EMB-505 - Embraer
13.07.2015 • Views
Share Embed Flag

EMB-505 - Embraer

EMB-505 - Embraer

EMB-505 - Embraer

SHOW MORE
SHOW LESS
ePAPER READ
DOWNLOAD ePAPER
  • No tags were found...
embraer.com

Create successful ePaper yourself

Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.

START NOW

ÀREA DE NÃO INTERFERÊNCIATM<strong>EMB</strong>-<strong>505</strong>GROUND HANDLINGANDSERVICING HANDBOOKGHSH-326120 NOV<strong>EMB</strong>ER 2009REVISION 3 - 24 FEBRUARY 2011HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.Copyright © 2011 by <strong>EMB</strong>RAER S.A. All rights reserved. The information, technical data, designs and drawingsin this document are proprietary information of <strong>Embraer</strong> or third parties and shall not be used or disclosed toany third party nor copied or reproduced, whether in whole or in part, in any form or by any means whatsoeverwithout the express written authorization of <strong>Embraer</strong>.

CUSTOMER COMMENT FORMPlease use this Customer Comment Form to notify us of any discrepanciesor problems you encounter in our Technical Publications. We wouldalso welcome constructive suggestions on how we can further improveour documentation or service.Your feedback will be acknowledged, and we will advise you of theaction we intend to take.Sincerely,<strong>Embraer</strong> Technical Publications.HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.

CUSTOMER COMMENT FORMPlease Specify:Publication Part Number: ...................................................................................Chapter: .................................. Revision:.......................... Date:.......................HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.Comment/Suggestion:...............................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................Your Name: ................................................ Department: ..................................Company Name: ................................................................................................Address:.............................................................................................................Fax Number: ................................... Telephone Number: ..................................E-mail:............................................. Website: ...................................................Please return this Customer Comment Form to:<strong>EMB</strong>RAER S.A.TECHNICAL PUBLICATIONSAv. Brigadeiro Faria Lima, 2170CEP 12227-901São José dos Campos SP-BRASILFAX: ++ 55 12 3927-7546E-mail: distrib@embraer.com.brWebsite: www.embraer.com.brThis Space Reserved for <strong>Embraer</strong>CCF Nº ..........................................Comment received:...................................Date Acknowledged:.......................Person Actioned:................................................................................................Action to be taken:...................................................................................................................................................................................................................................................................................................................................................Proposed date for implementation:....................................................................Implemented:.....................................................................................................

EMPRESA S.A.AV. BRIGADEIRO FARIA LIMA, 2170 - CAIXA POSTAL 8050 - TELEFONE (55) 12 3927-7517FAX (55) 12 3927-7546 - CEP 12.227-901 - SÃO JOSÉ DOS CAMPOS - SÃO PAULO - BRASILe-mail:distrib@embraer.com.br/http://www.embraer.comTO: HOLDERS OF PUBLICATION No. GHSH-3261 - “GROUND HANDLINGAND SERVICING HANDBOOK”, APPLICABLE TO <strong>EMB</strong>-<strong>505</strong> AIRCRAFT.REVISION No. 03 DATED FEBRUARY 24/11HIGHLIGHTSPages which have been added, revised, or deleted by the current revision are indicatedby an asterisk, on the List of Effective Pages.HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.HIGHLIGHTS Page 1 of 2Feb 24/11Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKCHAPTERSECTION PAGE DATESUBJECTCHAPTERSECTION PAGE DATESUBJECTFRONTMATTERLOEP...........................* LEP-1 ..............Feb 24/11LOEP...........................* LEP-2 ..............Feb 24/11LOEA........................... LEA-1 ..............Nov 20/09LOEA............................ LEA-2 ..Blank.. Nov 20/09INTRODUCTION ...... INTRO-1 ............ Nov 20/09INTRODUCTION....... INTRO-2 ............ Nov 20/09INTRODUCTION....... INTRO-3 ............ Nov 20/09INTRODUCTION....... INTRO-4 ............ Nov 20/09INTRODUCTION....... INTRO-5 ............ Nov 20/09INTRODUCTION....... INTRO-6 ............ Nov 20/09INTRODUCTION ...... INTRO-7 ............ Nov 20/09INTRODUCTION....... INTRO-8 ............ Nov 20/09INTRODUCTION....... INTRO-9 ............ Nov 20/09INTRODUCTION....... INTRO-10 .......... Nov 20/09INTRODUCTION....... INTRO-11 .......... Nov 20/09INTRODUCTION....... INTRO-12 .......... Nov 20/09PROCEDURETOC................................. 001 .............. Nov 20/09TOC................................. 002 .............. Nov 20/09TOC................................. 003 .............. Nov 20/09TOC................................. 004 ...Blank.. Nov 20/0909-10-01-500-801-A........ 201 ............. May 28/1009-10-01-500-801-A........ 202 .............. Nov 20/0909-10-01-500-801-A........ 203 .............. Nov 20/0909-10-01-500-801-A........ 204 .............. Nov 20/0909-10-01-500-801-A........ 205 .............. Nov 20/0909-10-01-500-801-A........ 206 .............. Nov 20/0910-10-00-500-801-A........ 201 .............. Nov 20/0910-10-00-500-801-A........ .202 ............. May 28/1010-10-00-500-801-A........ 203 .............. Nov 20/0910-10-00-500-801-A........ 204 .............. Nov 20/0910-10-00-500-801-A........ 205 .............. Nov 20/0910-10-00-500-801-A........ .206 ............. May 28/1010-10-00-500-801-A........ 207 ............. May 28/1010-10-00-500-801-A........ .208 ............. May 28/1010-10-00-500-801-A........ .209 ............. May 28/1010-10-00-500-801-A........ .210 ............. May 28/1010-10-00-500-802-A........ 201 .............. Nov 20/0910-10-00-500-802-A........ 202 ...Blank.. Nov 20/0910-20-00-500-801-A........ .201 .............. Nov 20/0910-20-00-500-801-A........ .202 .............. Nov 20/0910-20-00-500-801-A........ .203 .............. Nov 20/0910-20-00-500-801-A........ .204 .............. Nov 20/0910-30-00-500-801-A........ 201 .............. Nov 20/0910-30-00-500-801-A........ 202 .............. Nov 20/0910-30-00-500-801-A........ 203 .............. Nov 20/0910-30-00-500-801-A......... 204 .............. Nov 20/0910-30-00-500-802-A........ 201 .............. Nov 20/0910-30-00-500-802-A........ 202 .............. Nov 20/0910-30-00-500-802-A........ 203 .............. Nov 20/0910-30-00-500-802-A........ 204 ...............Nov 20/0910-30-00-500-802-A........ 205 ...............Nov 20/0910-30-00-500-802-A........ 206 ...Blank...Nov 20/0912-11-00-650-801-A ........ 301 .............. Nov 20/0912-11-00-650-801-A ........ 302 .............. Nov 20/0912-11-00-650-801-A ........ 303 .............. Nov 20/0912-11-00-650-801-A ........ 304 .............. Nov 20/0912-11-00-650-802-A ........ 301 .............. Nov 20/0912-11-00-650-802-A ........ 302 .............. Nov 20/0912-11-00-650-802-A ........ 303 .............. Nov 20/0912-11-00-650-802-A ........ 304 .............. Nov 20/0912-11-00-650-803-A ........ 301 .............. Nov 20/0912-11-00-650-803-A ........ 302 .............. Nov 20/0912-11-00-650-803-A ........ 303 .............. Nov 20/0912-11-00-650-803-A ........ 304 .............. Nov 20/0912-11-00-650-803-A ........ 305 ...............Nov 20/0912-11-00-650-803-A ........ 306 ...Blank...Nov 20/0912-11-00-680-801-A ........ 301 .............. Nov 20/0912-11-00-680-801-A........ 302.............. Nov 20/0912-11-00-680-801-A........ 303.............. Nov 20/0912-11-00-680-801-A........ 304.. .Blank.. Nov 20/0912-12-00-210-801-A ....... 301.............. Nov 20/0912-12-00-210-801-A ....... 302.............. Nov 20/0912-12-00-210-801-A ....... 303.............. Nov 20/0912-12-00-210-801-A ....... 304... Blank.. Nov 20/0912-12-00-612-801-A ....... 301.............. Nov 20/0912-12-00-612-801-A ....... 302.............. Nov 20/0912-12-00-612-801-A ....... 303.............. Nov 20/0912-12-00-612-801-A ....... 304.. Blank.. Nov 20/0912-14-00-610-801-A .......* 301.............. Feb 24/1112-14-00-610-801-A .......* 302.............. Feb 24/1112-14-00-610-801-A ....... 303.............. Nov 20/0912-14-00-610-801-A ....... 304.............. Nov 20/0912-15-01-613-801-A ....... 301.............. Nov 20/0912-15-01-613-801-A ....... 302.............. Nov 20/0912-15-01-613-801-A ....... 303.............. Nov 20/0912-15-01-613-801-A ....... 304.............. Nov 20/0912-15-03-600-801-A ....... 301.............. Nov 20/0912-15-03-600-801-A .......* 302.............. Feb 24/1112-15-03-600-801-A .......* 303.............. Feb 24/1112-15-03-600-801-A ....... 304.............. Nov 20/0912-15-03-600-801-A ....... 305.............. Nov 20/0912-15-03-600-801-A ....... 306... Blank.. Nov 20/0912-23-00-100-801-A ....... 301.............. Nov 20/0912-23-00-100-801-A ....... 302.............. Nov 20/0912-23-00-100-801-A ....... 303.............. Nov 20/0912-23-00-100-801-A ....... 304.............. Nov 20/0912-23-00-100-801-A ....... 305.............. Nov 20/0912-23-00-100-801-A ....... . 306... Blank.. Nov 20/0912-23-00-100-802-A ....... 301.............. Nov 20/0912-23-00-100-802-A ....... 302.............. Nov 20/0912-23-00-100-802-A ....... 303.............. Nov 20/0912-23-00-100-802-A ....... 304.............. Nov 20/0912-23-00-100-802-A ....... 305.............. Nov 20/0912-23-00-100-802-A ....... 306.............. Nov 20/0912-23-00-100-802-A ....... 307.............. Nov 20/0912-23-00-100-802-A ....... 308.............. Nov 20/0912-23-00-100-802-A ....... 309.............. Nov 20/0912-23-00-100-802-A ....... 310.............. Nov 20/0912-23-00-100-802-A ....... 311.............. Nov 20/0912-23-00-100-802-A ....... 312.............. Nov 20/0912-23-00-100-802-A ....... 313.............. Nov 20/0912-23-00-100-802-A ....... 314.............. Nov 20/0912-23-00-100-802-A ....... 315.............. Nov 20/0912-23-00-100-802-A ....... 316.............. Nov 20/0912-23-00-100-802-A ....... 317.............. Nov 20/0912-23-00-100-802-A ....... 318.............. Nov 20/0912-23-00-100-802-A ....... 319.............. Nov 20/0912-23-00-100-802-A ....... . 320... Blank.. Nov 20/0920-00-00-910-801-A ....... 201.............. Nov 20/0920-00-00-910-801-A ....... 202.............. Nov 20/0920-00-00-910-801-A ....... 203.............. Nov 20/0920-00-00-910-801-A ....... 204.............. Nov 20/0920-40-02-910-801-A ....... . 201.............. May 28/1020-40-02-910-801-A ....... . 202.............. May 28/1020-40-02-910-801-A ....... 203.............. May 28/1020-40-02-910-801-A ....... 204.............. Nov 20/0924-36-01-000-801-A ....... 401.............. Nov 20/0924-36-01-000-801-A ....... 402.............. Nov 20/0924-36-01-000-801-A ....... 403.............. Nov 20/0924-36-01-000-801-A ....... 404.............. Nov 20/0924-36-01-000-801-A ....... 405.............. Nov 20/0924-36-01-000-801-A ....... 406... Blank.. Nov 20/0924-36-01-000-802-A ....... 401.............. Aug 27/1024-36-01-000-802-A ....... 402.............. Nov 20/0924-36-01-000-802-A ....... 403.............. Nov 20/0924-36-01-000-802-A ....... 404.............. Nov 20/0924-36-01-400-801-A ....... 401.............. Nov 20/0924-36-01-400-801-A ....... 402.............. Nov 20/09HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.Pages revised or added by current revision are indicated by an asterisk (*). Pages deleted by the current revisionare indicated by (Del)*. Pages deleted by the previous revision are indicated by (Del).EFFECTIVITY: ALLLIST OF EFFECTIVE PAGESPage LEP-1Rev.03- FEB 24/11Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKCHAPTERSECTION PAGE DATESUBJECTCHAPTERSECTION PAGE DATESUBJECTHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.24-36-01-400-801-A........ 403 .............. Nov 20/0924-36-01-400-801-A........ 404 ...Blank.. Nov 20/0924-36-01-400-802-A........ 401 .............. Aug 27/1024-36-01-400-802-A........ 402 .............. Nov 20/0924-36-01-400-802-A........ 403 .............. Nov 20/0924-36-01-400-802-A........ 404 .............. Nov 20/0924-41-00-860-801-A........ 201 .............. Nov 20/0924-41-00-860-801-A........ 202 .............. Nov 20/0924-41-00-860-801-A........ 203 .............. Nov 20/0924-41-00-860-801-A........ 204 .............. Nov 20/0924-41-00-860-802-A........ 201 .............. Nov 20/0924-41-00-860-802-A........ 202 .............. Nov 20/0924-41-00-860-802-A........ 203 .............. Nov 20/0924-41-00-860-802-A........ 204 .............. Nov 20/0927-04-01-710-801-A........ 501 .............. Nov 20/0927-04-01-710-801-A........ 502 .............. Nov 20/0928-00-00-910-801-A........ 201 .............. Nov 20/0928-00-00-910-801-A........ 202 .............. Nov 20/0928-00-00-910-801-A........ 203 .............. Nov 20/0928-00-00-910-801-A........ 204 ..Blank... Nov 20/0929-10-00-910-801-A........ 201 .............. Nov 20/0929-10-00-910-801-A........ 202 .............. Nov 20/0929-10-00-910-801-A........ 203 .............. Nov 20/0929-10-00-910-801-A........ 204 .............. Nov 20/0929-10-00-910-801-A........ 205 .............. Nov 20/0929-10-00-910-801-A........ 206 .............. Nov 20/0929-10-00-910-802-A........ 201 .............. Aug 27/1029-10-00-910-802-A........ 202 .............. Aug 27/1029-10-00-910-802-A........ 203 .............. Aug 27/1029-10-00-910-802-A........ 204 .............. Aug 27/1029-10-00-910-802-A........ 205 .............. Aug 27/1029-10-00-910-802-A........ 206 ..Blank... Aug 27/1029-10-00-910-802-A.. Del 207 .............. Aug 27/1029-10-00-910-802-A.. Del 208 .............. Aug 27/1032-00-00-910-801-A........ 201 .............. Nov 20/0932-00-00-910-801-A........ 202 .............. Nov 20/0932-45-00-210-801-A........* 601 .............. Feb 24/1132-45-00-210-801-A........* 602 .............. Feb 24/1132-45-00-210-801-A........* 603 .............. Feb 24/1132-45-00-210-801-A........ 604 .............. Aug 27/1032-45-00-210-801-A........ 605 .............. Aug 27/1032-45-00-210-801-A........ 606 ...Blank...Nov 20/0971-00-01-910-803-A........ 201 .............. Nov 20/0971-00-01-910-803-A........ 202 .............. Nov 20/0971-00-01-910-803-A........ 203 ............. May 28/1071-00-01-910-803-A........ .204 .. Blank...May 28/10APPENDIXGSE TOC ..................... ..TOC-1 ........... Nov 20/09GSE TOC ........................TOC-2..Blank. Nov 20/09GSE 003.......................... ........1 .......... Nov 20/09GSE 003................... ...............2 ............Nov 20/09GSE 009................... .............. 1............ Nov 20/09GSE 009................... .............. 2............ Nov 20/09GSE 016......................... ........ 1............ Nov 20/09GSE 016......................... ........ 2............ Nov 20/09GSE 016......................... ........ 3............ Nov 20/09GSE 016......................... ........ 4.Blank . Nov 20/09GSE 022................... .............. 1............ Nov 20/09GSE 022................... .............. 2............ Nov 20/09GSE 023......................... ........ 1............ Nov 20/09GSE 023......................... ........ 2............ Nov 20/09GSE 026................... .............. 1............ Nov 20/09GSE 026................... .............. 2............ Nov 20/09GSE 027................... .............. 1............ Nov 20/09GSE 027................... .............. 2............ Nov 20/09GSE 029................... .............. 1............ Nov 20/09GSE 029................... .............. 2............ Nov 20/09GSE 030................... .............. 1............ Nov 20/09GSE 030................... .............. 2............ Nov 20/09CPA.............................. .. CON-1 .......... Nov 20/09CPA.............................. .. CON-2 .......... Nov 20/09Pages revised or added by current revision are indicated by an asterisk (*). Pages deleted by the current revisionare indicated by (Del)*. Pages deleted by the previous revision are indicated by (Del).EFFECTIVITY: ALLLIST OF EFFECTIVE PAGESPage LEP-2Rev.03- FEB 24/11Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKTHIS MANUAL IS APPLICABLE TO ALL PHENOM 300EXECUTIVE JETS IN OPERATION.HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALLGHSH List of Effective AircraftPage LEA-1/2NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKINTRODUCTIONHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.

