerosol leak. 

tost (see figure no. 2), Perform aerosol leak test and documnent results, Test flaw at 1500 CPM. 

Downstream percent 

concentration reaings 

of HEPA filter 

* 0.01 

LI 

kequired cFm atost I 

Actzal CFM at test 4 

Photometer infr, All 

Photometer model no. IA2-M 


Aerosol generator model no, n .5 

Aerosol type b*-Alpha leIn 

0.01 

NOTBS: Aerosol was irniected into the inlet of-the-duotwork. Downstream sample was taken a minimium of 

ten duct diameters -downstream of the H"SPA filter (see figure no. 2). The "black dot" indicates where the hole 

is located during the test, The upstream. cqncenwradon readings were 100% when using the 100% scale ofthe 

photometer. The leak is expressed in a percentage of the downstream photometer reading to the upstream 

Photometer reading. 

The following conditions apply to the remainder of the teslinr. 

(1) The leakc is expressed in a percentage of the-downstreanmphotomneter reading to the upstream photometer 

reading. 

()The HEPA filter that was used in the single wide conventional aerosol leak test was removed and placed in 

the multi-wide test sectionlfilter housing system 

Pagoe15

F6"er IA MA 

7013 XtT. 92E 


TEL: 252-923-2911 

FAX. 252-923-6931 

Objective 9 (contiued) 

Perfonn aerosol loak test orithe 1stHBPAfaer bank (BMPA #1) trough the inlet and omnbination test 

sections. Test flow at 1500 CPM. Documet results. 

HEPA I HIEPA 2 

Rtequired CFM at test flQ(both fiters) 

ActulW CFM attest 28592 (both filers) 

Photometer m~fr. Anl 

Photometer model no. T2A2f 

Photometer serial no. IM2 

Aerosol generator model no.- DA* 

Aerosol type Roiv_-AbIlia-Ol 

Concentration readings 

downstream of HEPA #1 through 

test section 

0.01 

0.01 

0.01 

0.01 


Page C-131 

istHiEPAbank(lstHBPAfllter): 'tearslijcinprsa h iKttscin h e.cmiain 

* ~NOTES: Aerosol was injected into th eooneto ort onteaine testae e trouh the ntrmbiain 

and outlet test sections wareC in the !,test mode". Upstream aeroso rea wa00/ taken ousig the ujDKsc'anl 

*sample ports on the inlet test section, Upstream~ concentration readings wr 0%we ~igte10 cl 

on the photometer. Downstream Teadings Were taken throu~gh the downstream sample Port located on the 

combination test section, lVehind the leakingfitur only. The "'black- dor~ indicates where the hole is-located 

during each test 

Page 16

__ 

W 

7013 xT. 92B 


TEL: 252-923-4911 

!FX252-923-6931 

objective' R (continued) 

perform aerosol leak test ort the IstH.BPA filter bank WHBA #.2) through the inlet Ind combination test 

sections. Test flow at±15D0 CF. Dacunent results. 

HEPA I H3PA2 

Concentzation readingS 

downstream OfMBPA #2 through 

the teot section 

0.01 

1 0.01 

Required CFM at test Mi (both filters) - - 

AotWs C7M at test =5 (both f flters) 

Phtmtrmfr- All 

Pooeamodelzo, MfA-ZE 

Photometer serial no.= 

Aerosol generstormodelno. TDA-S 

Aerosol type ElQlYn-k- 

1 st REPA bank (2nd EVA flter): 


Page C-I 32 

* .NO~S: erosol wa injeetedinto the aerosol injeotitm ports on the inlet test section. Teilt oibntei 

and, outlet test sections were in the "it mode". Upstream Aerosol reading w~z taken through the upstram 

,a'eports on the Wnettest section. *Upstream. concentaflon radig pwere 100% whenuin he10 

* ~scale on th phtmeeI 

&ontemtdnBW- 

re tWk through the downstream sample poxt located on the 

combination test section, behind the leaking filter only. Thle '.1black o"idctswee h oei oae 

during eaoh test 

Pape17

Rautkn /~&Fi 

7013 RT. 92E 


TEL.: 252-923-29211 

FAX: 252-923-6931 


perform aerosol leak test on the 2nd HEPA filter bank (HEPA #1) through the combination and downstream 

test sections. Test flow at 1500 MLIA Document results. 

EWA 1 EHEPA 2 

Concentration readings 

downstream of HEPA #1 thiroughi 

the test section 

~ 0.01 

Required CFM at test (othifliters) 

Actual CFM at test 2M. (both filters) 

Photometer M&. AUl 

Photometer model nio. T 

Photometer serial o. =32 

Aerosol generator model no, TDA-SA 

Aerosol type i'olv-Alo'h--efif 

0.01 

0.01 

0,01 


Page C-1 33 

2nd HEPA bank (1st HEPA Miter):. 

NOTES: Aerosol was injected into &he aerosol injection ports on the combination test section. The inlet, 

combination, and outlet test sections were in the "test mode'. Upstream, aerosol reading was taken through the 

u pstream samople ports on the comtbination test section. Upstream concentration readings 'were 100% when 

using the 100% scale on the photometer. Downstream readings were taken thirough the downstream sample 

port located on the downstream test section, behind the leaking fIter only. The "black dot" indicates Where the 

hale is located during each test 

Page Is

7013 XT. 92H 

BATS, 'NC 27808 

TIM: 252-923-2911 

FAX: 252-923-6931 

*Objective 9 (contineti 

Perform aerosol leek test on the 2nd BEPA filter bankc (HEI'A #2) through the combination and downstream 

*test sections. Tedt flow at 1500 CFM. Document results. 

IMEA 1 HPA 2 

Required CFM at test MQ~ (both filters) 

ActmuaM at test 25 

Photometer nif. AUf 

photometer model no. M -2 

Photometer serial no. 2IM5 

Aerosol generator model no. MfAS-A 

Concentration redins 

downstream of HBPA #2 thrrough 

thetatbSection 

0.01 

0.01 


Page C-134 

2nZxd EPA bank (2nd EEPA filter): tearslijcinprso h obnto etscin h lt 

NOTES: Aerosol was injected intothaeooinetopotontecmitonesscin.TeIet 

* combination, and cutlet test sections were in the "test mode. Upstream. =rool reading was taken through the 

upstrn sample ports on the combion test secto. Upstream. concentration~ readhng were 100% when 

* using the 100% scale on ft~ pbptometer. Downsteam readings wore taken through the downatrei= sample 

-ptort located qnthe downsiroarri test section, behind the leakcing filter only. TheL ".bladk dof indicates -where the 

hole is located during =4chtest 

ObjeetIVe 9 (continued) 

Compar the downstream concentration readings from the Ist HEPA filter bank (HEPA fiter no.1I & 2)and the 

2nd BBPA filter bank (BEPA filter no. 1 & 2) to the conventional aerosol leak test fore itgle wide HEPA 

housing. 

. Page 19

7013 KT, 928 

B3ATY4 NC 27808 

TEL: 252-923-2911 

FAX: 252-923-6931 

Tolerance requires that test section concentration readings are within +15% of single wide filter housing 

conventional aerSol leak test 

Are all readings ac ebe X-'O5 .no 

Test techniia ,2' 

Date of test 9/09/99 1 


Page C-1 35 

In conclusion, the test proved that the Flnders/CSC in-place test sections meets the requirements of air aerosol 

uimfo~rmity. and air distribution of A2NSIAShVE NSJl l9S & ASIMNS510-1989. V4=i performning an aerosol 

leak test on a HEPA fllter, the FlandeWsCSC in-place test section will detect a failed HEPA filter as well as a 

conventional aerosol leak test, 

Testpersoialfled 

AistonDunbar, LevelmIIN45.2.6 (1978) 

Tony Chrifmon, LevelII N45.2.6 (1978) 

JohnMw~nsFlanders/CSC Q-6- Manager 

REFERENCES: 

* ANSL'ASMEN45.2,6-197 ......... Qualification of inspection, Examination, and Testing Personnel for 

0 

* 

Nuclear Power P'lants 

ANSIIASIMN5. 0-1980 ............ Testing, of Nuclear Air-Treatmaent Systems 

ASMBN510-1989 ................... Testing of Nuclear Air-Treatment Systems 

) NDUSTRIAL VENTILATlON HANDBOOK-18TE EDITION.A Manual of Recommended. Practice 

PLM.IDERSICSC FILENAME 

2F:\USERkWh\WFD0C\R&kl5OO)CPM 

Page 20


Page C-1 36 

PRENM TECHNOLOGY, INC. Projeet No. -- 006765.0.000 

(VRF MIR 

%w~fThnoogy 

rlS -242-A Evaporator Ki Exhanast 

Ventilation Systemn 

FACTORY ACCEPANCE TMS PLAN 

Contrct .06 

N..________ 

EPP-SEC-36062 

Spec No. Rev 0 

Attachment 6.22


Page C-1 37 

Twin City Fan, Inc Test Procedure and Report has 

been removed from this report and relocated in VI 

File 50676 (See Supplement 10)

PRiEMIER TECHNOLOGY, INC. Project No. 006765.0-000 


Page C-1 38 

V WRP S - 242-A Evaporator 1(1 Exhaust Contract 40167 

~~IiL~hrA~gx; ~Ventflation System No. RPSE-66 

FACTORY ACCEPTANCE TEST PLAN Spec No. Rey o 

Attachment 6.23

Engineer. Y~- sc= Io -do I Iae~- 

......... 

j a A, I 1 

4-- - 

- 

4- 

J. 

L 

i~sfJ~r g~ I I 


Page C-1 39 

.,..

Engineer: Y-3- l Job: ~c ~~~ Date:~ 

-~~~~ 

Ls'na 

.z1. 

J. 

I 

k L 

U d Au - * 

ILL 

II- 

4- 

T T 

-.. 

'~~.......-.. . 

~I2Li~i I~.~T~§ 1 . 

I 


Page C-140 

V 

_k'6

Eniner -OY- ~u!T1 Jb-6 e-- Date;~ ~-5- 

a 3 3jW Nq .~ R-"~~*~. 

T ~ I 

A 

F" 

T~ 

4 1'-TT~ '~~ 

* 

I ~TL 


Page C-141 

a 

V


Page C-142 

CaI 

o2fl - 

wp 

zz

00 

000 

CuJO 

u 

-1Id-t)I 

-J.Kld-1)I 

z 3.1 

---------------------------------- 

a) ZpJ.o"-) 


Page C-143



Page C-144

Tchnolog9y, Test #: 11-1445 



Page C-145 

Pro' ect Descrintin:n 

Premier Technology, Inc. Project #: 

client P0 #: 

Date of Test: 

Test performed By & Cert. Level: 

Witnessed Bx: 

Procedure Number and Rev: 


item ID or Serial Number: 

Pressure Gauge Serial Number: 

Cal Date and Due Date: 

Pressure G~auge Range: 

Pg I of 1I( 

Washington River Protection Solutions 242-A Eaorator KI 

6765 

N/A 

3/17/11 

Caleb Killian Levie I eV 

Paul Mcbride 

TP 1.7 REV 5 

FLOW 

242-A Eva orator Ki 

PTI-378 

6/14/10-6/14/11 

0-30 IN HG 

Pressure Gauge Manufacturer: 

Pressure Gauge Model: 

DWYER 

DP GW-00 


23.8 in H2O* 

Desig Pressure: 

18.96 IN H20 

Tracer Gas Used: 

AIR 

Leak Solution Manufacture /Brand Swagelock/ Snoop/ MS-SNOOP-GAL 

Name / Part Number: 

Start Time: 

2:40 PM 

End Time: 

3:15 PM 

Tern rature Gauge Serial Number: PTI-397 


Tempe-rature Glauge Range: -58 DEG F TO 2000 DEG F 

Temperature Gauge Manufacturer: Coo er-Atkins Corp 

Ternperature Gauge Model: TD2000-01 

Avera e Ter perature Dunin Test: 51 DEG F 

Results of Test: Acceptable U-cceptable (x 

Sketch the method or technique used below: 

lain Below) 

Comments: *This pressure mandated by FAT test step 7.4.4. 

This inspection satisfies steps 7.4.4, 7.4.5, 7.4.6, and 7.4.7. 

Form n-l1.7-1, Revision 0, 3/6/08

PREMIIER TECHNOLOGY, INC. 

Rate of Decay Test Report Test #: 11-1569 

Isolation Barrier Identification: 242-A Evaporator KI Exhaust Ventilation System 

Test Equipment 

Manometer/Pressure Gauge: S/N: PTI-378 Calibration Due: 6/14/11 

Barometric Pressure gauge S/N: PC30121A71 Calibration Due: 6/22/11 

identification 

Thermometer S/N: PTI-584 Calibration Due: 11/12/11 

Test Parameter 

V =Volume of System to be Tested 1949 cubic feet 

At=Total Test Time: 15 mini 

P= Required Test Pressure -23..7 -inH2O 

Convert Specified Acceptance Value (SAV) into CFM using the equation below: 

SAV= 0.O0ixV SAV 0.001 X 1949 SAV= 0.0325 -CFM 

60 mm. 60 min. Max.Permissible Leak 


Page C-146 

Test Readings 

TIME Start Finish At =tf A. 

(Mn)7:44 AM 7:59 AM 15 

TEMP. Start Finish 

(OF) 

31.3 +459.7=Ti 31.7 +459.7 Tf 

MANOMETER/ (Pim) Initial (Pm) Final 

PRESSURE GAUGE 

(Pm) -24.3 -24.0 

(inl{ 20) 

BAROMETRIC Initial =PiB Final =Pf 

PRESSURE (PB) (mug) 25.59 25.59 

TP-l.15.6765 Rate of Decay Test for 6765 Rvson 0 

1lof 2 /

PREMEER TECHNOLOGY, INC. 

CalculationsHgt 

be 

1. R 2.Deterniie Pi & Pf (Convert from inches W.G. and IN H ol/ 

53.35 pi= Pim x 5.204 + AiB x 70.73 Pf = Pfn x 5.204 +. PfB x 70.73 

p 

f 703 

(Gas =-23x5.0+259x707 

Constant p~= -2. .0 55 07 f=-24.0 x 5.204 +I 25.59 x 70.73 

for Air) Pi (-126.4572) + (1809.9807) Pf =(-124.896) + (1809.9807) 

P. 163,523 pf =1685.047 


Page C-147 

3 .Calculat Ie Average Leak Rate of Housing using the following equation: Steps A-E 

(Pf' V (1683.5235 1685.0847 1949 

Stp . TI Tf ) R At (0.075) SeB.=k 491.0 491.4 (53.35)(15) (0.075) 

Step C. =(3.4288 - 3.4292) 1949 Step D. = (-.0004) (32.4732) 

60.01875 

Step E. = -Q029EM 

SAYV= 0.0325 C-LFM 

If Qis less than SAy. permissible leakage, housing or system is aceptable.....~. .. 

Test Results 

Test Duration Average total leakage Accept/Reject Test Date 

15 MIN. 

-0.0129 CFM ACCEPT 4/4/11 

Test Performed by: 4 Certification! Level Date: 

Print Caleb Killian 

Signature J 1 

Level 11q111 

Test Witnessed by: Paul Mcbride Date 4/4/11 

TP-115.765Rate of Decay Test for 6765 

2 of 2 


.

premir Im.Bubble Tecnolmy 

Project Des 'tion: 

Premnier TechnolOgY, Inc- Proed #: 

client PO #: 

Date of Test: 

Test erormed By & Cert. Level: 

Wtessed By 

pcedure Number and Rev' 

Test Method or Techliue: 


DePressure peSraNub: 

Trassure Gas Used:e 

Leak Solution Manufacture fBrand 


Start Time: 

End Time: 

T erature Gau e eilNmer. 



Page C-148 

Leak Test Procedtre- 

Av e T erature Durin Te 

Results of Test: Ace eU- ale li eo 

Sketch the method or techni e used below: 

Location of Leak 

Repair Method 

Co ents: 

* ITP1.7 Bubble Leak Test procedure Revision 5 

UNCONTROLLED IF49HARDCOPY F ORM

-Y 

VIC~ 

S TE tZ-' 

-JJCd-TN 

-h1ad-TNl 

___ 

0 z_ - 

Ile. 

- --- - 

.0 c 

* 

_ E _D 

- a 

' 

. 

_ 1A _ ll 

_ _ 

IJOA ~~ ~ ~ h ~-s . 

4 jJ14 

cz"-, ISv. 

_ Jo~IL~ ~z - - 

E0 

4o*vIL 

WA 

- - ZZ 

N.4 


PAge C-149 

-

It)) 

U)1X 

IT- 

602 

-iKid-1N 6 

EM 

E:.U 

-zJio 

coJOH7 4- - -- 

caa I 

60 

m IB' 

RPP-RPT-49670 Rev a 

Page C-1 50


RPP-RPT-49670 Rev 0, 

Page C-1 51

Te Chnolog-y, ifC. Test #: 11-1539 



Page C-1 52 

Pr~et ifon:Washington 

Dscr 

Pg 1, of 1 

River Protection Solutions 242-A Evaporator K1 

Premier Technolo ,y Inc. Project #: 167651 

Client PO #: 

N/A1 

Date of Test: 

13/30/11 

Test Pei fonned By & Cert. Level: Caleb Killian LII 

Witnessed By: 

Paul Mcbride 

procedure Number and Rev. TP 1.7 REV 5 


FLOW 

~ 

Item ID or Serial Number: 

Pressure Gauge Serial Number: 

Cal Date and Due Date: 

Pressure Gauge Range: 

Pressur e Gauge Manufacturer: 

242-A Evaporator Ki tadminandb 

No pressure gauge used. Pressure was seanmitiedb 

setting fans to 19,500 SCFM speed per the instruction given in 

FAT Washington River Protection Solutions 242-A Evaporator 

KI Exhaust Ventilation Systems Factory Acceptance Test Rev 

puae 9au e FL K 

Tererasure Gauge Ma uatrr Model: 516. Temoee 

rests ofrestur: Aresue N/.tuabl U-c ce tabeai8Blo 

Comments *Se Thiiresest NC-111 satisfie the reureet ot12 71.2ad7.03insaedFT 

Time:I 

w0 

Form 

4M 

R2vsio 0,3//0

goo z9 

c 

C O 

0I0 

-4* 


Page C-153

V8X 

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fls 

OT 

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* E _____ 

ro 

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ieox 

EI*) .'03 

j- -. JdT 

/E 

n 0 

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up: 

60S 

906 

NQ I 


Page C-1 54

S. ~ I. t~ A~ 

lAO% 

'poll 

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-. Lad-t 

110dS tM A 

~~:E 

- - tZ 

~apcy o 

-hC-Q 

~BN I~bc 


Page C-155

*4n 

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, ( bi 


Page C-1 56 

'm- ~ ~ - - - - - - 

0 * /, 

E~ VOA :-~o~ 

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6k 00Eli 

a & t



Page C-157

RPP-RPT-49670 RevO0 

Page C-1 58 

Technlogy.~flC.Test #: 11-1540 

Bubble Leak Test Report Pg 1 of 1I C 

Pro-ect Descri ti on: Wsnon River Protection Solutions 242-A Eva orator K1 

Premier Technology, Inc. Project #: 6765 

client P0 #: 

N/A 

Date of Test: 

3/30/11 

Test Performed By & Cert. Level: Caleb Killian Level 11 16" V& 

Witnessed By: 

Paul Mcbride 


TP 1.7 REV 5 


FLOW 


242-A Evaporator Kl 

Pressure Gau e Serial Number: No pressure gauge used. Pressure was se and maintained by 

Cal Date and Due Date: setting fans to 19,500 SCFM speed per the instruction given in 

Pressure Gauge Range: FAT Washington River Protection Solutions 242-A Evaporator 

pressure Gauge Manufacturer: KI Exhaust Ventilation Systems Factory Acceptance Test Rev 

ae-o 


Start Time: 

2:3 5PM 

End Time: 

3:03 PM 

Ternperature Gauge Serial Number: PTI-584 

Cal Date and Due Date: 11/12/10- 11/12/11 

Temperature Gauge Range: -127 to 600 DEG C. 

eraerature Gauge Manufacturer: IFLUKE ,' 

Temperature (Ian e Model: 5111I Thermometer 

Avera e Ter erature Dun et *46.5 Deg. F. 