GROUND HANDLING ANDSERVICING HANDBOOKGHSH INTRODUCTION1. GeneralA. This handbook is intended to assist ground handling and servicing personnelthat are not familiar with the <strong>Embraer</strong> Phenom 300 aircraft. The <strong>Embraer</strong> Phenom300 Aircraft Maintenance Manual contains detailed maintenance orinspection information.B. This handbook is a supplement to the Aircraft Maintenance Manual (AMM)and the Airplane Flight Manual (AFM). In case of conflict between this guideand the AMM and / or AFM, the AMM and / or AFM shall take precedence.C. The source of all information in this manual is, basically, the information in thepublications listed below:(1) Aircraft Maintenance Manual (AMM).(2) Illustrated Tool and Equipment Manual (ITEM).(3) Consumable Products Catalog (CPC).2. The improvement of methods and development of new techniques by the operatorsare contributions to be included in this manual. If you have suggestions orneed any assistance regarding maintenance technical publications, please contactus at:• contact.center@embraer.com - For contributions/request for assistance regardingtechnical subjects related to Maintenance Technical Publications, GSE,Service Bulletins, AIPC and SRM I;• distrib@embraer.com.br - For assistance regarding purchase and distributionof manuals;• cdrom.support@embraer.com.br - For assistance regarding Digital TechnicalPublications contained in electronic media.3. It is vital that the operators commit themselves to keeping this manual update bystrictly inserting the revised pages in the proper locations according to the lastrevision of manual available in the Fly<strong>Embraer</strong> site.4. The GHSH is composed by (Figure 1):A. The front matter:(1) Front PageShows the manufacturer's masthead, identification of the manual, the initialissue date, and revision number and date.(2) Customer Comment Form(3) List of Effective AircraftProvides a cross-reference tabulation of Aircraft Commercial Designation,Customer Aircraft Number, and Manufacturer Serial Number.(4) List of Effective Pages:Lists all chapters and their list of effective pages with the latest issue dates.HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALLINTRODUCTIONPage INTRO-1NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.NOTE: • Pages revised or added by the current revision are indicatedby an asterisk (*).(5) Title of Introduction(6) Introduction• Pages deleted by the current revision are indicated by del *.Pages deleted by the previous revision are indicated by del.B. GHSH ProceduresThe GHSH procedures section is composed by:(1) Procedures Title Page(2) Table of Contents(3) GHSH Procedures(a) The GHSH procedures are organized into chapters:Chapter NumberTable 1 – GHSH Chapters9 Towing & TaxingChapter Title10 Parking, Mooring, Storage & Return to Service12 Servicing20 Standard Practices-Airframe24 Electrical Power27 Flight Controls28 Fuel29 Hydraulic Power32 Landing Gear71 Engine(b) PDF Page Identification and NumberingThe GHSH task numbering is shown in the top of the body page and inthe skirting board page, and is composed as follows:1. Top of Body PageGHSH TASK 12-11-00-650-801-AElements 1, 2, and 3 comprise the equipment identifier. The fourthelement is the three-digit function code, which defines the maintenancefunction being performed by tasks. The fifth element is athree-digit number used to create unique numbers for all tasks, whichare similarly numbered through the first four elements. Tasks arenumbered from 801 through 999. The sixth element is an alphabeticidentifier (task) used to uniquely identify differences in configuration,methods / techniques, variations of standard practices applications,etc.2. Skirting Board PageEFFECTIVITY: ALLCopyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.INTRODUCTIONPage INTRO-2NOV 20/09

GROUND HANDLING ANDSERVICING HANDBOOKThe task numbering shown in the skirting board page shows thebody page numbering followed by the page block numbering, that isused to inform the type of procedure to be executed.12-11-00-650-801-A/300The table below lists the pageblocks and their respective names:Table 2 - GHSH PageBlocksPageBlock NamePageBlocksSystem Description Section 000Component Location 100Maintenance Practices 200Servicing 300Removal/Installation 400Adjustment/Test 500Inspection/Check 600Cleaning/Painting 700Repairs 800C. GHSH Appendixes(1) Appendix Title Page(2) GSE (Ground Support Equipments) Title Page(3) TOC GSE(4) GSE (Ground Support Equipments)(a) The GSE Appendix is composed of the GSE's referenced in the GHSHtasks.The GSE Appendix is arranged in GSE number increasing order.For information about other GSE's used in the Phenom 100, pleasecheck the Illustrated Tool and Equipment Manual (ITEM).(5) Consumable Products Title Page(6) Consumable Products(a) The Consumable Products Appendix is composed of a table whichlists all the consumable products referenced in the GHSH tasks. TheConsumable Products Appendix is arranged in part number alphabeticalorder. The Consumable Products Appendix provides the followinginformation about consumables:1. PART NUMBER ColumnThis column provides the product part number and/or trade name.When the product does not have a part number, its specification isrepeated in this column.2. SPECIFICATION ColumnThis column gives the specification with which the material mustcomply. A simple dash in this column denotes that the product doesnot meet any specification or that only the product referred to in thisHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALLINTRODUCTIONPage INTRO-3NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.catalog shall be used.3. DESIGNATION ColumnThis column presents a brief description of the material.4. SUPPLIER ColumnThis column lists the names of the most usual suppliers of thematerial.5. SHELF LIFE ColumnThis column gives the period of time (in months) between the fabricationdate and the last date when the conditions for use of theproduct are still assured, providing the material is packed andstored as specified.6. DANGER CLASS ColumnThis column gives the product danger class according to the InternationalAir Transportation Association (IATA) - Dangerous GoodsRegulations.7. STORAGE CODE ColumnThis column lists codes referring to the conditions that assure theproper preservation of the consumable products during their storageperiod.NOTE: The information from the manufacturer/supplier shallalways prevail over the one herein.The table Storage Conditions gives the codes associated with theconditions under which each product must be stored. This tablepresents the following requirements:a. TemperatureThis column gives the proper ambient temperature, both in Celsiusand Fahrenheit degrees, to store a product. It may give arange of temperature (4 to 38 °C, for example) or the maximumallowable temperature (25 °C (maximum), for example).b. Away FromThis column gives the products/conditions from which the itemshould stay away in order to guarantee its adequate preservation.The following table gives the storage conditions.Table 3 - Storage CodeStorage Code Temperature Away From01 4 to 38 °C (39 to 100 °F)Fuel, Ozone and/or spark generatingdevices Moisture, Dust, Oil,Grease, Direct Sunlight, FluorescentLight, Air in Circulation.EFFECTIVITY: ALLINTRODUCTIONPage INTRO-4NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKTable 3 – Storage Code (Continued)Storage Code Temperature Away From02 25 °C (MAX.)(77°F (MAX))04 4 to 38 °C (39 to 100 °F)07 4 to 38 °C (39 to 100 °F)08 4 to 38 °C (39 to 100 °F)09 25 °C (MAX)(77 °F (MAX))10 4 to 38 °C (39 to 100 °F)11 25 °C (MAX)(77 °F (MAX))12 4 to 38 °C (39 to 100 °F)13 4 to 38 °C (39 to 100 °F)14 4 to 38 °C (39 to 100 °F)15 4 to 38 °C (39 to 100 °F)Sources of heat, Ozone and/orspark generating devices, Oxidants,Dust, Oil, Fuel, Water,Direct Sunlight, Air in Circulation.Sources of heat, Spark generatingdevices, Oxidants, Dust, DirectSunlight.Sources of heat, Spark generatingdevices, Oxidants, Oxygen cylinders.Sources of heat, Spark generatingdevices, Oxidants, Corrosive acid,Direct sunlight.Sources of heat, Dust, Oil,Grease,Direct sunlight.Sources of heat, Dust, Oil,Grease, Direct sunlight.Sources of heat, Ozone and/orspark generating devices, Dust,Vibrations, Magnetic fields, Air incirculation.Sources of heat, Spark generatingdevices, Oxidants, Corrosivebase, Direct sunlight.Sources of heat, Spark generatingdevices, Oxidants, Direct sunlight.Sources of heat, Spark generatingdevices, Oxidants, Direct sunlight.Sources of heat, Spark generatingdevices, Corrosive acid and base,Direct sunlight.16 According to local regulatory authorities and manufacturer.17 25 °C (MAX)(77 °F (MAX))50 According to local manufacturer/supplier.99 4 to 38 °C (39 to 100 °F)Electrostatic fields, Magneticfields, Dust, Direct sunlight.Sources of heat, Ozone and/orspark generating devices, Dust,Vibrations, Magnetic fields, Corrosiveacid and base, Oxidants,Flammable liquids, Explosives.HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALLINTRODUCTIONPage INTRO-5NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

TMCopyright 2008 by <strong>EMB</strong>RAER − Empresa Brasileira de Aeronáutica S.A. All rights reserved. This documentshall not be copied or reproduced, whether in whole or in part, in any form or by any means without the expresswithout permission of <strong>Embraer</strong>.GHSH−326114 AUGUST 2009written authorization of <strong>Embraer</strong>. The information, technical data, designs and drawings disclosed in this docu−ment are proprietary information of <strong>Embraer</strong> or third parties and shall not be used or disclosed to any third partyThe figure 1 shows the GHSH manual structure.GROUND HANDLING ANDSERVICING HANDBOOK<strong>EMB</strong>−<strong>505</strong>HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.GROUND HANDLINGANDSERVICING HANDBOOKCUSTOMER COMMENT FORMLIST OF EFFECTIVE AIRCRAFTLIST OF EFFECTIVE PAGESINTRODUCTION TITLEINTRODUCTIONPROCEDURES TITLE PAGEPROCEDURES TABLE OF CONTENTSPROCEDURESAPPENDIX TITLE PAGEGROUND SUPPORT EQUIPMENT APPENDIXTITLE PAGEGSE APPENDIX TABLE OF CONTENTSGROUND SUPPORT EQUIPMENTSCONSUMABLE PRODUCTS APPENDIXTITLE PAGECONSUMABLE PRODUCTS APPENDIXEM500ENGHSH000024A.DGNGHSH Manual StructureFigure 1EFFECTIVITY: ALLINTRODUCTIONPage INTRO-6NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKD. Revisions(1) Revisions to the GHSH are issued for the whole manual.(2) A list of effective pages is provided for the whole manual. The pages thatare revised, added, or deleted by the current revision will be identified onthe list of effective pages by an asterisk.(3) When texts or art in illustrations are revised, a black bar will appear in thepage left-side margin, beside the revised, added, or deleted material. ForPDF files, a bar beside the page number or the section title and the printingdate indicates that neither the text nor the illustration has beenchanged, but the material has been relocated to a different page or atotally new page has been added.D. Tools, Equipment and Auxiliary Items(1) Aircraft Zones (Figure 2)The GHSH procedures may refer to a zone to give the references necessaryfor the identification of the service areas or components. The figure 2illustrates the zones location.HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALLINTRODUCTIONPage INTRO-7NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKEM500ENGHSH000023A.DGNHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.<strong>EMB</strong> − <strong>505</strong>Aircraft ZonesFigure 2EFFECTIVITY: ALLINTRODUCTIONPage INTRO-8NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOK(2) Consumable MaterialsThe consumable material used in the GHSH procedures are describe inthe Consumable Appendix, localized in the end of the manual.(3) Circuit Breakers (Figure 3) (Figure 4) (Figure 5)The circuit breakers used in the GHSH procedures appear in the followway:"TOILET FLUSH-RHCBP (SHED BUS)"where:(a) TOILET FLUSH identifies the designation;(b) RHCBP identifies the location of the circuit breaker. On the example,the circuit breaker is located in right (RH) circuit breaker panel (CBP).(c) (SHED BUS) identifies the bus.The figure 3 and figure 4 shows the circuit breaker panels location on theaircraft.HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALLINTRODUCTIONPage INTRO-9NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.BAALH CB PANELEMERGENCY BUSDC BUS 1HOT BUS 1 SHED BUS 1RH CB PANELDC BUS 2EMERGENCY BUSSHED BUS 2 HOT BUS 2BEM500ENGHSH000020A.DGNRH and LH Circuit Breaker Panels LocationFigure 3EFFECTIVITY: ALLINTRODUCTIONPage INTRO-10NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKZONES241242BZONE212 CADBELPDUEPDUACHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.DRPDUEEM500ENGHSH000021A.DGNEPDU, RPDU and LPDU LocationFigure 4EFFECTIVITY: ALLINTRODUCTIONPage INTRO-11NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.AZONES231232MONUMENTPARTITIONLH SECONDARYCB PANELSRH SECONDARYCB PANELSAEM500ENGHSH000022A.DGNRH and LH Secondary CB Panels LocationFigure 5EFFECTIVITY: ALLINTRODUCTIONPage INTRO-12NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKPROCEDURESHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.