Results of Test: Acceptable [1Un-Acceptable ( lain Below) 


Comments *See NCR 11-171. 

This test satisfies the requirements of steps 7.15.2 and 7.15.3 in stated FAT. 

Form TP-1.7-1, Revision 0, 3/6/08



Page C-1 59

Technogy. I1C, 

Test#: 11-1538 



Page C-160 

Pg 1 of 1 

Pro'ect Descrinti On: 

IWashin onRiver Protection Solutions 242-A Evaporator K1 

Premier Technology, Inc. Project #: 16765 

Client P0 #: 

N/A 

fDate of Test: 

13/30/11 

Test Performed By & Cert. Level: Caleb Killian Level HIee 

Witnessed B e: 

Paul Mcbride 


TP 1.7 REV 5 


FLOW 


242-A Evaporator K1 

Pressure Gauge Serial Number: No pressure gauge used. Pressure was set and maintained by 

Cal Date and Due Date: setting fans to 19,500 SCEM speed per the instruction given in 

Pressure Gau e Ran e: FAT Washington River Protection Solutions 242-A Evaporator 

Pressure Gauge Manufacturer: K1 Exhaust Ventilation Systems Factory Acceptance Test Rev 

Pressure Gau e Model: 6. 


Desig Pr essure: 

Pressure 18.96 IN N/A. 1120 Actual SCFM 19,F5.166 


AIR 

Leak Solution Mnftue IBrand Swagelock/ Snoop! MS-SNOOP-GAL 


Start Time: 

1:00 PM 

End Time: 

1:15 PM 

Tem erature Gauge Serial Number: PTI-584 

Cal Date and Due Date: 11/12/10- 11/12/11 

Tem nerature Gauge Ran e: -12-l7 to 600 DEG C. 

Te erature Gauge Manufacturer. FLUKE 

Temperature Gauge Model: 51 HI Thermometer 

Avera, e Temperature During Ts: *25DG F. 

Results of Test: Acceptabl UnAccentable (Ex lain Belo 


Comments: *See NCR 11-171. 

This test satisfies the requirements of step 7.16.2 in the stated FAT. 

Form TP-1.7-l, Revision 0, 3/6/08 

Q

4)4 

V m 

0 

-x 

.SEn 

cm- 

E 


Page C-161


Page C- 162 


?~AIE WRPS -242-A Evaporator Ki Exhaust Contc 

Te'cchnolloiy Inc. Ventilation System NO. 6 

FAC~TORY ACCEPTANCE TEST PLAN Spec No. "RSeC-30 

Attachmnent 7.18 

115

AIRFLOW CAPCITY 

AND 

- - -DISTRIBUTION TEST, 

NUCON Procedure 12-101 Revision 7 

UNCONTROLLED COPY 

This is an uncontrolled copy and 

will not be updated wit additions 

and / or revisions- 

NUCON international, Inc. 


Page C-163

NUCON Procedure 12-1 01 Rev. 7 

Original Issue Prepared By Revised By Approval By 

01 April 198l ________ zX____ _.4_Z 

R, G. Cruickshank K. M. Fleming C. L. Karn 


16 Dec. 82 W* 'W 4 ,R SMOff H. l 4C 

All Pae John Hunt R. R Sommer C. L Kerm 


01 Feb 84__ _ _ _ 6'Sd# Zoei 

Set 5.3 & 5.4 .1. W. Jacax R G, Cruickshank Mv. J. Toeppe 


26 April 85 _ _)._54* 

~All Pages K. 0. Jackson R, R. Sommer 11 E. D. Shepherd 



Page C-164 

16 Oct. 87__ _ _ _ 'SOMIt_ _ _ _ 

Ail Pages K. D. Jackson R. R. Sommer 11 S. A. Fratlanne 


4Feb. 87 5, WS&X ) .1A9Mw 

All Pages E . M. Banks K. D, Jackson S. A. Fratlanrie 


July 93 _ _ _ _ 

All Pages W. 0. Wikaff J. I. Otermat P. E. Kovach 

Prepared By Validated By ,, 6 7 proval 


April 2007 Even. R. Solarailo, ric, M. Banks Paull E. Kovach 

All Pager./,- 

DateDateDate 

117

NUCON Procedure 12-101 Rev. 7 

1.0 SCOPE 


Page C-165 

1.1. This procedure is utilized to perform airflow capacity and distribution tests on 

air cleaning / treatment units and systems. Airflow capacity tests are 

performed for acceptance testing arnd for surveillance testing. Airflow 

distribution tests are performed for acceptance testing of the original 

installation and following modification, or major repair of the air cleaning 

system. This procedure has been developed to meet the requirements of 

Reg. Guide 1.140,1.52, ASME N-510, AG-I and complies with the quality 

assurance requirements of NUCON 045. 

1~0 APPLICABLE DOCUMENTS (current revision unless noted otherwise) 

2.1. NUCON 045, Quality Assurance Program Manual. 

2.2. NUCON Procedure 7QA-1 81, Evaluation and f or Reporting Procedure in 

Compliance with 1 OCFR2I. 

2.3, NUCON Procedure 7QA-23Q, Collection, Storage, and Maintenance of 

Quality Assurance Records. 

2.4. NUCON Procedure 12-225, Training and Qualification of Personnel to 

Perform ANSI N51 0 Testing. 

2.5. NUCON Procedure 12-255, Visual Inspection of Nuclear Air Treatment 

Systems (as applicable). 

2.6. NUCON Procedure 12-307, Airflow Correction Factors for Correcting 

Measured Velocity or Volumetric Flow Rate to Standard or Actual Conditions. 

2.7. ASME (ANSIIASME) N.-61 0, Testing of Nuclear Air Cleaning / Treatment 

Systems (applicable revision). 

2.8. ASME AG-I, Code on Nuclear Air and Gas Treatment (applicable revision). 

2.9. NRC Regulatory Guide 1.140, (applicable revision) Design, Testing, and 

Mainteniance'Criteria For Normal Ventilation Exhaust System Air Filtration and 

Adsorption Units of Light-water-Cooled Nuclear Power Plants (as applicable). 

2.10. NRC Regulatory Guide 1.52, (applicable revision) Design, Testing,- and 

Maintenance Criteria For Post Accident Eng ineered-Safety-Feature 

Atmosphere Cleanup System Air Filtration and Adsorption Units of Light- 

Water-Cooled Nuclear Power Plants (as applicable). 

2.11. American Conference of Governmental Industrial Hygienists (ACGIH) 

Industrial Veptilation, Section 9, (applicable revision). 

Page 1 ofII 

lie

NUGON Procedure 12-101 Rev. 7 

2.12. Attachments: 

2.12.1. NUCON Form FB-07A, Rectangular Duct Traverse Report. 

2.12.2. NUCON Form FB-07B3, Round Duct Traverse Report. 

2.12.3. NUCON Form FB-08, Duct Traverse-Zone Summary. 

2.12.4. NUCON Formn FT-I 3, Acceptance for In-Place Testing. 


Page C-166 

2.12.5. NUCON Form FT-16, Airflow Capacity and/or Distribution Test Report 

Form 

2.12.6. NUCON Form FT-21, Raw Data Grid. 

2.12.7. NUCON Form FT-28A, Duct Traverse and Calculation Form 

(Uncorrected). 

2.12.8. NUCON Form FT-28B3, Duct Traverse and Calculation Form 

(Corrected).. 

3.0 SUMMARY OF METHOD 

3.1. This procedure provides a method in which to quantify the volumetric airflow 

rTatp and / or the air~distribution within a duct or air cleaning / treatment 

system. For airflow capacity, this is accompli Ished by traversing, at 

predetermined points in the duct, with an appropriate airflow measuring 

device (e~g., Pitot tube and manometer, heated wire anemometer, etc.). 

These readings are averaged and then multiplied by the duct area to arrive at* 

the volumetrip airflow ra Ite, in cubic feet per minute (6frn). 

3.2. For airflow distribution, the face velocity of the: individual components is 

obtained by using an appropriate airflow measuring device (e.g., heated Wire 

anemometer, rotating vane anemometer, etc.). These readings are averaged 

and the highest and lowest readings are compared to the average reading. 

4.0 DEFINITIONS, 

4.1. HEPA filter High Efficiency Particulate Air filter. 

4.2. Pressure drop, design clean - The minimum housing component pressure 

drop in an air cleaning I treatment system. This pressure drop is based on 

newly installed components. 

Page 2 of 11


4,3. Pressure drop. desicin dirty - The maximum housing component- pressure 

drop in an air cleaning I treatment system. This pressure drop is based on 

the calculated maximum individual component pressure drop, assuming 

maximurbn component loading. 

5.0 EQUIPMENT 

5.1. Pitot Tube.(as required) 

Range: N/A 

Accuracy: N/A 

5.2. Manometer or equivalent (as required) 


Page C-167 

Range: As required, (minimum resolution of 0.01'inches w.g.) 

Accuracy: Per project specifications or applicable revision of ASME N51 0 or 

AG-I. 

5.3. Rotating Vane or Heated Wire Anemometer, or equivalent (as required) 

Range: As required 

Accuracy: Per project specifications or applicable revision of ASME N510 b r 

AG-I. 

5.4. Thermometer (as required) 

Range: 32OF to 120OF 

Accuracy: ±1 0 F 

5.5. Psychrometer (as required) 

Range: 32OF to 120OF 

Accuracy: ± 1 0 F 

5.6. Barometer (as required) 

Range: As required, (minimum resolution of 0.10 inches of Hg) 

Accuracy:, Per project specifications or applicable revision of ASME N51 0 or 

AG-I. 

Page 3 of 11 

120


80 SAFETY PRECAUTIONS 

6.1. Due to the nature of -the testing. environment, safe work practices shall be 

observed during all phases of testing. As a minimum, NUCON and site 

specific (as applicable) SAFE work practices shall be followed. 

7.0 PREREQUISITES 


Page C-168 

7.1. Personnel performing this procedure shall be, as a minimum, QUALIFIED as 

a Level 11 in accordance with NUCON Procedure 12-225. 

7.1.1. NUCON Level I personnel may perform portions of this procedure under 

the direct supervision of a NUCON Level 11 or ill. 

7.2. AF the unit being tested fails to meet the prerequisites of this procedure, AND 

I OR the client elects to waive any of these prerequisites, it shall be NOTED 

on Form FT-1 3. 

7.3. A visual inspection, shall be initiated per NUCON Procedure 12-255, as 

applicable, prior to this test, 

7.4. CONDUCT an inspection of the system to ensure that it is ready for testing. 

RECORD any deficiencies on Form FB-08 or FT-16 and inform the Client. 

7.5. The Client SHOULD NOT allow any system alignment changes for the 

system being tested or any system changes that may affect the flowrate of 

the system being tested. 

8.0 PROCEDURE 

NOTE: These steps may be performed out of sequence as deemed necessary by 

the NUCON Test Engineer to facilitate performance of this procedure. 

8.1. Airflow Capacity 

8.1.1. Surveillance Testing 

8....SELECT a position in the duct work for a Pitot tube or anemometer 

traverse where the airflow is steady and, if possible, where no flow 

disturbances occur for at least 8 duct diameters upstream and 2 

duct diameters downstream of that position. If this is not possible, 

SELECT a position that is thought to provide the best readings for 

the given conditions. IF airflow capacity is to be determined by 

using the component average velocity, refer to Section 8.2. 

Page 4 of I1I 

121


CAUTION: VERIFY that there is no internal obstruction that may 

interfere with the accuracy of the reading. IF internal 

interference is noted THEN consideration should be given' to 

relcatng hetraers pint AloVERIFY that the duct is 

not internally insulated, if it is, then take this into account in 

the duct area calculation- 

8.1.1.2. MEASURE the internal duct size and RECORD on the appropriate 

Form FT-28 or F13-07. 

8.1.1.3. CALCULATE and MARK the Pitot tube or anemometer probe at 

the appropriate divisions, as determnined by Section 8 of ACGIH 

Industrial Ventilation, or other traverse guidelines (e.g. Log- 

Tchebycheff) for the duct traverse being performed. 

8.1.1.4. VERIFY that the system under test is properly aligned and 

operating to the clients specification. 

8.1.1.5. MEASURE and RECORD the velocities or'velocity pressures as 

applicable, on Form FT-28 or F13-07. 


Page C-169 

8....MEASURE and RECORD the duct static pressure on Form FT-28 

or FB-07, as applicable. 

CAUTION. Exercise caution to avoid evacuating the manometer 

of Its fluid or, over (under) pressurizing the test 

I instrument. 

8.11.61.When OBTAINING the duct centerline static pressure for 

a NEGATIVE pressure system, REMOVE the total 

pressure line from the Pitot tube. 

*8.1.1.6.2. 

When OBTAINING the duct centerline static pressure for 

a POSITIVE pressure system, DISCONNECT both the 

total pressure and static pressure lines from the Pitot tube. 

RECONNECT the total pressure line to the static 

pressure port on the Pitot tube. 

ffNT:Refer to NUCON Procedure 12-307 for additional information onl 

NOE:applying correction factors. 

8.1.1.7. IF corrections for density are to be taken into account, MEASURE 

the dry bulb temperature and center line static at the traverse point, 

inside the duct. Also, obtain the local barometric pressure. 

RECORD this data onto Form FT-28B or F13-07. 

Page 5 of 11 

122


8....IF NO corrections are required UTILIZE Form FT-28A~or FB-07. 

8.1.1.9. PERFORM all calculations in accordance with Section 9 of this 

procedure and the appropriate Form FT-28 or FB-07. 

INOTE: 

This section is performed only following original installation, 

modification, or major repair of the air cleaning system.I 

8.1.2. Acceptance Testing 


Page C-170 

8.1.2. 1. SIMULATE the design clean filter resistance.(this, Is not applicable 

If all internal components have been installed in the air cleaning 

unit) as specified by the project specifications. 

WARNING: Unstable fan operation is indicated when one or more of the 

following conditions exist; fan surging, changes In fan noise, 

changes in filter resistances, etc.J 

8.1.2.2. CHECK for stable fan operation over a fifteen-mInute period at this 

filter resistance. IF unstable fan operation is noted at any time, 

IMMEDIATELY REDUCE the filter resistance to the point at which 

the fan is returned to a stable condition OR STOP the fan. 

8.1.2.3. PERFORM airflow. measurements in accordance with Sections 

8.1.1.1 through 841.1.9 of this procedure, as applicable. 

WARNING:The following step may create an unstable fan condition that 

WARNNG:could cause d amage to the fan and to the surroundingI 

8.1.2.4. CREATE an artificial filter resistance of at least 1.25 times the 

design dirty filter condition or as required by the project 

specifications. 

8.1.2.5. CHECK for stable fan operation over a fifteen-minute period at this 

filter resistance. IF unstable fan operation is noted at any time, 

IMMEDIATELY REDUCE the filter resistance to the point at which 

the fan is returnedl to a stable condition OR STOP the fan. 

8.1.2.6. -Perform airflow measurements in accordance with Sections 8.1.1.1 

through 8.1.1.9 of this procedure, as applicable. 

8.1.2.7. CREATE an artificial filter resistance that Is about 50% (midway) 

between the resistance determined in Step 8.1.2.1 and 8.1.2.4, or 

as required by project specifications. 

Page 6 of I1I 

123


8,1.2.8, PERFORM airflow measurements in accordance with Sections 


Page C-171 

- .-. .~~-----**-8.11through 8.1.1.9 of this procedure, as applicable_--- -- 

8.2. Airflow Distribution 

Tifno 

NOTE: This section is normally performed following original installation, 

modification or major repair of the air cleaning system. In addition, 

possible traverse point is available in the ducting (or lack of 

ducting) this may be used to confirm the approximate airflow 

capacity. 

NT:Care should be taken so as not toditrtharfoptentrug 

NT:the filter bank being tested. dstrtharfo ptentrug 

8 .2.1. Velocity measurements should be taken immediately downstream of the 

bank being tested using a vane anemometer, heated wire anemometer, 

or equivalent. When this is not possible, EVALUATE an alternative 

method and denote on Form FT-21. IMPLEMENT the alternative 

method. 

NOTE, For units with only one filter component in a bank, the distribution 

test may not be required. Refer to the project specifications. 

8.2.2. The MINIMUM number of readings for any given bank of components is 

ten, or as required by the project specifications. These readings shall be 

measured in the center of each component. Where less than ten 

components per bank exist, refer to the following steps. 

8.2.3. For prefilters, moisture separators, HEPA's, Type I and Type IV adsorbers 

and similar components: 

8.2.3.1. For filter banks containing fewer than 10 HEPA filters, moisture 

separators, prefilters, Type I or Type IV adsorbers, the minimum 

number of velocity readings will be 10 or as required by the project 

specifications. This will include at least one reading in the center of 

each filter component in the bank. 

8.2.3.2. MEASURE and RECORD on Form FT-21 the velocity for each 

component. 

Page 7 of I I 

124

NUCON Procedure 12-1 01 Rev. 7 

8.2.4, For Type I I adsorbers: 


Page C-1 72 

NOTE: Care must be exercised when performing air distributions on Type 

11 adsorbers. The probe of the velocity-measuring. device must be 

held exactly the same distance from the air channel on each 

reading, to help reduce wide variances in these readings. 

8.2.4.1. For Type 11 adsorber trays, the air distribution test will follow the 

same procedure as specified in 8.2.2. The exception to this is that 

all velocity measurements will be made precisely in the plane of the 

face of the air channels, in the center of every open channel, and 

not less than 10 measurements or as required by the project 

specifications. 