GROUND HANDLING ANDSERVICING HANDBOOKGHSH PROCEDURES - TABLE OF CONTENTSSUBJECTCHAPTERSECTIONSUBJECTTASK NUMBERPAGETowing & TaxingTowing with Towbar -Procedure......................................... 09-10-01-500-801-A 201Parking, Mooring, Storage &Return to ServiceParking - MaintenancePractices .......................................... 10-10-00-500-801-A 201Parking in Cold Weather Condition -Maintenance Practices..................... 10-10-00-500-802-A 201Aircraft Mooring - MaintenancePractices .......................................... 10-20-00-500-801-A 201Return-to-Service after NormalParking - Maintenance Practices ...... 10-30-00-500-801-A 201Cold Weather - MaintenancePractices .......................................... 10-30-00-500-802-A 201ServicingFuel Tank - Refueling ....................... 12-11-00-650-801-A 301HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.Fuel Tank - Defueling ....................... 12-11-00-650-802-A 301Fuel Tank - Pressure Refueling..........12-11-00-650-803-A 301Fuel Tank - Draining......................... 12-11-00-680-801-A 301Engine Oil Level - VisualCheck............................................... 12-12-00-210-801-A 301EFFECTIVITY: ALLGHSH Procedures - Table of ContentsPage TOC-1NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKSUBJECTCHAPTERSECTIONSUBJECTTASK NUMBERPAGEEngine Oil - Filling............................ 12-12-00-612-801-A 301Servicing of NLG and MLGTires ................................................. 12-14-00-610-801-A 301HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.Water Tank - Servicing ..................... 12-15-01-613-801-A 301WasteTank - Servicing ..................... 12-15-03-600-801-A 301External Aircraft - Cleaning .............. 12-23-00-100-801-A 301Internal Aircraft - Cleaning ............... 12-23-00-100-802-A 301Standard Practices-AirframeAircraft Maintenance SafetyProcedures....................................... 20-00-00-910-801-A 201Static Grounding - StandardPractices .......................................... 20-40-02-910-801-A 201Electrical PowerMain Battery - Removal.................... 24-36-01-000-801-A 401Main Battery - Disconnection ........... 24-36-01-000-802-A 401Main Battery - Installation................. 24-36-01-400-801-A 401Main Battery - Connection................ 24-36-01-400-802-A 401Energization of the Aircraft with anExternal DC Power Supply - Aircraft/SystemConfiguration............... 24-41-00-860-801-A 201Aircraft De-energization - Aircraft/System Configuration....................... 24-41-00-860-802-A 201EFFECTIVITY: ALLGHSH Procedures - Table of ContentsPage TOC-2NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKFlight ControlsSUBJECTCHAPTERSECTIONSUBJECTTASK NUMBERPAGETrim Actuator Controller -Operational Test............................... 27-04-01-710-801-A 501FuelFuel - Maintenance and ServicingPractices .......................................... 28-00-00-910-801-A 201Hydraulic PowerMain Hydraulic System -Depressurization .............................. 29-10-00-910-801-A 201Main Hydraulic System -Pressurization .................................. 29-10-00-910-802-A 201Landing GearLanding-Gear Safety Pin -Standard Practices........................... 32-00-00-910-801-A 201NLG and MLG Tires - GeneralVisual Inspection .............................. 32-45-00-210-801-A 601Engine Start Procedure .....................71-00-01-910-803-A 201HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALLGHSH Procedures - Table of ContentsPage TOC-3/4NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKGHSH TASK 09-10-01-500-801-A1. Towing With Towbar - ProcedureA. General(1) The aircraft towing is the usual procedure when it is necessary to movethe aircraft on the ground.B. Job Set-UpWARNING: MAKE SURE THAT THE AIRCRAFT IS IN A SAFECONDITION BEFORE YOU DO THE MAINTENANCEPROCEDURES. THIS IS TO PREVENT INJURY TOPERSONS AND/OR DAMAGE TO THE EQUIPMENT.(1) Make sure that the landing gear safety pins are installed (GHSH TASK 32-00-00-910-801-A/200).NOTE: The use of safety pins on MLG and NLG is optional when youtow or push the aircraft. This occurs when the aircraft is inposition for the flight crew to taxi before or after a flight.CAUTION: REMOVE ALL TOOLS, EQUIPMENT, AND MATERIALSFROM THE TOWING AREA. MAKE SURE THAT THE AREAIS CLEAN.(2) Before you start the towing operation, remove the unnecessary objectsfrom around the aircraft.(3) Make sure that aircraft is in safe condition before the towing procedure.NOTE: If the aircraft had a flat tire while parked or moving on theground, you must replace this tire because it is permanentlydamaged.WARNING: BEFORE YOU DO THE TOWING PROCEDURE, MAKESURE THAT THE LOWER PART OF THE TORQUE LINKIS DISCONNECTED. IF YOU DO NOT OBEY THISPRECAUTION, DAMAGE TO THE NLG AND INJURY TOPERSONS CAN OCCUR.(4) Disconnect the torque link from the nose landing gear (Figure 201) as follows:(a) Remove the quick disconnect pin.(b) Install the torque link to the upper support.(c) Install the torque-link quick disconnect pin to the upper support.(5) Install the towbar head (GSE 026 ) to the towbar (GSE 027) (Figure 202).NOTE: Make sure that the shear pin of the towbar head is in goodcondition.(6) Connect the towbar head (GSE 026) to the Nose Landing Gear tow fittingas follows:HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL 09-10-01-500-801-A/200Page 201Rev.01 - MAY 28/10Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.(a) Pull the handle.(b) Connect the towbar head to the nose landing gear tow fitting.(c) Release the handle to lock the towbar head to the NLG tow fitting.(7) Connect the other end of the towbar (GSE 027) to the tractor.C. Towing with Towbar(1) Make sure that the emergency/parking brake is released.CAUTION: THE MAXIMUM SPEED RECOMMENDED FOR AIRCRAFTTOWING IS THE WALKING SPEED. A TECHNICIAN MUSTCOME ALONG WITH THE AIRCRAFT TO PUT WHEELCHOCKS AGAINST THE WHEELS AFTER COMPLETIONOF THE TOWING OR IN CASE OF AN UNEXPECTED STOP.IF YOU DO NOT OBEY THIS PRECAUTION, DAMAGE TOTHE AIRCRAFT CAN OCCUR.(2) Tow the aircraft slowly straight ahead before you try to turn.NOTE: If during the towing operation the towbar head (GSE 026)shear pin is broken, do an inspection of the NLG for damageand replacement of the shear pin.(3) Brake Assembly - Inspection (Figure 203)WARNING: MAKE SURE THAT THE AIRCRAFT IS IN A SAFECONDITION BEFORE YOU DO THE MAINTENANCEPROCEDURES. THIS IS TO PREVENT INJURY TOPERSONS AND/OR DAMAGE TO THE EQUIPMENT.(a) Make sure that the wheel chocks are in position against the landinggear wheels.(b) In the cockpit, make sure that the landing-gear control lever is in theDN position.(c) Use a flashlight and a mirror, if necessary, to examine these componentsof the NLG:• Main fitting• Sliding tube• Retraction actuator• Locking stay• Downlock release actuator• Downlock proximity switch• Bonding jumpers• Torque links• Shimmy damper• Drag brace• Doors• Door mechanismEFFECTIVITY: ALL 09-10-01-500-801-A/200Page 202NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOK• Grounding CableNOTE:Make sure that the grounding cable end touches theground. If it does not touch the ground, adjust its length.(d) Make sure that these components show no signs of:• Mechanical damage• Unsatisfactory installation• Surface corrosion• Damage to the surface finish• Loose or missing items(e) Examine these components for leakage of hydraulic fluid:• Sliding tube• Downlock release actuator• Shimmy damper• Retraction actuatorD. Job Close-UpCAUTION: THE EFFECT OF THE PARKING BRAKE CONTINUES FOR48 HOURS AFTER THEY ARE SET. AFTER THIS YOU MUSTRELEASE THE EMERGENCY PARKING BRAKE HANDLE. IFYOU DO NOT OBEY THIS PRECAUTION, THE BRAKE PADSMAY STICK TO THE BRAKE DISC AND DAMAGE TO THEEQUIPMENT CAN OCCUR.(1) Apply the emergency/parking brake (brakes on).(2) Remove the towbar (GSE 027) from the tractor (Figure 202).(3) If the nose wheel is not in the zero-degree position, align it with the zerodegreereference in the NLG.(4) Remove the towbar head (GSE 026) from the NLG tow fitting.(5) Connect the torque link back to its initial position as follows (Figure 201):(a) Remove the quick disconnect pin from the upper support.(b) Connect the torque link to the NLG.(c) Install the torque-link quick disconnect pin.HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL 09-10-01-500-801-A/200Page 203NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKAZONE711BHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.TORQUE−LINK QUICKDISCONNECT PINCBTORQUE LINKTORQUE−LINK QUICKDISCONNECT PINASUPPORTCEM500ENGHSH090010A.DGNTorque Link - TowingFigure 201EFFECTIVITY: ALL 09-10-01-500-801-A/200Page 204NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKAZONE711ASHEARPINDTOWBAR(GSE 027)SAFETYBOLTSTOWBARHEAD (GSE 026)BDBHOOKCTOWBARHEAD (GSE 026)HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.STOPCHANDLEEM500ENGHSH090011A.DGNTowbar - TowingFigure 202EFFECTIVITY: ALL 09-10-01-500-801-A/200Page 205NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKAZONE711HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.RETRACTIONACTUATORTORQUE LINKJACKING GSEATTACHMENT POINTLOCKING STAYSLIDING TUBEDRAG BRACEFORKSHIMMY DAMPERWHEEL/TIREDOWNLOCKRELEASEACTUATORUPLOCK BOXUPLOCK BOX AND TOWBARATTACHMENT POINTAEM500ENGHSH320025A.DGNNLG - General Visual InspectionFigure 203EFFECTIVITY: ALL 09-10-01-500-801-A/200Page 206NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKGHSH TASK 10-10-00-500-801-A1. Normal Parking - Maintenance PracticesA. General(1) This task gives the procedure to do the aircraft normal parking.(2) Normal parking includes overnight parking and parking from 0 to 7 days.B. Job Set-Up(1) Make sure that there is sufficient room in the aircraft parking area, to permitits movement.NOTE: We recommend that the aircraft be sheltered in the hangar.(2) Tow the aircraft into the position specified for parking (GHSH TASK 09-10-01-500-801-A/200).NOTE: • If possible, park the aircraft headed into the wind.• Before you park the aircraft, move it in straight line forapproximately 3 meters. This will remove all torsionalstresses applied to the landing gear components and tiresduring a turn.(3) Make sure that the flaps are in neutral position.(4) Release the emergency/parking brake.(5) Make sure that the LG safety pins are installed.C. Normal Parking - Maintenance Practices(1) Put the wheel chocks against the LG wheels.(2) If the aircraft will stay parked outside the hangar, do as follows:CAUTION: IF UNFAVOURABLE WEATHER CONDITIONS SUCH ASTHUNDERSTORMS AND STRONG WINDS ARE FORE-CAST, MAKE SURE THAT THE AIRCRAFT IS PROPERLYAND SAFELY PARKED. IF YOU DO NOT OBEY THIS PRE-CAUTION, DAMAGE TO THE AIRCRAFT CAN OCCUR.CAUTION:THE AIRCRAFT MUST BE SHELTERED IN THE HANGARWHEN THERE ARE WIND VELOCITIES OF 55 KNOTSOR MORE. IF YOU DO NOT OBEY THIS PRECAUTION,DAMAGE TO THE AIRCRAFT CAN OCCUR.(a) Look for the wind velocity chart best suitable for the floor condition inFigure 203, and, if the wind velocity is out of the limits, refer to AMMTASK 10-20-00-500-801-A/200 to moor the aircraft.NOTE:Perform frequent visual inspections of the mooring ropesand wheel chocks.(b) Install the cockpit transparency shade set (GSE 029).HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL 10-10-00-500-801-A/200Page 201NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.(c) Close the window shades.(d) Set the gust locks. Refer to AMM SDS 27-70-00.(e) Install the covers to these parts:1. Pitot-static probe (GSE 003).2. IASP - (Integrated air data and stall protection probe)(f) Install the engine covers (GSE 030) as follows (Figure 202, Sheet 3):1. Install the engine air inlet plug to engine air inlet.2. Install the engine exhaust outlet plug perpendicular to engine air outlet.3. Put the plug into the correct position and pull it back through the handle.(g) Cover the outlet and inlet openings that follow with a cotton fabric or equivalentattached to the aircraft skin with adhesive tape:1. Ground cooling fan inlet.2. Ground cooling fan exhaust.3. Condenser fan inlet.4. Condenser fan exhaust.5. Ram-air inlet.(h) Close all the doors and access panels.(i) Make sure that wheel chocks are installed.(j) Where there are freezing or ice conditions, do the subsequent step:1. Remove, drain and storage the waste tank. Refer to GHSH TASK12-15-03-600-801-A/300.NOTE: For matter of hygiene, we recommend that the wastetank be serviced.2. Drain the water tank. Refer to GHSH TASK 12-15-03-600-801-A/300.EFFECTIVITY: ALL 10-10-00-500-801-A/200Page 202Rev.01 - MAY 28/10Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKDBAGUST LOCKSAFETY PINZONES223224PILOT CONTROLYOKE (REF.)PITOT−STATICCOVER (GSE 003)CEIASP COVER(GSE 052)AILERON/ELEVATOR ANDRUDDER GUST LOCKBADEECEM500ENGHSH100020A.DGNHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.Normal Parking - Maintenance PracticesFigure 201EFFECTIVITY: ALL 10-10-00-500-801-A/200Page 203NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKZONES430440ZONES223224ECGHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.AZONES711721731BTYPICALWHEELCHOCKSZONE351COCKPIT TRANSPARENCYSHADE SET (GSE 029)BDATYPICALCDDEM500ENGHSH100019A.DGNNormal Parking - Maintenance PracticesFigure 202 - Sheet 1EFFECTIVITY: ALL 10-10-00-500-801-A/200Page 204NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKFRAM AIR INLETCOVER (REF.)GROUNDCOOLINGFAN INLETCONDENSERFAN INLETGROUNDCOOLINGFAN OUTLETFRAM AIR INLETCOVER (REF.)ENGINE COVERS(GSE 030)CONDENSERFAN OUTLETEENGINE COVERS(GSE 030)HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.ENGINE COVERS(GSE 030)GEM500ENGHSH100021A.DGNNormal Parking - Maintenance PracticesFigure 202 - Sheet 2EFFECTIVITY: ALL 10-10-00-500-801-A/200Page 205NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOK1ENGINE AIR INLET (REF.)STARTERGENERATORVENT OUTLET (REF.)ENGINEPLUG−AIRINLETHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.STARTERGENERATORAIR INLET (REF.)INSTALL THE ENGINE PLUG−AIR INLET TO THEENGINE AIR INLET, STARTER GENERATOR AIRINLET AND STARTER GENERATOR VENT OUTLET.3ENGINE AIROUTLET (REF.)2ENGINEPLUG−EXHAUSTOUTLETAINSTALL THE ENGINE PLUG−EXHAUSTOUTLET PERPENDICULAR TOTHE ENGINE AIR OUTLET.ENGINE AIROUTLETAHANDLEAPUT THE PLUG INTO THE CORRECTPOSITION AND PULL IT BACK THROUGH THEHANDLE.EM500ENGHSH710003A.DGNNormal Parking - Maintenance PracticesFigure 202 - Sheet 3EFFECTIVITY: ALL 10-10-00-500-801-A/200Page 206Rev.01 - MAY 28/10Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKWIND (knot)63626160595857565554535251504948474645444342414039383736353433323130292827262524232221201918171615146600 kgf6350 kgf5600 kgf5150 kgf3400 kgf8150 kgf7650 kgf6850 kgf8200 kgfNOTE: CALCULATION VALID FORFLAP 0° CONDITION ONLY.IT IS MANDATORY THAT AIRCRAFTFLAPS BE SET TO 0° PRIORTO PARKING WITH NO TIE−DOWN.0 2 4 6 8 10 12 14 16 18 20 22 24 26 28 30 32 34 36 38 40 42 44 46 48 50 52 54 56CG POSITION (% MAC)WIND VELOCITY VS. CG POSITION − DRY FLOORWEIGHT (kgf)EM500ENGHSH100022A.DGNHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.Wind Velocity ChartsFigure 203 - Sheet 1EFFECTIVITY: ALL 10-10-00-500-801-A/200Page 207Rev.01 - MAY 28/10Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.WIND (knot)5857565554535251504948474645444342414039383736353433323130292827262524232221201918171615146600 kgf6350 kgf5150 kgf3400 kgf8150 kgf7650 kgf5600 kgf6850 kgf8200 kgfNOTE: CALCULATION VALID FORFLAP 0° CONDITION ONLY.IT IS MANDATORY THAT AIRCRAFTFLAPS BE SET TO 0° PRIORTO PARKING WITH NO TIE−DOWN.130 2 4 6 8 10 12 14 16 18 20 22 24 26 28 30 32 34 36 38 40 42 44 46 48 50 52 54 56CG POSITION (% MAC)WIND VELOCITY VS. CG POSITION − WET FLOORWEIGHT (kgf)EM500ENGHSH100023A.DGNWind Velocity ChartsFigure 203 - Sheet 2EFFECTIVITY: ALL 10-10-00-500-801-A/200Page 208Rev.01 - MAY 28/10Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKWIND (knot)5453525150494847464544434241403938373635343332313029282726252423222120191817161514136600 kgf6350 kgf5150 kgf3400 kgf5600 kgf8150 kgf7650 kgf6850 kgf8200 kgfNOTE: CALCULATION VALID FORFLAP 0° CONDITION ONLY.IT IS MANDATORY THAT AIRCRAFTFLAPS BE SET TO 0° PRIORTO PARKING WITH NO TIE−DOWN.120 2 4 6 8 10 12 14 16 18 20 22 24 26 28 30 32 34 36 38 40 42 44 46 48 50 52 54 56CG POSITION (% MAC)WIND VELOCITY VS. CG POSITION − SNOWY FLOORWEIGHT (kgf)EM500ENGHSH100024A.DGNHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.Wind Velocity ChartsFigure 203 - Sheet 3EFFECTIVITY: ALL 10-10-00-500-801-A/200Page 209Rev.01 - MAY 28/10Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOK3231307650 kgf8150 kgf8200 kgfHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.WIND (knot)292827262524232221201918171615141312111009086600 kgf3400 kgf6350 kgf5150 kgf5600 kgf6850 kgfNOTE: CALCULATION VALID FORFLAP 0° CONDITION ONLY.IT IS MANDATORY THAT AIRCRAFTFLAPS BE SET TO 0° PRIORTO PARKING WITH NO TIE−DOWN.WEIGHT (kgf)070 2 4 6 8 10 12 14 16 18 20 22 24 26 28 30 32 34 36 38 40 42 44 46 48 50 52 54 56CG POSITION (% MAC)WIND VELOCITY VS. CG POSITION − ICY FLOOREM500ENGHSH100025A.DGNWind Velocity ChartsFigure 203 - Sheet 4EFFECTIVITY: ALL 10-10-00-500-801-A/200Page 210Rev.01 - MAY 28/10Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKGHSH TASK 10-10-00-500-802-A1. Normal Parking in Cold Weather Conditions - Maintenance PracticesA. General(1) This task gives the procedure for normal parking in cold weather condition.(2) A cold weather condition is when the temperature is lower than 0°C(32°F).(3) Normal Parking in cold weather includes overnight parking.B. Job Set-Up(1) Obey the procedures given in GHSH TASK 10-10-00-500-801-A/200.C. Normal Parking in Cold Weather Condition - Maintenance Practices(1) If the parking area has ice or snow, put one of these items under the tires,as applicable:(a) A mat, or(b) A layer of thick sand or(c) Other applicable material.NOTE: This will prevent the freezing of the tires to the ground.CAUTION: WHILE THE AIRCRAFT IS PARKED, EXAMINE THE WINGSAND STABILIZERS AT REGULAR INTERVALS AND, IFNECESSARY, APPLY DEICING/ANTI-ICING FLUIDS TOTHESE AREAS. YOU MUST ALSO EXAMINE FOR THEPRESENCE OF DEICING/ANTI-ICING FLUID RESIDUES INHIDDEN PLACES OF THE WINGS AND STABILIZERS AND,IF NECESSARY, REMOVE THESE RESIDUES. IF YOU DONOT OBEY THIS PRECAUTION, DAMAGE TO THE AIR-CRAFT CAN OCCUR.CAUTION: REPETITIVE APPLICATION OF THICKENED DEICING/ANTI-ICING FLUID CAN CAUSE THE FORMATION/BUILDUP OF DRIED RESIDUES. DRIED RESIDUES CANOCCUR WHEN SURFACES ARE TREATED BUT THE AIR-CRAFT DOES NOT FLY SUBSEQUENTLY, AND IS NOTSUBJECT TO PRECIPITATION. AN APPROPRIATEINSPECTION AND CLEANING PROGRAM MUST BEESTABLISHED.