8.2.4.-2.. MEASURE and RECORD on Form FT-21 the velocity for each 

component 

8.2.5. For Type IlI adsorbers: 

NOTE: Care must be exercised when taking readings on the upstream or 

downstream face of the Type Ill adsorber. Some designs only 

allow for -% the normal velocity on the two outer air channels, this 

must be taken into account when readings are obtained. As in 

Type It adsorbers, the probe placement is critical and must be the 

same distance from the air channel for each reading. 

8.2.5.1. For Type Ill adsorbers, velocity measurements for the air 

distribution test shall be made in the centers of equal areas that 

cover the entire open face, not in excess of 12 inches between 

points, and not less than 10 measurements or as required by the 

project specifications. 

8.2.5.2. MEASURE and RECORD on Form FT-21 the velocity for each 

component. 

8.2.6. After all- readings are obtained, an average of all the readings is then 

calculated. This average Is, compared to the highest and lowest reading, 

and a percentage difference is then calculated. Refer to Section 9 of this 

procedure. 

Page 8 of 11 

125


INOTE: This technique should only be used when a traverse of the duct 

-- - ---- system cannot be performed. - -- 

8.2.6.1. IF a quantitative value for airflow through the unit is to be 

calculated, the velocities are averaged as in Step 8.2.7. This 

aver-age is then multiplied by the area of the bank under test to 

determine the volume of air passing through the unit, in cfm. 

9.0 CALCULATIONS 

9.1. Converting velocity pressure (VP) to feet per minute (fpin): 

9.1.1. FPM =4005 x IV- 

Where: EPM = Feet per Minute 

VP =Velocity Pressure (inches w.g.) 

9.2. Area of a duct or filter component (A). 

NOTE: When the area of a component is being calculated, only that area 

9.2.1. For a rectangular duct or component 

9.2..1.Are (F2)~ =Width (inches) x Height (inches) 

9.2..1.Areat-r144 

9.2.2. For a round duct or component 

9.2.2.1. 

Ae(p 


Page C-1 73 

Where: Tr 3.14159 

r the square of the radius of the duct or Component in inches 

Page 9 of 11 

126


9.3. Density calculation (p) 

7B+460 

Where: -p =Density of air (Rho), (Ibm IFt?) 

Pb = Barometric Pressure, (inches of mercury, Hg) 

Ps Center Line Static taken (inches w.g.) 

TDB = Dry Bulb Temperature (OF) 

9.4. Density correction factor for actual conditions(dci) 

9A. 1. dof=: 

p 

Where: p =Calculated Density from 9.3 

9.5. Average velocity (Va) 

9.5.1. V1 

Nubrof. je dIngs 

Where: Vt = Total velocity, the sum of all velocities (fpm). 

9.6. Volumetric flow rate (Q) 

9.6. 1. Q -V. xA 

Where: Q = Volumetric flow rate (cfrn) 

Vt Average velocity, from 9.5 (fpm) 

A = Area of the duct or component from 9.2 Mf 2 

9.7. Airflow distribution (% Difference From Average) 

9.7.1.. % High 

Highest Reading - Average Reading10 

9.7. 1. 1. % High = Average Readingx10 

9.7.2. % Low 

9.72. . %LO= Lowest Reading -Average Reading. Xl00 

9.7..1. LowAverage Reading 

Page 10 of 11 

127 


Page C-174

N UCON Procedure 12-101 Rev. 7 

10.0 ACCEPTANCE CRITERIA 


Page C-1 75 

10.1. COMPARE results with the project Specification. NOTIFY the client of the 

test results. Adjustments and further testing shall be performed at the clients 

discretion. 

11.0 REPORTING 

11.1. REPORT test results on Form FB-08 or FT-16. 

11.2. IF multiple tests are required due to multiple banks or failure of the preceding 

test(s), RECORD results for each test on separate applicable raw data sheets 

Forms FT-28 or FB-07, and / or FT-21 (as applicable). 

11.3. Evaluation and reporting of 100CFR21 deviations or non-compliances shall be 

in accordance with NUCON Procedure 7QA-181 (as applicable). 

11.4. Test data shall be maintained in accordance with NUCON Procedure 7QA- 

230. 

Page 1 of I1I 

128

FB-07A (Rev. 2 06/05) 

NUCON International, Inc. 

Date:_________ 

Poet 

CI RECTANGULAR DUCT TRAVERSE 


Page C-1 76 

ClientlIPlant:_______________________________ 

system: Ts o:___ 

Traverse station: Barmert Prssr o________ 

Instrument(s) I D:__Barometric:_____Pressure:___ 

Temp. DB / WB:__________ Density:_____ Correction Factor:__________ 

DUC~T REQUIRED RECORDED 

S.P. ____Tdnp.___ A, S, or M CFM _______ A, S, r CFM_______ 

Machk forintamdifsuatof and obstrctions) FPM_______FP _____%D89f 

D STANGE 

FROM PoSITION 1 2 3 4 5 6 7 8 a 10 111 12 13 

EDGE ____ 

2 

3 

8 

10 

11- - - - - - 

12- 

13- 

DISTANCE FROM 

DUCT EDGE == == 

NOTE Traft readings with air hiowing towr the obswvw. 

Remarks: 

Test Personnel Signature(s): NUCON International. Inc. 

129

FB-07B (Rev. 2 06/05) 

NUCON Internationa'l, Inc. 

ROUND DUCT TRAVERSE 

Date:_________ 

Project: 


Page C-1 77 

Client!I Plant 

;System: Ts o: 

Traverse Station:Baoeti 

Pesssure: 

Istrument(s) ID:______________________ CoaroetinPressr:__________ 

TmeaueDB I WB:_______ Density:________Creto 

DUCT REQUIRED RECORDED 

S____Temp. S,or MCFM __ _ _ _ _ A, S, or MCFM_ 

rchack for inten at InsullOn -nd obstnwiion) FPM FM____%Dsg 

NOTE: Take readings with air flowing toward the observer. 

Distance 

from 

Edge of 

Duct 

2- 

3 

4 __ 

9_ 

10- 

Remarks: 

Hoz 1-01-Suttl Number of Point' -___ 

Vert. Subtotal:,vrg:_______ 

Test Personnel Sign tre(s): NUCON International, Inc. 

130

FB-08 (Rev. 1 06/05) Dt 

NUCON InternationoIl, Inc. 

DUCT TRAVERSE-ZONE SUMMARYI 


Page C-1 78 

Project_ ________ 

Client/I Plant:_______________________________ 

System: 

SYSTEM ZONE DUCT DUCT DESIGN MEASURED I 5wATIC 

NO. NO. SIZE AREA VL CPM VEL. CFM -A ESS. 

Remarks: 


131

FT- 13 (Rev. 7 111Q5) 

NUCON Internotiorkol, Inc. 

Unit: 

Date: 

Project: 

_________ 

Clen Pan:ACCEPTANCE FOR IN-PLACE TESTING* 

Location: 


Page C-1 79 

Aceptance Test Yes - No_- Testing standard: ANSI/ASME N510-..... 

Other. 

ANSI N51 0 Test Section(s)- Sec. 5 Sec. 6 Sec. 7 Sec. 8 Sec. 9 

(circle section(s) utilized) Sec. 10 Sec. 11 Sec. 12 Sec. 13 Sec. 14 

FAirflow: 

______________________ 

Acceptance Criteria 

H-EPA Max. Leak:,________________________ 

Adsorber Max. Leak:______________ 

_________ 

Commenlts:_ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 

.*Only one (1) FT-13 needs to be comnpleted for each test series performed on each system. 

Accepted By (Signature) 

NUCON _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 

Client 

132


Page C-180 

FT-1 6 (Rev. 5,11/05) Date:________ 

SNUCON International, I'm. Project:________ 

cJ AIRFLOW CAPACITY AND I OR DISTRIBUTION TES 

client IPlant: ________________________________ 

Unit: _______________________________Test 

Test Type: Capacity____ and/or Distribution_____ 

Test LodAtldn: Duct_______ or - Filter Face_______ 


Flow Rate: Face Velocity 

No:____ 

Total_____ FPM 

P 

Specified ________MCFM, ACEM, or SCFMAvrg_____ P 

(circle one)Avrg 

Measured _______MCFM, ACFM, or SCFM Obtained Readings 

(ollrde one) Mxmm____ P 

% of Design 

Minimum____ FPM 

Minimum___FPM 

* / Deviation from Average: 

(0/6 of Design = -Measign X00) High + %____ 

Designtow -___ %_ 

Fan Stability Check: ___Sat 

___Unsat. 

DIc = (NiCctMn)-A~x.0 

%~iin ~.~n 

___N/A _________ 

Acceptance Criteria Met? __Yes No 

Notes IComments:_____________________ 



133


NUCON Internoioflal, Inc. 

client / Plant: 

instrument(s) ID: ______________________________________ 


RAW DATA GRID 


Page C-1 81 

Date:______ Time:_____ 

Project: 

Test_____________________No:____________ 

Type of Test: Airflow CapactY*. - - MutileSapl 

Airflow Distribution......... AirlAerosol Distribution_ Ohr________ 

(specify) 

Notes I Comments: ____________________________ 

Test Personnel & Signature(s): NUCON rIntemariawa, Inc. 

Velocity or Concentration 

(circle one) 

Total_______ __ 

Average 

Obtained Readings 

Maximum_______ 

Minimum________ 

%Deviationl from Average 

%High + ______ 

%Low-____ 

_ 

(MaxD cwin.) - Avg. 

Eration= 

~k. A. Reading 

If required for 

airflow capacity 

*Componient Area 

FT? 

*No. of Components 

*Bank Area 

*CFM 

FT 2 

lO


Page C-182 

FT-28A (Rev. 4, 11105) Page 1 of 2 

NUCON International Inc. Date: Time:_____ 

Proje ct:__ __ 

DUCT TRAVERSE & CALCULATION F ORM (UNCORRECTED) 

Client IPlant: _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 

Unit: __ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ Test No: _ _ _ _ _ _ 

Traverse Station:__ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 

Instrument(s) ID:_____________________________________ 

1 *Dc Width _____inches X Duct Height ______inches 

Duct Area _______In. 

C) *Dc Diameter (________inches )2 X 0. 78539 =Duct Area __________in 2 

*Check for internal insulatifon and obstruct~ons 

Duct Area (in2) Duct Area 0F2) 

144 

Total Velocity MFPM +No. of Readings ____Ave. Velocity______ MFPM 

Ave. Velocity MFPM X Duct Area ____Ft 

Notes I Comments: ____________________________ 


2 Measured CFM MCEM

E311 

FT-28A (Rev. 4, '11105) 

NUCON Inlterna~tional Inc. D ate T9e______ 

ProlJect: 

Velit 

DUCT TRIA VE R SE 1R EAD1 NG= 

a:___________esedFePeMnueMF) 

position 


Page C-183 

Page 2 of 2


Page C-184 

FT-28B (Rev. 4 11/05) Page I of 2 

SNUCON International, Inc Date: _____Time: _____ 

Project:______________ 

1J DUCT TRAVERSE & CALCULATION FORM (CORRETD 

Client / Plant: _____________________________________ 

Unit: ___________________________Test No:_____ 

Traverse Station: _________________________________ 

Instrument(s) ID: ______________________________________ 

Uncorrected Barometric Pressure =____ inches Hg (Pb) Air Temperature OF 

(D.B. /W.B.) 

.Duct Static Pressure _ _ _ _ _ __in. w.g. + 13.6 _______in. Hg (Ps) 

Actual Correction Factor (ACF) to Calculate ACFM 

AirDesit =(Pb)+ _ (Ps) =0. 

AirDesit = FD..) x 1.328 0.0_____Ibm/ft2 (p) 

(RHO~p)) 460 + ____ 

]o.075 + 0.0 (p)= _____ACF 

Standard Correotion Factor (SCF) to Calculate SCFM 

_(Pb) + rP)x53 C 

29.921 (Ps} 460 + 530 *(D.B.)J C 

177 *Duct Width _____inches X Duct Height_____ inches =Duct Area _______in2 2 

0*utDiameter( ________nches) 

X 0.78539 =Duct Area in_______2__ 

*Check for internal insulation and obstructons 

Duct Area In 2 =DutAe 2 

144 

Total Velocity _______FPM - No. of Readings =Ave. Velocity ______FPM 

Ave. Velocity ______FPM X Duct Area, F1f [F~ared CFMCF 

MCFM X ACF lActual CFM ACFMI 

MCFM _______X SCF _____Standard CFM .S~ 

Notes: 


13

RF-28B (Rev. 4 11/05) 

! ~NUCON Internioflali Inc. 

Ition 

Date:_____ 

DUCT TRAVERSE READINGS 

----- 138 


Page C-1 85 

Page 2of 2 

(Crceaprprtt:nis

FT-16 (Rev. 5,11/05) Date: Z2L , 4 2,011 


Page C-186 

NUCON International, Inc. Project: 1UQv>laAy 1+4 

ciAIRFLOW CAPACITY AND I OR DISTRIBUTION TEST REPORT 

CletPlant: IiL~ 

Unit: 6; Z L4A'OU,- Test No:4. 

Test Type: Capacity___c-'' and/or Distribution____ 

Test Location: Duc lz or Filter Face_______ 



Specified 155 00; 66!= I&0/.CFM, ACFM, o[ CLF Aveage ___ FP 

(circle one) I AeaeF 

Measured i~ iMCFM, ACFM, or A Obtained Read! s 

4 (circle one)MaiuFM 

% ofDesgn imum FPM 

Deviation om Average: 

Measured N 

%of Design= -X100 High+ ____ 

Design Low %_____ 

Fan Stability Check: _ _Sat. ~(Mccrm) -ftlO 

Acceptance Criteria Met? _..i es No 

Nte l Comments: 71L,! roaw -,~~tt a "a= aflA4JIOC4404:4 7L-4J -. 

W S'-' e rcvu' I- oparmc .~-0r . -rc-. 

Test Per onne nature(s): NUCON International, Inc. 


FB.0 7 B (Rev. 2 06105) 

NUCON Internatiofl, Inc. 

Project:.~ 

EROUND DUCT TRAVERSE 


Page C-1 87 

rmR Client / plant: 

system: . iy~e 

armti resr. -- 

Traverse Station: 

CoBaretion Frctor: 

instrument(s) ID:- 

Temperature DB / WB.________ West_______ Cor to Facto-YR:______________ 

SieX~ 

Distance 

from 

Edge of 

Duct 

0- -934. 

Remarks: 

~ UTREQUIRED 

2 Area 

6o r Z .Zb4 

7 _ 7e 

8-W-3:4 

r t . S u b 

Total: 60 e55 

NOTE: Take readins wiSarfoigtwr 

FPM~ 

h bevr 

45 N u m b e r Po i nsf2 

to t l . - R r A v e ra g e : ~ 

ATest ersonneII Siqnaure(s): NUcl\ inenational, Inc. 

1-- D 1


Page C-188 

FT-16 (Rev. 5,11/05) Date: 2zZAt,J 4 26/ 

NUCON International, Inc. Project: 10,fi qSZ 

AIRFLOW CAPACITY AND!I OR DISTRIBUTION TEST REPORT 

client/IPlant: Are#v,-e r 

Unit: al Test No: L 

Flow Rate: 

Test Type: Capacity___ and/or Distribution____ 

Test Location: Duct____ or Filter Face......eXi1I 

CAPACITY 

DISTRIBUTION 

Face Velocity 

Specified ________MCFM, AC ,or SCFM Total sgz _FPM 

(circle on Average -FPM 

Measured FM, ACEM, or SCFM Obtained Readings 

(circle one) Maximumn 6'99 FPM 

Minimum 5*9 FPM 

% ofDesin %Deviation from Average: 

%of Design= Mesrdx100 High + 6-?1' % 

__________ Design _____ Low - X-. % 

Fan Stability Check: ___Sat. j(m(mcrlmr)-Af. x1Xd 

Lsat. Ag.Reading 

Acceptance Criteria Met? Yes No 

Notes I Comments: M-L- t~ee, -Tsi - S 

Test Personnel ignature(s): NUCON International, Inc. 


FT-21 (Rev. 3 11/05) 


Page C-189 

fae2i~tA Time:___ 

NUCON Interna~tional, Inc. Project: 4Q#~iA6/ 

RAW DATA GRID 

~ client/IPlant: '''i# c k(lV 

Unit: "'A ZZ 1 5 

Instrument(s) ID: kv1Z- 

Bank Identification: A ' I 

6r1u&A c4 -. 

TestNo 

Type of Test: Airflow Capacity* ~.Multiple Sampling 

Airflow Distribution Air/Aerosol Distribution_ Other_________) 

TI 2 3 Velocity or Concentration 

(circe one) 

6P 4' 9 Total S'92 Z 

Average 

_ _ 


e3 40maximum ( J - 

____ 

&?' "'%High ~3/ 

____ 

Minimum 4 ~ 

9 %Deviation from Average 

+ - 

- 94 

____%Low ____ 

Dvain=(max or Miri) - Avg. 10 

Notes~ ~ ~ ~ ~ ~ ~~~~~~~~Ag Reomns:ading___________________________ 

T~~~~~~~~~+~~*1 

C NItrntoaIc 

required~ forfntr(S~N


Page C-1 90 

FT-16 (Rev. 5,11/05) Date: .,,a-4 ?( 

NUCON International, Inc. Project: 'P?7 gY 

cz jAIRFLOW CAPACITY AND I OR DISTRIBUTION TEST REPORT 

Client /Plant: Paalt I~ ej 

Unit: A- Test No 

Test Type: Capacity___ and/or Distribution.. 

Test Location: Duct____ or, Filter Face_______ 



Specified ______ MCFM, ACF1M CFM Total 5-6? FPM 

(cirle ne)Average (a Z?- FPM 

Measured FM, ACEM, or SCEM Obtained Readings 

(circle one) Maximum &9'3 FPM 

% of Design Miiu%7 P 


% of Design esignd X100 High + JR,-/ % 

________________Design _______ Low - la,-3 - % 

Fan Stability Check: ___Sat. E(/6DMc (Kxr~ A A00] 

. sat. Avg.Pazrg 

Acceptance Criteria Met? j Yes __No 

Notes I Comments: V ~ei rt-nS 

Test Personnel $ignature(s): NUCON International, Inc. 



NUCON Internationlal, Inc. 

CLI 

RAW DATA GRID 

Client I Plant #2e A dy 

Unit: 4Test 


Page C-191 

Dae~~I.-Time:- 

Project: /9 ROk qg1 r'S 

No:-L- 

instrument(s) ID: _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 

Bank Identification:A 

Type of Test: Airflow Capacity m...~~ultiple Sampling - 

Airflow DistributioflL _Z .Air/Aerosol Distributio Othr___________ 

'L/ 

~'3 5'~Maximum 

'1 

Velcityor Concentration 

(circle one) 

obtained Readings 

Minimum 

69 43 

Z~ 

b%High 


+ . 