(2) Perform frequent visual inspections not to permit accumulation of snow orice on the aircraft.(3) Make sure that the wheel chocks are installed to the LG wheels.(4) Make sure that you obeyed the procedures for waste tank given in GHSHTASK 10-10-00-500-801-A/200.(5) Make sure that you obeyed the procedures for water tank given in GHSHTASK 10-10-00-500-801-A/200.(6) If the temperature is foreseen to be less than -18 °C (0 °F), remove themain battery (GHSH TASK 24-36-01-000-801-A/400).HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL 10-10-00-500-802-A/200Page 201/202NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKGHSH TASK 10-20-00-500-801-A1. Aircraft Mooring - Maintenance PracticesA. General(1) The mooring procedure must be performed only when required in GHSHTASK 10-10-00-500-801-A/200 normal parking procedures.(2) This task gives the procedure to moor the aircraft.(3) There is one mooring point on each MLG, one on the NLG, and one on therear fuselage.B. Job Set-Up(1) Tow the aircraft to the parking area where there are tiedown anchors(GHSH TASK 09-10-01-500-801-A/200).(2) Refer to Figure 201 for mooring points coordinates.(3) Do the procedures to make the aircraft safe for maintenance (GHSH TASK20-00-00-910-801-A/200).(4) Do the normal parking procedure (GHSH TASK 10-10-00-500-801-A/200).C. Mooring - Maintenance Practices (Figure 202)CAUTION: THE AIRCRAFT MUST BE SHELTERED IN THE HANGARWHEN THERE ARE WIND VELOCITIES OF 65 KNOTS ORMORE. IF YOU DO NOT OBEY THIS PRECAUTION, DAMAGETO THE AIRCRAFT CAN OCCUR.(1) Moor the aircraft in the parking area with nylon rope.(2) Attach the nylon rope to the mooring point and attach the anchor with abowline knot.HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL10-20-00-500-801-A/200Page 201NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKYHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.NOTES:ABCDEFGHABXX− 0.46m (−1.5ft) UP TO 0.46m (1.5ft)− 0.46m (−1.5ft) UP TO 0.46m (1.5ft)X− THE NYLON ROPES SHALL BE ARRANGED WITHIN THE SHADED AREA.− TO MARK THE TIEDOWN POINTS ON THE GROUND, USE THE NOSE LANDINGGEAR WHEEL TIRE FOOT PRINT AS THE ZERO REFERENCE POINT.CDMAXIMUM 6.32m (20.73ft)MAXIMUM 6.32m (20.73ft)MINIMUM 6.76m (22.17ft)MINIMUM 6.76m (22.17ft)XEFGHNLG TIEDOWN POINTSMLG TIEDOWN POINTSREAR FUSELAGE TIEDOWN POINTS9.55m (31.33ft) UP TO 11.51m (37.76ft)9.55m (31.33ft) UP TO 11.51m (37.76ft)YMINIMUM 0.63m (2.0ft)MINIMUM −0.63m (−2.0ft)Y1.27m (4.16ft) UP TO 1.42m (4.65ft)−1.27m (−4.16ft) UP TO −1.42m (−4.65ft)1.27m (4.16ft) UP TO 1.42m (4.65ft)−1.27m (−4.16ft) UP TO −1.42m (−4.65ft)YMINIMUM 1.19m (3.9ft)MINIMUM −1.19m (−3.9ft)EM500ENGHSH100014A.DGNMooring Points CoordinatesFigure 201EFFECTIVITY: ALL10-20-00-500-801-A/200Page 202NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKCABZONE711ZONE231ZONES721731BMOORINGPOINTMAIN LANDINGGEAR (REF.)ENOSE LANDINGGEAR (REF.)CMOORINGPOINTNYLONROPEAMOORINGPOINTFDHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.DNYLONROPEEFNYLONROPEEM500ENGHSH100015B.DGNMooring PointsFigure 202EFFECTIVITY: ALL10-20-00-500-801-A/200Page 203NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOK1 2HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.35 6BOWLINEKNOT4MOORINGATTACHMENTPOINTEM500ENGHSH100002A.DGNAircraft Mooring RopesFigure 203EFFECTIVITY: ALL10-20-00-500-801-A/200Page 204NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKGHSH TASK 10-30-00-500-801-A1. Return-to-Service after Normal Parking - Maintenance PracticesA. General(1) This task gives the procedure to return the aircraft to service after normalparking.B. Return-to-Service after Normal Parking(1) Remove the wheel chocks.(2) Make sure that the LGCL (Landing Gear Control Lever) is in down position.(3) Do the steps below if the aircraft is parked outside the hangar.(a) If applicable, unground the aircraft (GHSH TASK 10-20-00-500-801-A/200).(b) Remove cockpit transparency shade set.(c) Release the gust lock.(d) Remove these covers from these parts:1. Pitot-static probe (GSE 003).2. IASP - (Integrated air data and stall protection probe).3. Engine (GSE 030).(e) Remove the covers and the adhesive tapes from these parts:1. Ground cooling fan inlet.2. Ground cooling fan exhaust.3. Condenser fan inlet.4. Condenser fan exhaust.5. Ram air inlet.(f) Refill and install the waste tank, if applicable (GHSH TASK 12-15-03-600-801-A/300).(g) Do the water tank servicing (GHSH TASK 12-15-01-613-801-A/300).(h) If the aircraft stayed parked for exactly 7 days, do this additional step:1. Drain the fuel tanks to check for presence of water (GHSHTASK12-11-00-680-801-A/300.(i) Tow the aircraft from the parking area (GHSH TASK 09-10-01-500-801-A/200).(j) Do a visual inspection of the pitot-static probe and the IASP for:1. Damage2. Obstruction3. Foreign objects(l) Make sure that there is no obstruction and foreigner objects in theNACA air intakes of wing tanks.HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL10-30-00-500-801-A/200Page 201NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKDBAHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.GUST LOCKSAFETY PINZONES223224PILOT CONTROLYOKE (REF.)PITOT−STATICCOVER (GSE 003)CEIASP COVER(GSE 052)AILERON/ELEVATOR ANDRUDDER GUST LOCKBADEECEM500ENGHSH100020A.DGNNormal Parking - Maintenance PracticesFigure 201EFFECTIVITY: ALL10-30-00-500-801-A/200Page 202NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKZONES430440ZONES223224ECGAZONES711721731BTYPICALWHEELCHOCKSZONE351COCKPIT TRANSPARENCYSHADE SET (GSE 029)BDATYPICALCDHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.DEM500ENGHSH100019A.DGNNormal Parking - Maintenance PracticesFigure 202 - Sheet 1EFFECTIVITY: ALL10-30-00-500-801-A/200Page 203NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKFRAM AIR INLETCOVER (REF.)GROUNDCOOLINGFAN INLETHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.CONDENSERFAN INLETGROUNDCOOLINGFAN OUTLETFRAM AIR INLETCOVER (REF.)ENGINE COVERS(GSE 030)CONDENSERFAN OUTLETEENGINE COVERS(GSE 030)ENGINE COVERS(GSE 030)GEM500ENGHSH100021A.DGNNormal Parking - Maintenance PracticesFigure 202 - Sheet 2EFFECTIVITY: ALL10-30-00-500-801-A/200Page 204NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKGHSH TASK 10-30-00-500-802-A1. Return-to-Service after Normal Parking in Cold Weather Condition - MaintenancePracticesA. General(1) This task gives the procedures to return the aircraft to service after normalparking in cold weather condition.B. Job Set-Up(1) Obey the procedures given in GHSH TASK 10-30-00-500-801-A/200.C. Return-to-Service after Normal Parking in Cold Weather Condition MaintenancePractices(1) Remove ice, frost, slush, or snow from the aircraft surfaces (GHSH TASK12-23-00-100-801-A/300).(2) Install the batteries, if applicable (GHSH TASK 24-36-01-400-801-A/400).(3) Install the waste tank, and do the servicing (GHSH TASK 12-15-03-600-801-/300).(4) Do a check of the portable fire extinguishers as follows (Figure 201):(a) Open the clamp and remove the portable fire extinguisher.(b) Examine the portable fire extinguisher and make sure that the nozzleis not clogged.(c) Examine the extinguisher for exterior damage and corrosion.(d) Examine the frangible green seal. Make sure that it is in position andnot damaged.(e) Install the portable fire extinguisher on its support and close the clampthat attaches it.(5) Do a check of the oxygen cylinder pressure. If necessary, do the servicingof the oxygen system.(a) Do the servicing of the oxygen system as follows (Figure 202):NOTE: Use aviator's breathing oxygen only (MIL-O-27210, type 1).1. Do a check of the overboard discharge indicator before you fill theoxygen cylinder to make sure that the oxygen did not discharge.2. Remove the protective cap from the fill valve.3. Connect the high pressure oxygen servicing regulator to the oxygensource.4. Connect the high pressure oxygen servicing regulator to the fillingvalve and make sure that there is no leak.5. Measure the ambient temperature (OAT - Outside Air Temperature).6. With the OAT, find the filling pressure. Refer to Figure 203.NOTE: The system filling pressure is 12755.3 kPa (1850 psig)at OAT of 21 °C (70 °F).HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL10-30-00-500-802-A/200Page 201NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.7. Slowly fill the oxygen cylinder up to the recommended pressure.NOTE: Slowly fill the system at a rate not greater than 1378.95kPa (200 psig) to prevent heating in the system and,consequently, an incorrect pressure indication.8. Monitor the pressure gauge of the aircraft and of the high pressureoxygen servicing regulator.9. Wait at least 10 minutes to let the temperature of the oxygen cylinderbecome stable.10. Close the high pressure oxygen servicing regulator shutoff valve.11. Carefully disconnect and remove the high pressure oxygen servicingregulator from the fill valve to release the remaining pressurein the hose.(b) Do a leak test on the fill valve.1. Use fluid Leak-Tec 16-OX (Refer to Consumable Products Appendix)on the connection to do the leak test. If there are leaks, replacethe fill valve.(6) Do a check of the engine oil level (GHSH TASK 12-12-00-210-801-A/300).(7) Do a check of the pressure of the MLG (Main Landing Gear) and NLG(Nose Landing Gear) tires (GHSH TASK 32-45-00-210-801-A/600) and(GHSH TASK 12-14-00-610-801-A/300).(8) Do a check of the hydraulic system. If necessary, do the servicing. Pleaseuse the contact information given in the GHSH Introduction for the applicablemaintenance action.(9) Do a check to make sure that the primary control surfaces and the trimtabs operate correctly. Please use the contact information given in theGHSH Introduction for the applicable maintenance action.(10) Do a check of the rain repellent coating. Please use the contact informationgiven in the GHSH Introduction for the applicable maintenance action.(11) Make sure that there is no obstruction and foreigner objects in the NACAair intakes of wing tanks.(12) If the aircraft stayed parked for exactly 7 days, do this additional step:(a) Drain the fuel tanks to check for presence of water (GHSH TASK 12-11-00-680-801-A/300).(13) To start the engines after normal parking in cold weather conditions, referto engine starting procedure (cold weather). Please contact <strong>Embraer</strong> Supportfor the applicable maintenance action.EFFECTIVITY: ALL10-30-00-500-802-A/200Page 202NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKAZONE224AZONE231BRACKET(REF.)PORTABLE FIREEXTINGUISHERHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.CLAMP (2x)ATYPICALEM500ENGHSH100016A.DGNPortable Fire ExtinguisherFigure 201EFFECTIVITY: ALL10-30-00-500-802-A/200Page 203NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.AZONES211811BOXYGEN PRESSUREREGULATOROVERBOARD DISCHARGEINDICATOR (REF.)CAFILLVALVEBPROTECTIVECAPOXYGENSOURCE (REF.)COXYGENPRESSUREGAUGEEM500ENGHSH100017A.DGNOxigen CylinderFigure 202EFFECTIVITY: ALL10-30-00-500-802-A/200Page 204NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKCORRECTED OXYGEN PRESSUREAT 21°C (70°F) − PSI2200210021°CINDICATED GAUGE PRESSURE − PSI20001900180017001600150014001300120011001000900800700600500400300200−40160012001000−30 −20 −10 0 10 20 30 40 50 60CYLINDER COMPARTMENT TEMPERATURE − °C−40 −22 −4 −14 32 50 68 86 104 122 140CYLINDER COMPARTMENT TEMPERATURE − °F18501400800600400320EM500ENGHSH100018A.DGNHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.ChartFigure 203EFFECTIVITY: ALL10-30-00-500-802-A/200Page 205/206NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKGHSH TASK 12-11-00-650-801-A1. Fuel Tank - RefuelingA. General(1) This task gives the procedure to refuel the aircraft by gravity.(2) These fuels are approved by <strong>Embraer</strong>:• Fuel JET A-1 (Refer to Appendix C - Consumable Materials)• Fuel JET A (Refer to Appendix C - Consumable Materials)• Fuel JP-8 (Refer to Appendix C - Consumable Materials)(3) These fuel additives are approved by <strong>Embraer</strong>:• DIETHYLENE GLYCOL MONOMETHYL ETHER (Refer to Appendix C -Consumable Materials).• CORROSION INHIBITOR/LUBRICITY ADDITIVE - MIL-I-25017 (Referto Appendix C - Consumable Materials).B. Job Set-Up(1) Do the procedure to make the aircraft safe for maintenance (GHSH TASK20-00-00-910-801-A/200).(2) Do the procedure to make the aircraft safe for maintenance of the fuel system(GHSH TASK 28-00-00-910-801-A/200).(3) Statically ground the aircraft (GHSH TASK 20-40-02-910-801-A/200).NOTE: Make all grounding connections between the fuel source, aircraft,and fuel nozzle (refer to the requirements of the localregulatory authorities).(4) Energize the aircraft with an external DC (Direct Current) power supply(GHSH TASK 24-41-00-860-801-A/200).(5) Open the LH (Left-Hand) and RH (Right-Hand) gravity filler caps:(a) Insert the key to the key lock port and turn it counterclockwise to theOPEN position.NOTE: It is not possible to remove the key from the key lock portwhen it is in the OPEN position.(b) Lift the lever of the gravity filler cap and turn it counterclockwise.(c) Pull the gravity filler cap from the gravity filler neck.C. Fuel Tank - Gravity FuelingWARNING: DO NOT LET JET FUEL AND LUBRICATING OILS TOUCHYOU. THESE FLUIDS CAUSE INJURY TO THE SKIN.(1) Put the fueling nozzle into the gravity filler neck.(2) Start the fueling operation and monitor the fuel quantity in the tank on theMFD (Multi-Function Display) fuel synoptic page or on the EICAS (EngineIndication Crew Alert System) fuel indicating area.NOTE: The total fuel-tank capacity is approximately 2976 l (786 gal.).HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL12-11-00-650-801-A/300Page 301NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.(3) Remove the fueling nozzle from the gravity filler neck after you have thecorrect fuel quantity in the tank.D. Job Close-UpCAUTION: WHEN YOU INSERT THE GRAVITY FILLER CAP INTO THEGRAVITY FILLER ADAPTER, MAKE SURE THAT THE LAN-YARD IS CORRECTLY POSITIONED INTO THE ADAPTER.IF YOU DO NOT OBEY THIS PRECAUTION, THE FILLERCAP CAN SMASH THE LANYARD AGAINST THE FILLERADAPTER.(1) Close the LH and RH gravity filler caps:(a) Put the gravity filler cap on the gravity filler neck.(b) Turn the lever on the gravity filler cap clockwise and then turn the lever down.(c) Turn the key clockwise to the CLOSE position and remove the key from thekey lock port.(2) De-energize the aircraft (GHSH TASK 24-41-00-860-802-A/200).(3) Remove the grounding cable(s) from the aircraft (GHSH TASK 20-40-02-910-801-A/200).EFFECTIVITY: ALL12-11-00-650-801-A/300Page 302NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKZONE641ARIB 13RIB 12ZONE541ARIB 12RIB 13CRIB 12BRIB 13LEVERGRAVITYFILLER CAPGRAVITYFILLER CAPGRAVITYFILLERNECKBATYPICALFUELING NOZZLEGRAVITYFILLERNECKHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.CEM500ENGHSH120004B.DGNFuel Tank - RefuelingFigure 301EFFECTIVITY: ALL12-11-00-650-801-A/300Page 303NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKAB87.8 TO 87.8ATR2.5N1% 2.5EICASIGN ITT C ____ ____ IGNOFFOFF55.1 N2% 55.1OIL PRES PSIOIL TEMP CFUELFF PPHFQ LBHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.LEFT TANKANALOGUEFUEL QUANTITYBARLEFTTANK FUELQUANTITYMFD(FUEL SYNOPTIC PAGE)330 KGTOTAL660KGUSED279 KGLEFT FUELQUANTITYTOTAL FUELQUANTITY330 KGTEMP XX CELECBATT1BATT2SPDBRKOAT-237ATRONLGDN0V0VTAKEOFF DATA SETCALTRATELFEOXYATOTAL FUELQUANTITYFUEL USEDDELTA-PCABINFLAPSRIGHT TANK ANALOGUEFUEL QUANTITY BARRIGHT TANK FUELQUANTITYRIGHT FUELQUANTITYBEM500ENGHSH120006B.DGNFuel Tank - IndicatingFigure 302EFFECTIVITY: ALL12-11-00-650-801-A/300Page 304NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKGHSH TASK 12-11-00-650-802-A1. Fuel Tank - DefuelingA. General(1) This task gives the procedure to defuel the aircraft by gravity.(2) The fuel tanks are defueled through the dump valves installed in the lowestpart of each fuel tank, near the wing root and the centerline of the aircraft.B. Job Set-Up(1) Do the procedure to make the aircraft safe for maintenance (GHSH TASK20-00-00-910-801-A).(2) Do the procedure to make the aircraft safe for maintenance of the fuel system(GHSH TASK 28-00-00-910-801-A).(3) Statically ground the aircraft (GHSH TASK 20-40-02-910-801-A).NOTE: Make all grounding connections between the fuel sources, aircraft,and fuel nozzle (refer to the requirements of the localregulatory authorities).(4) Energize the aircraft with an external DC (Direct Current) power supply(GHSH TASK 24-41-00-860-801-A).(5) Open the access door 194BL.WARNING: DO NOT LET JET FUEL AND LUBRICATING OILS TOUCHYOU. THESE FLUIDS CAUSE INJURY TO THE SKIN.(6) Remove the drain valve:(a) Put a container (1 gal.) below the drain valve.(b) Remove the screws from the drain valve.(c) Install two of the removed screws in the drain-valve removal nuts.(d) Pull the drain valve through the screws and remove the drain valvefrom the dump valve.EFFECTIVITY: ALLNOTE: In cold weather, use a pair of pliers to help in the pulling ofthe drain valve.(e) Discard the face seal O-ring.C. Fuel Tank - Gravity DefuelingWARNING: DO NOT LET JET FUEL AND LUBRICATING OILS TOUCHYOU. THESE FLUIDS CAUSE INJURY TO THE SKIN.(1) Install two of the removed screws from the drain valve in the dump valve180° apart from each other.NOTE: Do not tighten the screws fully. Let a gap of approximately 2 -3 mm (0.08 - 0.12 in.) stay between the screw head and thedump valve flange.(2) Push up and turn counter-clockwise the defueling tool (GSE 023) until it isCopyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.12-11-00-650-802-A/300Page 301NOV 20/09HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.