% Low- 

Notes~ ~ ~ ~ ~ ~ ~ ~~~~~~o Commnts 

of 

_______________________________ 

tr(~ UO nentoaIc 

~~~~~~~~~~~~Bn A~~f aI~ 

(Mabn ax. or Min.) - Avg. x11)


Page C-1 92 

FT-1 6 (Rev. 5, 11 /05) Date: -z--- '~ol 

NUCON Internaitional, Inc. Project:_1.'? q q-g T 

LzAIRFLOIW CAPACITY AND I OR DISTRIBUTION TEST REPORT] 

Client IPlant: _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 

Unit:, "-1;" u/S 9 Test No: 

Flow Rate: 

Test Type: Capacity_____ and/or DistributionA~ 

Test Location: Duct____ or Filter Face_______ 


Face Velocity 

Spciie MF AC o SFMTotal S ' -. FPM 

Spciie 

_______ CM, ACe o SCFM Average Lz FPM 

(circle 

one: 

Measured FM, ACFM, or SCFM Otie Raig 

4clrcle one) Maimum FPM 

Minimum _S FPM 


% of Design= Measured X10High + % 

Design Low - '' % 

Fan Stability Check: ___Sat. 1 (% (MMwXorM) -Avg. ln 

Unsat. 

Avg.emair 

Acceptance Criteria Met? Yes -No 

Notes IComments: L - q E?' 6 7 -S < V 

~I57 L '_sc 




ae2 jK-Ti,. 


Page C-193 

NUCON InnatlOiona~l, Inc. Project:__ '2'- gtc 

~,e0 

client I Plant: 

Unit: "" (1 

RAW DATA GRID 

instrument(s) 

Bank identification: "1: s 4~e 

_ __ _ __ _ _No:- __ _ __ _ Test___ __ _ __ _ -] __ --_ 

ID: _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 

Type of Test: Airflow Capacity Multiple Sampling te-- 

Airflow Distribution-; Air/Aerosol Distribution_ Othr___________ 

AAq 

(lo 5* 

I 

t 5 

S2~5( 1 (-I1-%High ~ 

Note _____________________________________________ 

I Cmmets: 

,~~~~~~~~e+~~~'iw 

UONItraioaI 

R,.irtueS 

Veocityor Concentration 

(circle one) 


Maximumn 

Minimum 


+ 

Y.laio 

(Mxo n.) - Avg. 

Rea~n~

FT-1 6 (Rev. 5, 11 /05) Date: ~'a~- 


Page C-194 

" NUCON International, Inc. Project:_______________qy 

czAIRFLOW CAPACITY AND I OR DISTRIBUTION TEST REPORT 

C3 Client /Plant:__ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 

Unit: ~ '-Sk 13sP(P- 

Flow Rate: 

Test Type: Capacity_____ and/or Distribution_____ 

Test Location: Duct_____ or Filter Face_______ 

CAPACITY 

Test No: 

DISTRIBUTION 

Face Velocity 

Specfie MCF, AFM, r MTotal '15-4 FPM 

Specifiedrd~ 

_______Moe)AEo Average L-t' FPM 

Measured ________M , ACFM, or SCFM Obtained Readings 

rd oe)Maximum 4?-FPM 

% of Design% 

Minimum FPM 

MeasuredDeviation 

% of Design~ MeasuredHih 

from Average: 

k-2- 

(00o '-esIgn Low - % 

Fan Stability Check: ___Sat. ((xorMn.) -Avg. xc 

7U.nsat. 

1KAg.e~rl 

____-N/A_____ 

___ 

Acceptance Criteria Met? ____Ye s No 

Notes I Comments: WEf~4-{e T-Sulc 




NUCON Internationaol, Inlc.________ 

IW ~wA TA GR I D 

Date--z __ Tme' 


Page C-1 95 

~~ ~client!I Plant:__ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 

Test No:_....... 

Unit .... 

Instrument(s) ID: 

Bank Identification:'3 

L 

Type of Test: Airflow Caait* Multiple Sampling 

~' 

Airflow Distribution _~.-~ AirIAerosol iti~if.. ~Ohr_______ 

T~~~~~~~~~~~+~I 

504 

U O nerainlI 

Minimumfy) 

Avea tlfrmAvrg 

%H-igh + L 6 

%Low - 

Dl afon 

(ma or IMn.) - Avg. 

Avg. ReaAn 

requiredn~ forn~~eS'

FT-1 6 (Rev. 5, 11/05) Date: ;72,04+f, Z?4il 


Page C-1 96 

Fl NUCON Internationail, Inc. Project: P,6.qSs 

cijAIRFLOW CAPACITY AND! OR DISTRIBUTION TEST REPORT 

Client IPlant:-Tt, 

Unit: Z64 £,Z 4. Test No: 

Test Type: Capacity_____ and/or Distribution_______ 

Test Location: Duct____ or Filter Face...... 1 .. 



Specified _______MCFM, ACFM, o FM Aveage !F Z FPM 

Measured ________M , ACFM, or SCFM Obtained Readings 

rlon)Maximum FPM 

% of Design Minimum ?v FPM 


%of Design= MesrdX100 High + % 

_________ Design______ Low -42 

Fan Stability Check: ___Sat. (Mr. or Mn) -Av. 1] 

Acceptance Criteria Met? VYes __No 

Notes I Comments: ttepc -(61S 5&-T 

1~s'l~eronne-FSnature(s): NUCON International, Inc. 


FT-2l (Rev. 3 11/05) 

NUCON Internationa~l, Inc.Pret: 

ci RAWDATA GRID ( 

client1 / Plant: 

Unit c. 

instrument(s) ID: f6~z 


Ca A16 4tA4 

Date-_2j 

p 


Page C-197 

Time 

6# 

TetN:-I 

etN:..... 

Type of Test: Airflow Capacity* Multiple Sapig- te 

Airflow iboZI_, ? Air/Aerosol Distribution Ote_______ 

-'n7 Sll 

Notes I Comments: 

Test 

z 

Velocity or Concentration 

13 Toaximum 1 67 

L~4~%High 

046%Low 

rsonne & Signature(s): NUCON International, Inc. 


+ 1; 

Dei ao (- (max or wnr.) -Avg. 0) 

*No. of Compo nts


Page C-198 

FT-1 6 (Rev. 5, 11/05) Date: z,4,- 2/ 

NUCON International, Inc. Project: i 

czjAIRFLOW CAPACITY AND I OR DISTRIBUTION TEST REPORT 

Client/ Plant: Plimiz- ~ . 

Unit: 6~7 /e4Test No: 

Test Type: Capacity___ and/or Distribution...~ Il 

Test Location: Duct____ or Filter Face..c:1II 



Specified__ MC ACE r SCFM Total 5'29 FPM 

Specifiedcl one)____MCM Average FPM 

Measured _______ M, ACFM, or SCFM Obtained Readings 

circle one) Maximum (,2? FPM 

% of Design Minimum . ZFPM 


from Average: 

%of Design= Design x100 High + :71____ % 

___ __ ___ ___ __ ___ ___ __ ___ __ ___ __Low - 3, % 

Fan Stability Check: ___Sat. (r/1Da cc- rMr)-Avg. X0 

____Unsat. AvgkI~ xl 

Acceptance Criteria Met? es: _es _No 

Notes I Comments: ASLL... H4 epc -E1rs ::, 

T~gt PersonneI Sign-aure(s): NUCON International, Inc. 


FT-21 (kev. 3 11/05) 

Dt:Z~g~-Tm:.~ 

NUCON Interntiona~l, Inc. Project:-Z - 

CI 


RAWIATA GRID 

client 1 Plant: 1N iA-4-"' 

Tes 

Unit: 6 i ,14 

O'- 

Bank Identification: r ~~4 

/ 


Page C-199 

15# ~'4 

etN : . 

Type of Test: Airflow Capacity* Multiple Sampling 

Airflow DistributioI Air/Aerosol Distribution_ Other__________ 

Aveat:il fo vrg 

%High + 

%Low- 

( eito (maxc or vln.) - Avg. 

AgReacing 

1 

If required for 

*Component Area 

Notes I Commenlts:_ _ _ _ _ _ _ _ _ _ _ _ _ _ __ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 

TrrrYlI 

sirn,ttjre( s):NU CON nter national, Inc.

FT-16 (Rev. 5,11105) Date: ~ 

NUCON International, Inc. Project: 


Page C-200 

SAIRFLOW CAPACITY AND I* OR DISTRIBUTION TEST REPORT 

Client IPlant:__ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 

Unit: O'-o.3S-e C' 1-7: VM -reZ Test No:____ 

Test Type: Capacity_______ and/or Distribution____ 

Test Location: Duct____ or Filter Face______ 



I ~ Spciie 6 MCFM, ACFM, o SCF Total ki -2- ( - FPM 

(circle one) I vrg P 

Measured 1-448, MOEM, ACFM, o CFOtandRdig 

(circle one) Maximum I ( )FPM 

% o Deign ~ %Minimum - 147" FPM 


%of Design= esignd X100 High + -z2,l %~ 

______________Design ________ Low - glkiI % 

Fan Stability Check: ___Sat. I(1/6~~r (M-xr~.) -A\,. X0 

____Unsat. I K Paing 

x N/A 

Acceptance Criteria Met? Yes /"No 

Notes I Comments: A-tLraco,.aE~- -~ 4E 

clu C; S. ~ -Cr- &'YxL~- 

0 N L-L- L).T--cs t>Z'-se ' i a 5e ,3-- cpc 

-r~-r~ ~s~T~ ~9 ~C2' v17-.e C:: ~ -1:r ~~r 

Test Pesnnel Signature(s): NUCON International, Inc. 



NUCON Interflcioill Inc. 

CII" 

EJ client! Plant: ___________________________________ 

instrument(s) ID: 


RAW DATA GRID 

Date: 

Project: -L 


Page C-201 

Type of Test: Aifown J_ util 

Airflow DistributioL... I Aijr/Aerosol Distribution-.~ Othr___________ 

+%Aea~ 

ime:- 

frm5veag 

%High + 

%/Low- IS7 

I iabo n (Max or tfin.) - Ag.x 

*componenlt Ar 

*No of Co ponents 

Notes I Commenlts:_ _ _ _ _ _ _ _ _ _ _ _ _ _ __ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 

-r. iD.rejnflI x sinflqT1rPe(b]. UCNinternational, Inc.

FT-1 6 (Rev. 5, 11 /05) Date: -Z- 'I--- 


Page C-202 

NUCON internaitional, Inc. Project: 

iz AIRFLOW CAPACITY AND I OR DISTRIBUTION TEST REPORT 

SClient /Plant: _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 

Unit: ? Tz -i.rr Test No: ____ 


Test Location: Duct____ or Filter Face_______ 


FlowRate: Face Velocity 

Speciied 

Specifiedrcl 

MFM. CF orSCFMTotal - S-i :f-z- 

CM one_____ AFSF Average s--*. -~ 

FPM 

FPM 

Measured FM, ACFM, or SCFM Obtained Readings 

(circle one) Maximum 1313 FPM 

Minimum - O FPM 


from Average: 

%of Design=- X100 High + '77-W % 

L_____Design__________ Low- -13c 

Fan Stability Check: ___Sat. [/EDaio=Kxrr)-v.10 

A.___N/A :A S A'. 

Acceptance Criteria Met? Yes v-i"o 

Notes I Comments: $~~C tz~. E''- 




NUCON InternaQtionl, Inc. 

CII 

instrument(s) ID: 

RAW DATA GRID 

Dae77-'-6- 

Prjc-2= 

- 


Page C-203 

client iPlanit _~~- -c TestNounit~ 

- 

Bank Identification, 

~ 

L_~?3 

x- 

Tye fTet Airflow Capacity* multiple Smpling~--- -- Ohe 

ofst Test:Z ATrflo 

Air/Aerosol Distributionl-~~Ohr_______ 

Airflw Ditribtion(specify) 

7;: + 

Notes~ ~ ~ ~ ~ ~~~~~~~"o Commmpt 

_______________________________ 

x~~~rfP s iinnture(sM: NUCON International, Inc. 

%DefAea~ fro Aveag 

%High~ + 2 - 

%Low -_________ 

*Ifc rq ie TorM.)-Ag 10 

of

FT-16 (Rev. 5,11/05) Date: -- '-- 


Page C-204 

F4 NUCON Interncition al, Inc. Project:________ 

czAIRFLOW CAPACITY AND I OR DISTRIBUTION TEST REPORT 

C3 

SClient / Plant:______________________________________________ 

Unit: 

Flow Rate: 


Test Location: Duct____ or Filter Face__________ 

CAPACITY 

Test No: 

DISTRIBUTION 

Face Velocity 

Specified __ ____MCFM, ACEM SCFM Total Llq4 FPM 

(circl one)Average Wt'S .5 FPM 

Measured _______ , ACEM, or SCFM Obtained Readings 

f? circle one) Maximum 1-3q3 FPM 

Minimum -'. FPM 


from Average: 

%of Design= Deinx100 High + -1 -% 

J _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ Low - - 1 G3 - 

Fan Stability Check: ___Sat. I(Weicn (N~x or Mn.) -Aug. 1X 1 

" 

____Unsat. Ag Pal n 

Acceptance Criteria Met? Yes "~No 

Notes/IComments: ~6 ' ~ ~ ~ 




NUCON Internotioflal, Inc._Prject:--------c~z 

RAW DATA GRID 

Dt: z 


Page C-205 

client I Planlt:_ _ _ _ _ _ _ _ _ _ _ _ _ __ _ _ _ _ _ _ _ _ _ _ _ 

Unit .~' '~~~ -- e&Test No:.L - 


Bank Identificatiofl ~ 

L-O_'VCk 

'~ 

- 

Type of Test: Airflow Cpct*_ 

Ai~o Capcot 

multiple sampling ---- 

Air/Aerosol Distribution- Other_______ 

13 

Y~ ;~c~n~ s ~Inn ( 

Veit~ 

romerageo 

Aeae:(Mw~o vn)-Ag 

%DUCatio fntrntona Avnc.g



Page C-206

ehoogc IiC 

Test #: 11-1704 


Page C-207 

Pg I of 1 


Wasbigon River protection Solutions 242-AEvortrK 

Pro'ect Descri-2tion: 

premier Technolo Y, Inc. Project #: 6765 

Client P0 : 

N/A 

Date of Test: 

4/18/11 

Test Perfrmed By & Cert. Level: Caleb Killian Level 11 A 

Witnessed B3v: 

Pau Mcbride 

Procedure Number and Rev: TP 1.7 REV 5 


FLOW 


242-A Evaporator KI 

Pressur Gauge Serial Number: PTI-378 


Pressure Gauge Ran e: 0-30 IN HG 

Pressure Gauge Manufacturer: D)W YER 

Pressure Gau, e Model: DPGW-00 


*24.2 IN H120 

Desi Pressure: 

18.96 IN H20 


AIR 

Leak Solution Mnfcre / Brand Swagelock/ Snoop! MS-SNOOP-GAL 


Start Time: 

3:10 PM 

End Time: 

3:26 PM 

Ter erature Gauge Serial Number: PTI-4 16 


Ter erature Gau e Ran e: -127 to 600 deg. C. 

Ter erature Gauge Manufacturer: Fluke 

Ternperature Gauge Model: 52 11 thermometer 

Avera. e Tern erature, Durnn Test: 55.4 de .-F. 

Results of Test: Acce-otable F- U-n-Acce tbe(E an eo 


Comments: *Pressure mandated by FAT. See test exception 010. 

'This test satisfies the requirements of steps 7.28.5 and 7 .28.6 of FAT for job 6765.


Rate of De y Test Report Test #:11-1705 

Isolation Barrier Identification: 22AEaoao iEhutVniainSse 

Test Equip ent 

Manomneter/pressure Gauge: S/N: PTI-378 Calibration Due: 16/14/11 

Barometric Pressure gauge S/N: PC30121A71 Calibration Due: 6/22/11 

identification 

Thermometer IS/N: PTI-41 6 Calibration Due: M9/23/1 1 

Test Parameter 

V = Volume of System to be Tested 232.21 cubic feet 

At =Total Test Time _ 15 m.n 

P= Required Test Pressure -23.7 ______nH2O 

Convert Specified Acceptance Value (SAY) into CFM using the equation below: 

SAV= 000xV SAV= 0.001 X 232.21 SAV = 0.0039 -CFM 

60 Min. 60 mim Max.Permissible Leak 


Page C-208 

Test Readings 

TIEStart Finish At tf A 1 

(Min.) 7:26 AM 7:41 AM 1 

nTEMP. 

Start 

Finish 

(O)29.6 +459.7 =Ti 30.1 +45E9.7 = T 

PRESSURE (PB) (in~g) 25.40254 

TP-1. 15.6765 Rate of Decay Test for 6765 Revision 0 

1of2


Calculatious WG n NH oI 

1. R = I2.Deternmine Pi & Pf (Convert from inches W.G an INm Hg to20 +b/Ft 07 


Page C-209 

5 3.3 5 P= Pjm x 5.204 + P x 70.73 P ~524+Px07 

(Gas P.= - 24.9 x 5.204 + 25.4) x 70.73 -P 2. .0 54 70.73 

Constant 

for Air) pi ( -129.5796) + (1796.5420) Pf =(-127,4980) + (1796.5420) 

P 166.924 P= -1669.0440- 

3 .alulteAverage Leak Rate of H-ousing using the following equation: Steps A-E 

~~Pi Pf~ V SeB.-(1666.9624 1669.0440 232.21 

StepA . -~Ti Tf'. RAt (0,075) StpB 489.3 489.8 ) (53.35)(15) (0.075) 

Step C., (3.4068 -3,4076) -- L2-2 Step D. = (-.0008 ) (3.8689) 

Step E. = -031 FM =-.1860 CFH 

SAV 0.039 CM =0.2340 CH 

if Qis less than SAV. permissible leakage, housing or system is acceptable 

Test Results 

Test Duration Average total leakage Accept/Reject Test Date 

15 MIN. 

-0. 1860 CFIll ACCEPT 4/19/11 

Test Performed by: Certification ILevel Date: 

Print Caleb Killian 

Signature j jit lb 

Test Witnessed by: Paul Mcbride 

LvlI 

Date 4/19/11 

TP1.15665 Rate of Decay Test for 6765 Rvso 

2 of 2



Page C-210


Page C-211 

Techoloy. 

nc.Test#:l11-1512 


Pg I of I 

Proe, Descri tion: 

Premier Technology, Inc. Proect #: 

Client PO #: 

Date of Test: 

Test Performed By.& Cert. Level: 

Washington River Protection Solutions 242-A Evaporator K1 

6765 

N/A 

3/28/l1 

Caleb Killian Level HI t_2 I 

Witnessed. BY: 

Paul Mcbride 

Namceur Number.dRv ? . E 

Tesd Meho 

4:30PMqu LO 

Treaure Gaue Serial Number: PTI-3784 

Cal Date and Due Date: 1/1/10-/12/11 

Treraure Gauge Range: -17t 00 DE G C 

Terersture Gauge Manufacturer: FLUER 

Preue NCRg 11e-171.-0 

This testure satifie the reu H2n0ofs 72. nth ttdFT 

Des' Presure .7-1, ReiNo 0H36/0

Sample 4 FAT Report Rev 0

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