GROUND HANDLING ANDSERVICING HANDBOOKHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.held by the screws installed in the dump valve to open it and defuel the aircraftfuel tank.NOTE: Assembly a hose with proper diameter and a bracket togetherwith the GSE023 and put the other hose end into a suitablefuel container.CAUTION: DO NOT OPERATE THE FUEL PUMP WITHOUT FUEL (DRYOPERATION). DRY OPERATION WILL CAUSE DAMAGE TOTHE SYSTEM.(3) Monitor the defueled quantity on the MFD (Multi-Function Display) fuelsynoptic page or on the EICAS (Engine Indication Crew Alert System) fuelindicating area. When you have the quantity of fuel to be defueled, turnclockwise and pull down the GSE 023 to remove it, close the dump valveand stop the aircraft fuel-tank defueling.(4) Remove the screws from the dump valve.D. Job Close-Up(1) Lubricate a new face seal O-ring with grease DC-33 and install it to thedrain valve.WARNING: DO NOT LET JET FUEL AND LUBRICATING OILS TOUCHYOU. THESE FLUIDS CAUSE INJURY TO THE SKIN.(2) Remove the screws from the drain valve.(3) Put the drain valve in its position, install the screws and torque them to1.36 - 1.69 N.m (12 - 15 lb.in).(4) Close the access door 194BL.(5) De-energize the aircraft (GHSH TASK 24-41-00-860-802-A).(6) Remove the grounding cable(s) from the aircraft (GHSH TASK 20-40-02-910-801-A).EFFECTIVITY: ALL12-11-00-650-802-A/300Page 302NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOK194 BLADUMP VALVEZONES531631DRAIN VALVEREMOVAL NUTSDUMP VALVECLAMPDRAINVALVEBINTO FUEL CONTAINER01 TORQUE: 1.36 − 1.69 N.m (12 − 15 lb.in)01CSCREW (4x)SCREW (2x)DEFUELINGTOOLHOSELOWER WINGSKINEEO−RINGBCDADEM500ENGHSH120010A.DGNHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.Fuel Tank - DefuelingFigure 301EFFECTIVITY: ALL12-11-00-650-802-A/300Page 303NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKAB87.8 TO 87.8ATR2.5N1% 2.5EICASIGN ITT C ____ ____ IGNOFFOFF55.1 N2% 55.1OIL PRES PSIOIL TEMP CFUELFF PPHFQ LBHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.LEFT TANKANALOGUEFUEL QUANTITYBARLEFTTANK FUELQUANTITYMFD(FUEL SYNOPTIC PAGE)330 KGTOTAL660KGUSED279 KGLEFT FUELQUANTITYTOTAL FUELQUANTITY330 KGTEMP XX CELECBATT1BATT2SPDBRKOAT-237ATRONLGDN0V0VTAKEOFF DATA SETCALTRATELFEOXYATOTAL FUELQUANTITYFUEL USEDDELTA-PCABINFLAPSRIGHT TANK ANALOGUEFUEL QUANTITY BARRIGHT TANK FUELQUANTITYRIGHT FUELQUANTITYBEM500ENGHSH120006B.DGNFuel Tank - IndicatingFigure 302EFFECTIVITY: ALL12-11-00-650-802-A/300Page 304NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKGHSH TASK 12-11-00-650-803-A1. Fuel Tank - Pressure RefuelingA. General(1) This task gives the procedure to do the pressure refueling of the aircraft.(2) These fuels are approved by <strong>Embraer</strong>:• Fuel JET A-1 (Refer to Appendix C - Consumable Materials)• Fuel JET A (Refer to Appendix C - Consumable Materials)• Fuel JP-8 (Refer to Appendix C - Consumable Materials)(3) These fuel additives are approved by <strong>Embraer</strong>:• DIETHYLENE GLYCOL MONOMETHYL ETHER• CORROSION INHIBITOR/LUBRICITY ADDITIVE MIL-I-25017NOTE: Obey the fluid manufacture's specifications to find the additiveproportions for each fuel.(4) Use the pressure refueling adapter and the pressure-refueling controlpanel to do this procedure.(5) The pressure-refueling control panel includes a repeater indicator displaywhich has an internal fuel-quantity preselecting system for refueling thetanks.(6) The pressure refueling adapter is installed adjacent to the pressure-refuelingcontrol panel, behind an access door on the right wing-to-fuselage fairing inzone 191.B. Job Set-UpWARNING: MAKE SURE THAT THE AIRCRAFT IS IN A SAFECONDITION BEFORE YOU DO THE MAINTENANCEPROCEDURES. THIS IS TO PREVENT INJURY TOPERSONS AND/OR DAMAGE TO THE EQUIPMENT.(1) Do the procedure to make the aircraft safe for maintenance (GHSH TASK20-00-00-910-801-A).(2) Do the procedure to make the aircraft safe for maintenance of the fuel system(GHSH TASK 28-00-00-910-801-A).(3) Statically ground the aircraft (GHSH TASK 20-40-02-910-801-A).NOTE: Make all grounding connections between the fuel source, aircraft,and fuel nozzle (refer to the requirements of the localregulatory authorities).(4) Energize the aircraft with an external DC power supply (GHSH TASK 24-41-00-860-801-A).NOTE: If an external DC power supply is not available, lift the guardand set the POWER SELECTOR switch to the BATTERYposition on the pressure-refueling control panel.HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL12-11-00-650-803-A/300Page 301NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOK(5) Open access door 191CR.(6) Remove the pressure-refueling adapter cap:(a) Push the lever of the pressure-refueling adapter cap to unlock it andturn it counterclockwise.(b) Remove the pressure-refueling adapter cap from the pressure refuelingadapter.HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.C. Fuel Tank - Pressure RefuelingWARNING: DO NOT LET JET FUEL AND LUBRICATING OILS TOUCHYOU. THESE FLUIDS CAUSE INJURY TO THE SKIN.(1) Do the fuel-tank pressure refueling in the auto or manual mode as follows:(a) Make sure that the REFUEL switch is in the CLOSED position.(b) Make sure that the LH TANK and RH TANK indicator lights come on.(c) Move up and hold the LAMP TEST switch to do the lamp test. After the test,release the LAMP TEST switch.NOTE: The LAMP TEST switch starts the operational test of thelamps and displays. The LH TANK and RH TANK indicatorlights keep lighted on, the FAIL indicator light lights on, andthe display shows all the segments that form the characterslighted on.(d) On the repeater indicator display, select the fuel tank through the TANKSELECTION switch.NOTE: The TANK SELECTION switch selects the total and theindividual tank quantity displays.(e) For fuel-tank pressure refueling in the auto mode only, on the repeater indicatordisplay, use the INC/DEC switch to set the necessary fuel quantity.NOTE: The INC/DEC switch increases or decreases the preselectedfuel quantity on the display.WARNING: MAKE SURE THAT THE REFUELING ADAPTER IS INGOOD CONDITION. A BAD CONNECTION OF THEFUEL NOZZLE CAN CAUSE FUEL SPILLAGE, FIRE,INJURY TO PERSONS AND DAMAGE TO THEEQUIPMENT.(f) Do a visual check of the pressure refueling adapter to make sure there are nodamages, cracks and/or contamination.(g) Connect the fuel nozzle to the pressure refueling adapter.(h) Open the valve handle on the fuel nozzle.WARNING: DURING THE PRESSURE REFUELING PROCEDURE,MAKE SURE THAT THE REFUELING PRESSURE ISBETWEEN 10 AND 50 PSI. PRESSURES ABOVE THEEFFECTIVITY: ALL12-11-00-650-803-A/300Page 302NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKSPECIFIED LIMITS CAN CAUSE DAMAGE TOEQUIPMENT AND INJURIES TO PERSONS.PRESSURES BELOW THE SPECIFIED LIMITS CANCAUSE UNSATISFACTORY OPERATION OF THEREFUELING COMPONENTS.(i) Pressurize the fuel system from 68.95 - 344.74 kPa (10 - 50 psig).(j) Make sure that the LH TANK and RH TANK indicator lights are on and thereis no fuel flow.(k) Make sure that the FAIL indicator light is off.NOTE: If the FAIL indicator light is on, stop the refueling procedureimmediately.(l) Set the REFUEL switch to the OPEN position and make sure that the LHTANK and RH TANK indicator lights go off.(m) Set and hold the SHUT-OFF TEST switch up and observe the LH TANK, RHTANK, and the FAIL indicator lights.NOTE:• The LH TANK and RH TANK indicator lights must comeon and the FAIL indicator light must be off.• If the FAIL indicator light comes on during the pressurerefueling, stop the refueling procedure immediately.(n) Release the SHUT-OFF TEST switch to continue the pressure refueling.(o) For fuel-tank pressure refueling in the auto mode only, when the preselectedfuel quantity is reached, make sure that the LH TANK and RH TANK indicatorlights come on and the fuel flow stops. Then, set the REFUEL switch to theCLOSED position.NOTE:• Maximum refueling time from empty to full is less than12 min, at 334.74 kPa (50 psig).• If fuel overflow occurs, stop the refueling procedureimmediately.(p) For fuel-tank pressure refueling in the manual mode only, when you have thenecessary fuel quantity, set the REFUEL switch to the CLOSED position andmake sure that the LH TANK and RH TANK indicator lights come on and thefuel flow stops.NOTE:• Maximum refueling time from empty to full is less than12 min, at 334.74 kPa (50 psig).• If fuel overflow occurs, stop the refueling procedureimmediately.(q) Close the valve handle on the fuel nozzle.(r) Disconnect the fuel nozzle from the pressure refueling adapter.HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL12-11-00-650-803-A/300Page 303NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.D. Job Close-Up(1) Close access door 191CR.(2) Install the pressure-refueling adapter cap.(3) Disconnect the external DC power supply from the aircraft (GHSH TASK24-41-00-860-802-A/200).NOTE: If you set the POWER SELECTION switch to the BATTERYposition on the pressure refueling control panel, set thePOWER SELECTION switch back to the NORM position anddown the guard.(4) Remove the grounding cable(s) from the aircraft (GHSH TASK 20-40-02-910-801-A).EFFECTIVITY: ALL12-11-00-650-803-A/300Page 304NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKZONE191A191 CRPRESSUREREFUELINGADAPTERBPOWERSELECTIONSWITCHREPEATERINDICATORDISPLAYPRESSURE REFUELINGCONTROL PANEL(REF.)NORMPOWER SELECTIONQUANTITYPRESELECTINCLH TANKINDICATORLIGHTBATTPRESSUREREFUELINGADAPTER CAPLEVERABORT REFUELING PROCEDUREIF THE FAIL LAMP IS ONLH TANK FAIL RH TANKCLOSEDCLOSEDLAMPTESTREFUELSHUT−OFFTESTCLOSEDOPENARH TANKINDICATORLIGHTFAILINDICATORLIGHTREFUELSWITCHHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.TANKSELECTIONSWITCHTANKSELECTIONINC/DECSWITCHDECBLAMP TESTSWITCHSHUTOFFTEST SWITCHEM500ENGHSH120021A.DGNFuel Tank - Pressure RefuelingFigure 301EFFECTIVITY: ALL12-11-00-650-803-A/300Page 305/306NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKGHSH TASK 12-11-00-680-801-A1. Fuel Tank - DrainingA. General(1) This task gives the procedure to drain the fuel from the fuel tanks.(2) Examine the fuel drained from each tank for water and other contaminants.You will usually see water as a layer below the fuel or as small bubblesin the fuel.(3) Let the aircraft be stable for approximately 2h (hours) before you drain it.B. Job Set-Up(1) Do the procedure to make the aircraft safe for maintenance (GHSH TASK20-00-00-910-801-A/200).(2) Do the procedure to make the aircraft safe for maintenance of the fuel system(GHSH TASK 28-00-00-910-801-A/200).(3) Statically ground the aircraft (GHSH TASK 20-40-02-910-801-A/200).NOTE: Make all grounding connections between the fuel source, aircraft,and fuel nozzle (refer to the requirements of the localregulatory authorities).WARNING: USE AN EXPLOSION-PROOF HEAT GUN IN AREASWHERE THERE IS RISK OF EXPLOSION. ADJUST THETEMPERATURE OF THE HEAT GUN TO A VALUE LESSTHAN THE FUEL SELF-IGNITION TEMPERATURE IN THEAIRCRAFT FUEL TANK. IF YOU DO NOT OBEY THISPRECAUTION, AN EXPLOSION CAN OCCUR ANDCAUSE INJURY TO PERSONS AND DAMAGE TOEQUIPMENT.CAUTION: THE HOT AIR TEMPERATURE FROM THE HEATING GUNMUST NOT BE MORE THAN 50 °C. TEMPERATURESABOVE 50 °C CAN CAUSE DAMAGE TO THE AIRCRAFTSYSTEMS.(4) For cold weather conditions, do a check of the fuel temperature as follows:NOTE: When the tank temperature is less than 0 °C (32 °F), you mustnot directly operate the drain valve. At a temperature less than0 °C (32 °F), water can freeze around the drain valve and makethe water flow impossible. If applicable, before you operate thedrain valve to drain the wing tank, use a heat gun to apply heatto the drain valve area.• Energize the aircraft with an external DC (Direct Current) power supply(GHSH TASK 24-41-00-860-801-A/200).• Do a check of the fuel temperature on the synoptic page.HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL12-11-00-680-801-A/300Page 301NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.• De-energize the aircraft (GHSH TASK 24-41-00-860-802-A/200).(5) Open the access door 194BL.C. Fuel Tank - Water DrainingWARNING: DO NOT LET JET FUEL AND LUBRICATING OILS TOUCHYOU. THESE FLUIDS CAUSE INJURY TO THE SKIN.(1) Do the steps that follow to drain the water from the fuel tanks:(a) Use the fuel sampler (GSE 022) to push the drain valve poppet up toopen the drain valve.NOTE: The drain valve closes when you remove the GSE 022from the drain valve poppet. Drain several times until thefuel in the container shows no water. Examine the collectedfuel for contamination, especially at the fuel/waterinterface.(b) Remove the GSE 022 after you drain a sufficient amount of fuel.NOTE: Make sure that the drain valve poppet is in the closed positionand that there is no fuel leak.(2) Visually examine the collected fuel for contamination. If you see microorganismsor other unwanted matter in the fuel, use a Fuel MicroorganismsTest Kit (Microb Monitor 2) to check the presence of microorganisms.Obey the instructions of the test kit manufacturer.NOTE: Refer to the full instructions (aviation fuel item) to do the procedures.(4) If the Fuel Microorganisms Test Kit (Microb Monitor 2) detects the presenceof microorganisms, please use the contact information given in the GHSHIntroduction for the applicable maintenance action.WARNING: WHEN YOU DISCARD DANGEROUS CONSUMABLEMATERIALS, USE PROCEDURES THAT AGREE WITHLOCAL REGULATIONS. THESE MATERIALS CANCAUSE INJURY TO PERSONS AND CONTAMINATION OFTHE ENVIRONMENT.(5) Discard the collected fuel.(6) Do this procedure again for the other drain valve.D. Job Close-Up(1) Close the access door 194BL.(2) Remove the grounding cable(s) from the aircraft (GHSH TASK 20-40-02-910-801-A/200).EFFECTIVITY: ALL12-11-00-680-801-A/300Page 302NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKAB87.8 TO 87.8ATR2.5N1% 2.5EICASIGN ITT C ____ ____ IGNOFFOFF55.1 N2% 55.1OIL PRES PSIOIL TEMP CFUELFF PPHFQ LBLEFT TANKANALOGUEFUEL QUANTITYBARLEFTTANK FUELQUANTITYMFD(FUEL SYNOPTIC PAGE)330 KGTOTAL660KGUSED279 KGLEFT FUELQUANTITYTOTAL FUELQUANTITY330 KGTEMP XX CELECBATT1BATT2SPDBRKOAT-237ATRONLGDN0V0VTAKEOFF DATA SETCALTRATELFEOXYATOTAL FUELQUANTITYFUEL USEDDELTA-PCABINFLAPSRIGHT TANK ANALOGUEFUEL QUANTITY BARRIGHT TANK FUELQUANTITYRIGHT FUELQUANTITYHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.BEM500ENGHSH120006B.DGNFuel Tank - DrainingFigure 301EFFECTIVITY: ALL12-11-00-680-801-A/300Page 303/304NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKGHSH TASK 12-12-00-210-801-A1. Engine Oil Level - Visual CheckA. General(1) This task gives the procedure to do the check of the engine oil level.(2) The engine has two oil sight glasses (inboard and outboard). One isinstalled on the external side of the AGB and the other is installed on theexternal side of the oil tank.B. Job Set-UpWARNING: MAKE SURE THAT THE AIRCRAFT IS IN A SAFECONDITION BEFORE YOU DO THE MAINTENANCEPROCEDURES. THIS IS TO PREVENT INJURY TOPERSONS AND/OR DAMAGE TO THE EQUIPMENT.WARNING: MAKE SURE THAT THERE WILL BE NO ACCIDENTALOPERATION OF THE ENGINES. AN ACCIDENTALOPERATION OF THE ENGINES CAN CAUSE INJURY TOPERSONS.(1) Wait for a minimum of ten minutes to elapse after engine shutdown before.NOTE: If the engine oil system is empty following a draining operationor if the engine has been newly installed after an overhaul, fillthe engine oil tank before checking the engine oil level (GHSHTASK 12-12-00-612-801-A/300).(2) Put the workstand in the work area.(3) Open the oil service door (Figure 301).C. Engine - Oil Level CheckWARNING: OBEY ALL POWERPLANT SAFETY PRECAUTIONS. IFYOU ARE NOT CAREFUL DURING THE POWERPLANTMAINTENANCE, INJURY TO PERSONS AND/ORDAMAGE TO EQUIPMENT CAN OCCUR.WARNING: DO NOT LET JET FUEL AND LUBRICATING OILS TOUCHYOU. THESE FLUIDS CAUSE INJURY TO THE SKIN.(1) Do a check of the engine oil level through the oil level sight glass visible inthe engine oil service door. The oil level sight glass checked must be theone located on the external side.(2) If the engine oil level is not visible in the visual oil level sight glass, checkthe engine for external oil leaks and do repairs as necessary. If no evidenceof an external oil leak is found, please use the contact informationgiven in the GHSH Introduction for the applicable maintenance action.(3) If the engine oil level is between the "MIN" and "MAX" marks, no furtherHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL12-12-00-210-801-A/300Page 301NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKaction is required.(4) If oil tank contents are visible but below the "MIN" mark in the visual oillevel indicator and there is no indication of excessive oil consumption, addengine lubricating oil to the oil tank to between the MIN and MAX marks onthe visual oil level sight glass (Figure 301).D. Job Close-Up(1) Close the oil service door (Figure 301).(2) Remove the workstand from the work area.HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL12-12-00-210-801-A/300Page 302NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKCACCESSORYGEARBOX(REF.)ABBACCESSORYGEARBOX(REF.)C1. OIL FILLERCAPAMAXMIN2. OIL LEVELSIGHT GLASSHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.CTYPICALEM500ENGHSH120020A.DGNOil Level Check - Components LocationFigure 301EFFECTIVITY: ALL12-12-00-210-801-A/300Page 303/304NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKGHSH TASK 12-12-00-612-801-A1. Engine Oil - FillingA. General(1) This task gives the procedures to fill the engine oil system.(2) There are two oil-filler necks in the engine, one installed on the externalside of the main oil tank and one on the external side of auxiliary oil tank.The engine oil-filler neck is part of the oil filler-cap assembly.B. Job Set-UpWARNING: MAKE SURE THAT THE AIRCRAFT IS IN A SAFECONDITION BEFORE YOU DO THE MAINTENANCEPROCEDURES. THIS IS TO PREVENT INJURY TOPERSONS AND/OR DAMAGE TO THE EQUIPMENT.WARNING: MAKE SURE THAT THERE WILL BE NO ACCIDENTALOPERATION OF THE ENGINES. AN ACCIDENTALOPERATION OF THE ENGINES CAN CAUSE INJURY TOPERSONS.(1) Do the procedures to make the aircraft safe for maintenance (GHSH TASK20-00-00-910-801-A/200).(2) Make sure that the engines are not operating during the oil filling procedure.(3) Put the workstand in the work area.(4) Open the oil servicing door (Figure 301).(5) Open the oil filler cap.C. Engine - Oil FillingWARNING: OBEY ALL POWERPLANT SAFETY PRECAUTIONS. IFYOU ARE NOT CAREFUL DURING THE POWERPLANTMAINTENANCE, INJURY TO PERSONS AND/ORDAMAGE TO EQUIPMENT CAN OCCUR.WARNING: DO NOT LET JET FUEL AND LUBRICATING OILS TOUCHYOU. THESE FLUIDS CAUSE INJURY TO THE SKIN.(1) Fill the engine oil system as follows:a) Make sure that the oil-tank drain plug is installed and tightened.b) Add oil until the oil level is at the MAX mark on the oil level sight glass(Figure 301). PW&C does not recommend the casual mixing of differentapproved brands of the same oil type or mixing of different types of oil.Refer to last revision of AFM (Airplane Flight Manual) to check the list ofapproved engine oils.NOTE: The engine oil capacity is 8.14 l.HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL12-12-00-612-801-A/300Page 301NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.c) If deliberate mixing of approved oil brands is necessary, or if inadvertentmixing of approved oil brands occurred, please use the contact informationgiven in the GHSH Introduction for the applicable maintenanceaction.d) If oils of brands not approved and/or other chemical substances wereinadvertently put in the engine oil tank, please use the contact informationgiven in the GHSH Introduction for the applicable maintenanceaction.e) Close and lock the engine-oil filler cap (Figure 301).D. Job Close-Up(1) Close the oil servicing door (Figure 301).(2) Remove the workstand from the work area.EFFECTIVITY: ALL12-12-00-612-801-A/300Page 302NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKCACCESSORYGEARBOX(REF.)ABBACCESSORYGEARBOX(REF.)C1. OIL FILLERCAPAMAXMIN2. OIL LEVELSIGHT GLASSHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.CTYPICALEM500ENGHSH120020A.DGNOil Level Check - Components LocationFigure 301EFFECTIVITY: ALL12-12-00-612-801-A/300Page 303/304NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKGHSH TASK 12-14-00-610-801-A1. Servicing of NLG and MLG TiresA. General(1) This task gives the procedure to do the check and servicing of the NLGand MLG tires.(2) Tire pressure must be checked within limits once each flight day.B. Job Set-UpWARNING: DO NOT GO NEAR HOT TIRES INSTALLED ON THEAIRCRAFT. IF IT IS NECESSARY TO MEASURE THE TIRETEMPERATURE, GO NEAR THE TIRE FROM ITS FRONT,NOT FROM ITS SIDE. HIGH TEMPERATURE CAN CAUSETIRE EXPLOSION.(1) Make sure that the temperature of the tire is the same as the ambient temperature.NOTE: If the aircraft had a flat tire while parked or moving on theground, you must replace this tire because it is permanentlydamaged.(2) Remove the cap from the valve.C. Check of Landing-Gear Tire Pressure(1) Connect the tire pressure gauge to the valve.NOTE:• Only use a pressure gauge which is calibrated and uses thecorrect unit of measurement.• Tire pressure must be checked within limits daily or beforethe first flight of the day.CAUTION: DO NOT BLEED AIR FROM A HOT TIRE TO MAKE THEPRESSURE COME TO THE CORRECT LIMITS BECAUSE,AT AMBIENT TEMPERATURE, ITS PRESSURE WILL BELESS THAN THE CORRECT OPERATIONAL PRESSURE.(2) The pressure must be within the values that follow with the aircraft on theground (loaded):NOTE: For unloaded inflation pressure, decrease these values by 4%to get the equivalent loaded inflation pressure.(a)For the (a) NLG, the pressure must range from 979 to 1048 kPa (142 to152 psi).(b)For the MLG, the pressure must range from 1200 to 1269 kPa (174 to184 psi).(3) If the destination airport temperature is lower than the departure airportHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL12-14-00-610-801-A/300Page 301Rev.03- FEB 24/11Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKtemperature with a difference greater than 27 °C (50 °F), increase the tirepressure by 1% for each 3 °C (5 °F) of difference.NOTE: The pressure is limited to 1420 kPa (206 psi) for the NLG tireand to 1572 kPa (228 psi) for the MLG tire in loaded condition(aircraft on the ground). Do not increase the tire pressure tomore than these values.HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.(4) If the pressure in a tire is at (or near) the bottom limit of the range, it isrecommended that the tire be inflated to the upper limit to preventunnecessary removals at subsequent pressure checks.(5) For tire with less than the minimum service pressure, refer to this table:Table 301 - Cold Pressure Setting Cold Tire Pressure Maintenance ProcedureEFFECTIVITY: ALLCold Tire Pressure95% to less than 100% of the minimumloaded service pressure.90% to less than 95% of the minimumloaded service pressure.Less than 90% of the minimum loaded servicepressure.[1] THE TIRE REMOVED BECAUSE OF LOW INFLATION PRESSURE MUST BE EXAMINED BY AN AUTHO-RIZED RETREADER TO MAKE SURE THAT THE CASING DID NOT HAVE INTERNAL DEGRADATION. IF IT DID,DISCARD THE TIRE.NOTE: If the tire pressure was fully lost during rolling, scrap the tire.(6) After the check, remove the tire pressure gauge from the valve.D. Service of Landing Gear TireMaintenance ProcedureInflate to the specified service pressureagain.Do a check of the tire/wheel assemblyfor the cause of the pressure loss.Inflate again and record this in the logbook.Remove the tire/wheel assembly ifthe pressure loss is more than 5%and occurs again in 24 hours. [1]Remove the tire/wheel assemblyfrom the aircraft . [1]WARNING: YOU MUST GO TO THE TIRE FROM THE FRONT ORBEHIND IN RELATION TO FLIGHT DIRECTION. NEVERSTAY ON THE SIDE OF THE TIRE (IN FRONT OF THEWHEEL) DURING THIS PROCEDURE.WARNING: ONLY USE TIRE INFLATION EQUIPMENT WHICH HASTHE APPROVAL OF THE AIRCRAFT MANUFACTURER.IF YOU INFLATE AN AIRCRAFT TIRE DIRECTLY FROM AHIGH-PRESSURE STORAGE CYLINDER, ANEXPLOSION CAN OCCUR.(1) Set up the tire servicing gauge with the low pressure servicing regulatorand nitrogen cylinder.12-14-00-610-801-A/300Page 302Rev.03- FEB 24/11Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOK(2) Connect the hose to the valve.(3) Inflate the tire and monitor the pressure with the pressure gauge.(4) Remove the hose from the valve.E. Job Close-Up(1) Make sure that there is no leakage from the valve.(2) Install the cap to the valve.CAUTION: TO PREVENT DAMAGE, EXAMINE ALL THE WORK AREASTO MAKE SURE THAT YOU REMOVED ALL TOOLS ANDEQUIPMENT AFTER YOU COMPLETED THE WORK.(3) Remove from the work area all tools, equipment, and materials that youused.HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL12-14-00-610-801-A/300Page 303NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKAZONE711AHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.TIRE (REF.)ZONES721731VALVEATYPICALCAPTIREPRESSUREGAUGE2kg/Cmlbs/Pol 2HOSETIRE SERVICINGGAUGELOWPRESSURESERVICINGREGULATORNITROGENCYLINDEREM500ENGHSH320028A.DGNTire Pressure - Check and ChargeFigure 301EFFECTIVITY: ALL12-14-00-610-801-A/300Page 304NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKGHSH TASK 12-15-01-613-801-A1. Water Tank - ServicingA. General(1) This task gives the procedure to do the servicing of the water tank.(2) The water tank contains clean but non drinkable water (for hygiene purposesonly).(3) Where there are freezing or icing conditions (below 0°C), you must drainthe water tank every day, after the last flight, for protection of the watersystem.For the same weather conditions, if the aircraft needs to be on ground formore than 1h, you must drain the water tank.B. Job Set-Up(1) Do the procedure to make the aircraft safe for maintenance (GHSH TASK20-00-00-910-801-A).(2) Pull the faucet rod to open the manual sink drain valve and drain the lineresidual water.(3) Open access panel 241EZ.(4) Open this circuit breaker and put a circuit breaker ring and tag on it:• WATER PUMP-INTERIOR/IFE CBP (AUX SHED DC BUS 1)C. Water Tank - Servicing(1) To remove the water tank, do as follows:(a)Loosen the strap to release the belt.(b)Disconnect the hydraulic connector and put a protective cap/plug on it.CAUTION: USE ONLY PROTECTIVE CAPS FOR THE PROTEC-TION OF CONNECTOR PINS OR SOCKETS IN ELEC-TRICAL CONNECTORS. OTHER MATERIALS CANCAUSE DAMAGE TO THE CONNECTOR PINS ORSOCKETS, OR LET UNWANTED MATERIALS STAY INTHE CONNECTOR.(c) Disconnect the electrical connector and put a protective cap on it.(d)Carefully pull the water tank by the handle, and remove it.EFFECTIVITY: ALLNOTE: Make sure that the cap of the water tank is fully closed toprevent leakage.(1) To drain the water tank, do as follows:(a)Remove the water tank from the aircraft.(b)Open the filling port.(c) Empty the water tank.(2) To fill the water tank, do as follows:(a) Fill the water tank with potable water up to a level.(b) Close the filling port.Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.12-15-01-613-801-A/300Page 301NOV 20/09HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.

GROUND HANDLING ANDSERVICING HANDBOOKHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.(c) Install the water tank on the aircraft, as follows:1. Put the water tank in its installation position.2. Put the belt in its installation position.3. Remove the protective cap/plug from the hydraulic connector andconnect it.4. Remove the protective cap from the electrical connector and connectit.5. Pass the belt through the strap.6. Lock the belt.D. Job Close-Up(1) Close access panel 241EZ.(2) Remove the circuit breaker ring and tag from this circuit breaker, and close it:• WATER PUMP-INTERIOR/IFE CBP (AUX SHED DC BUS 1)CAUTION: TO PREVENT DAMAGE, EXAMINE ALL THE WORK AREASTO MAKE SURE THAT YOU REMOVED ALL TOOLS ANDEQUIPMENT AFTER YOU COMPLETED THE WORK.(3) Remove from the work area all tools, equipment, and materials that you used.EFFECTIVITY: ALL12-15-01-613-801-A/300Page 302NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKZONE211ABCAP (REF.)HANDLEELECTRICALCONNECTORHYDRAULICCONNECTORBELT (2x)AWATERPUMP (REF.)WATER TANKLAVATORY SINKCABINET (REF.)HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.STRAP (2x)BEM500ENGHSH120024A.DGNEFFECTIVITY: ALLWater Tank- ServicingFigure 30112-15-01-613-801-A/300Page 303NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKZONE211AFAUCET RODFAUCET (REF.)HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.FILLINGPORTFLUID LEVELBA241EZLAVATORY SINKCABINET (REF.)WATERTANKBEM500ENGHSH120023A.DGNWater Tank - ServicingFigure 302EFFECTIVITY: ALL12-15-01-613-801-A/300Page 304NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKGHSH TASK 12-15-03-600-801-A1. Waste Tank - ServicingA. General(1) This task gives the procedure to do the servicing of the waste tank.(2) Where there are freezing or icing conditions (below 0 °C), you must drainthe waste system every day, after the last flight, for protection of the wastesystem.For the same weather conditions, if the aircraft needs to be on ground formore than one hour, you must drain the waste system.(3) Besides the normal servicing and pre-charging procedure, there is a specificprocedure to do the pre-charging of the waste system in cold weather(below 0 °C or 32 °F).B. Job Set-Up(1) Do the procedure to make the aircraft safe for maintenance (GHSH TASK20-00-00-910-801-A).C. Waste Tank - ServicingWARNING: DO NOT LET THE TOILET SYSTEM CLEANER GET INYOUR EYES, IN YOUR MOUTH OR IN YOUR SKIN. IFYOU DO, FLUSH YOUR EYES, MOUTH OR SKIN WITHWATER AND GET MEDICAL AID. THE TOILET SYSTEMCLEANER IS AN ACID AND CAN BURN YOU.WARNING: DO NOT GET WASTE FLUID ON YOUR SKIN, IN YOUREYES OR MOUTH. PUT ON APPROVED PROTECTIVECLOTHING, GOGGLES AND RUBBER GLOVES. IFWASTE FLUID TOUCHES YOU, HEALTH PROBLEMSCAN OCCUR.CAUTION: THE MAXIMUM PERMITTED PRESSURE FOR THE WASTETANK FILLING IS 45 PSI.(1) Do the cleaning of the waste system as follows:(a)Open access door 194FR.(b)Remove the cap from the RTS rinse valve.(c) Release the handle and open the cap of the RTS service panel drainvalve.(d)Connect the lavatory dumping coupling of the lavatory servicing cart tothe RTS service panel drain valve.(e)Connect the lavatory filling coupling to the RTS rinse valve.(f) Push the lever of the RTS service panel drain valve to open its internalflapper valve. Do not operate the coupling handle; its operation is notnecessary.(g) Pull the T-handle out and lock it to open the RTS waste drain valve as follows:EFFECTIVITY: ALLCopyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.12-15-03-600-801-A/300Page 301NOV 20/09HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.

GROUND HANDLING ANDSERVICING HANDBOOKHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.1. Fully pull the T-handle out (approximately 7.5 cm (3 in.)) and turn it(approximately 5 to 20 degrees) clockwise or counterclockwise tolock it.NOTE: Do not turn the T-handle many times in the same direction.The T-handle can be twisted and break.(h)Continue the waste tank drainage until the waste flow stops.(i) Flush with water through the RTS rinse valve for approximately 3 min.(j) Release the T-handle as follows:1. Turn the T-handle in (approximately 5 to 20 degrees) to unlock it (inthe opposite direction to that used to lock it).2. Push the T-handle in.(k) Pull the T-handle out and lock it to open the RTS waste drain valve.(l) Release the T-handle after all liquid is drained.(m) Disconnect the lavatory dumping coupling and lavatory filling coupling.(n)Close the cap of the RTS service panel drain valve and latch the lever.NOTE: The flapper valve closes automatically when the cap isclosed.(o) Install the cap on the RTS rinse valve.(p) Close access door 194FR.NOTE: The access door closes only if the RTS waste drain valve iscorrectly closed.CAUTION: DO NOT DO THE PRE-CHARGING PROCEDURE ON AIR-CRAFT PARKED IN COLD WEATHER. THIS COULD CAUSEDAMAGE TO THE SYSTEM.CAUTION: THE MAXIMUM PERMITTED PRESSURE FOR THE WASTETANK FILLING IS 45 PSI.(2) Do the pre-charging of the waste system as follows:NOTE: This pre-charging procedure is applicable to the temperaturecondition higher than 0 °C (32 °F). Where there are freezing oricing conditions, below 0 °C (32 °F) do the specific procedure.(a)Open access panel 194FR.(b)Remove the cap from the RTS rinse valve.(c) Connect the coupling lavatory filling to the RTS rinse valve.(d)Fill the waste system with the solution prepared in the lavatory servicingdolly:1. 3.8 l of water.2. Add 200 ml of URBAKTOL AF.(e) If you prefer, you can use DEJET to prepare the solution:1. 3.95 l of water.EFFECTIVITY: ALL12-15-03-600-801-A/300Page 302Rev.03- FEB 24/11Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOK2. Add 80 ml of DEJET - CLEANER, BASE, VACUUM TOILET SYS-TEM LINES.(f) Disconnect the coupling lavatory filling from the RTS rinse valve.(g)Install the cap on the RTS rinse valve.(h)Close access panel 194FR.NOTE: The access door will close only if the RTS service paneldrain valve is correctly closed.(3) Do the pre-charging of the waste system, as follows:NOTE: This pre-charging procedure is applicable only to the temperaturecondition below than 0 °C (32 °F), where there are freezingor icing conditions.NOTE: Prepare the solution outside the aircraft and use a liquid containerto transport the solution to the interior of the aircraft.CAUTION: BE CAREFUL WHEN YOU HANDLE THE INTERIORFURNISHINGS. IF YOU DO NOT OBEY THIS PRECAU-TION, DAMAGE TO FRAGILE PARTS CAN OCCUR.(a)Fill the waste tank, through the toilet bowl, with the solution that follows:1. 3.8 l of water.2. Add 200 ml of URBAKTOL AF.(b)If you prefer, you can use DEJET:1. 3.95 l of water.2. Add 80 ml of DEJET - CLEANER, BASE, VACUUM TOILET SYS-TEM LINES.D. Job Close-UpCAUTION: TO PREVENT DAMAGE, EXAMINE ALL THE WORK AREASTO MAKE SURE THAT YOU REMOVED ALL TOOLS ANDEQUIPMENT AFTER YOU COMPLETED THE WORK.(1) Remove from the work area all tools, equipment, and materials that youused.HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL12-15-03-600-801-A/300Page 303Rev.03- FEB 24/11Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKRTS RINSEVALVEAZONE190CAPT− HANDLEHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.CLOSED ANDUNLOCKEDPOSITIONPULLCB5° 5°20° 20°OPEN ANDLOCKEDPOSITIONTURNLAVATORYFILLINGCOUPLINGARTS SERVICEPANEL DRAINVALVECAPHANDLELEVERBLAVATORYDUMPINGCOUPLINGT− HANDLECLAVATORYSERVICINGCARTEM500ENGHSH120022A.DGNWaste Tank - ServicingFigure 301EFFECTIVITY: ALL12-15-03-600-801-A/300Page 304NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKZONE242AAFT CABINPARTITIONTOILET BACKPAD (REF.)ABHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.BEM500ENGHSH120025A.DGNWaste Tank - ServicingFigure 302EFFECTIVITY: ALL12-15-03-600-801-A/300Page 305/306NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKGHSH TASK 12-23-00-100-801-A1. External Aircraft - CleaningA. General(1) This task gives the instructions to clean the aircraft.(2) Clean the external aircraft surfaces frequently to keep them with theirgood visual properties and resistance to corrosion.(3) Always clean the aircraft external surfaces from the top to the bottom.(4) The aircraft external dirt can be light (dust, mud, etc.) or heavy (grease,exhaust deposits, oil, etc.).B. Job Set-UpWARNING: MAKE SURE THAT THE AIRCRAFT IS IN A SAFECONDITION BEFORE YOU DO THE MAINTENANCEPROCEDURES. THIS IS TO PREVENT INJURY TOPERSONS AND/OR DAMAGE TO THE EQUIPMENT.WARNING: DURING THE CLEANING PROCEDURE, DO NOT LETTHE CLEANING SOLUTION TOUCH YOU AND DO NOTBREATHE ITS VAPORS OR MISTS. DO THEPROCEDURE IN AN AREA WITH A GOOD AIRFLOW.PUT ON SAFETY CLOTHES, GOGGLES, AND GLOVES.WARNING: BEFORE YOU CLEAN AN EXHAUST SURFACE, MAKESURE THAT THE EXHAUST SYSTEM IS COLD.CLEANING PRODUCTS ARE FLAMMABLE AND, IF YOUAPPLY THEM TO HOT SURFACES, INJURY TOPERSONS AND DAMAGE TO EQUIPMENT CAN OCCUR.WARNING: IT IS VERY IMPORTANT THAT THE CLEANINGPRODUCT SAFETY PRECAUTIONS ARE OBEYED. USEPROTECTION GOGGLES AND CLOTHES. DO NOT LETCLEANING PRODUCT TOUCH YOUR SKIN, EYES, ORCLOTHES. IF YOU DO NOT OBEY THIS PRECAUTION,DAMAGE TO THE EQUIPMENT AND/OR INJURY TOPERSONNEL CAN OCCUR.WARNING: • DO THIS PROCEDURE IN AN AREA WITH A GOODFLOW OF AIR.EFFECTIVITY: ALL• PUT ON MASK, SAFETY GOGGLES, AND RUBBER ORLATEX GLOVES WHEN YOU TOUCH BIRD REMAINS.• DISCARD THE RUBBER OR LATEX GLOVES THAT YOUUSED.• WHEN YOU HANDLE BIRD STRIKE REMAINS, OBEYTHE LOCAL AUTHORITY RULES TO PREVENTHEALTH PROBLEMS.Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.12-23-00-100-801-A/300Page 301NOV 20/09HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.

GROUND HANDLING ANDSERVICING HANDBOOKHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.(1) Do the procedure to make the aircraft safe for maintenance.WARNING: MAKE SURE THAT THE LANDING GEAR SAFETY PINSARE INSTALLED. THIS IS TO PREVENT INJURIES TOPERSONS AND DAMAGE TO MATERIAL.(2) Make sure that the landing gear safety pins are installed.(3) Make sure that the aircraft is parked correctly.(4) Seal the inlets and outlets of the refrigeration pack compartments withpolyethylene film or equivalent water and detergent-resistant film, andadhesive tape or equivalent.(5) Seal the AOA vanes and their attachment bases on the fuselage withpolyethylene film or equivalent water and detergent-resistant film, andadhesive tape or equivalent.(6) Close the forward baggage-compartment door and seal it with adhesivetape or equivalent.(7) Close the aft baggage-compartment door and seal it with adhesive tape orequivalent.(8) Close the main door and seal it with adhesive tape or equivalent.(9) Install these items of GSE: GSE 003, GSE 009 and GSE 030.(10) Make sure that the water used for cleaning is free from sand residues andother contaminants.C. Aircraft Cleaning - Removal of Light Dirt from the FuselageCAUTION: DO NOT APPLY CLEANING SOLUTION TO LARGE AREASTHAT YOU CANNOT FULLY CLEAN BEFORE THE SOLU-TION DRIES ON THE SURFACE AND THE SURFACEBECOMES GLOSSY.(1) Prepare a cleaning solution in a dilution ratio of 10% by volume of detergentSUPERSOL-10 for 1 liter of distilled water.(2) Apply the cleaning solution of distilled water and detergent SUPERSOL-10 to the aircraft fuselage with a spray gun or a cleaning brush or equivalentequipment.(3) Let the cleaning solution of distilled water and detergent SUPERSOL-10 soakinto the surface for sufficient time for the dirt to become soft (approximately 5minutes).CAUTION: DO NOT USE HIGH PRESSURE (MAXIMUM 70 PSI) ANDDO NOT POINT THE FLOW OF WATER DIRECTLY TO THEANGLE-OF-ATTACK SENSORS OR OTHER MECHANICAL,ELECTRICAL, OR HYDRAULIC COMPONENTS. LIQUIDSTHAT GET INTO THESE AREAS CAN CAUSE SERIOUSDAMAGE TO THE EQUIPMENT.(4) Use a wiper cloth soaked in the solution to clean the fuselage.EFFECTIVITY: ALL12-23-00-100-801-A/300Page 302NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOK(5) Fully flush with clean water, three or more times. Finally flush the surfacefrom its top down to the bottom. Make sure that the solution is fullyremoved.NOTE: If necessary, apply the solution again and rub with a cleaningbrush to help remove the dirt.(6) Dry with forced air or dry rags.D. Aircraft Cleaning - Removal of Heavy Dirt from the FuselageCAUTION: DO NOT APPLY CLEANING SOLUTION TO LARGE AREASTHAT YOU CANNOT FULLY CLEAN BEFORE THE SOLU-TION DRIES ON THE SURFACE AND THE SURFACEBECOMES GLOSSY.(1) Prepare a cleaning solution with a detergent REMOVEGRAX MLS-12detergent and distilled water.(2) Apply the cleaning solution of distilled water and detergent REMOVEG-RAX MLS-12 to the dirt areas with a wiper cloth, a cleaning brush, orequivalent equipment.(3) Let the cleaning solution of distilled water and detergent REMOVEGRAXMLS-12 soak into the surface for a sufficient time for the dirt to becomesoft (approximately 5 minutes).(4) Use a wiper cloth soaked in the solution to clean the fuselage.(5) Fully flush with clean water, three or more times. Finally flush the surfacefrom its top down to the bottom. Make sure that the solution is fullyremoved.NOTE: If necessary, apply the solution again and rub with a cleaningbrush to help remove the dirt.(6) Dry with compressed air or dry rags.E. Aircraft Cleaning - Landing Gear Washing(1) Apply a solution of water and detergent REMOVEGRAX MLS-12 to theaircraft landing gear with the aid of a spray gun or cleaning brush.(2) Fully flush the landing gear with clean water until all the cleaning solutionis removed.(3) Polish the shock absorber rods with a flannel and make these surfacesmoist with hydraulic fluid.(4) It is recommended the lubrication of the MLG and NLG untill 6 hours (maximum)after you finish the cleaning procedure.NOTE: • <strong>EMB</strong>RAER strongly recommends that lubrication of the MLGand NLG be performed around 6 hours after the washing procedure.• High-pressure washing can remove the protective greasesHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL12-23-00-100-801-A/300Page 303NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.and let water into the inner working surface of the landinggear, which increases the risk of further environmental attack.F. Aircraft Cleaning - Windshield Washing(1) Remove all excess amounts of dirt and other foreign matter from the glasssurface with clean water. Preferred initial application is by spraying orflooding the surface to wash away any abrasive materials. If spraying orflooding is impractical, a clean sponge or soft cloth should be used.NOTE: Remove or cover/protect watches, rings, and other metalobjects on person (belt buckle, rivets on jeans, tools in pockets)that may cause scratches before a windshield maintenance.(2) Wash gently using 50% water and 50% isopropyl alcohol solution containingmild liquid soap in a 2% to 5% concentration.NOTE: The mild liquid soap can be detergents formulated for washingdishes by hand. Dawn, Joy, Palmolive or Ivory are recommended.(3) Rinse thoroughly with clean water and dry with a damp chamois, sponge,or cloth.G. Aircraft Cleaning - Side Window Washing(1) Remove all excess amounts of dirt and other foreign matter from theacrylic surface with clean water. Preferred initial application is by sprayingor flooding the surface to wash away any abrasive materials. If spraying orflooding is impractical, a clean sponge or soft cloth should be used.NOTE: Remove or cover/protect watches, rings, and other metalobjects on person (belt buckle, rivets on jeans, tools in pockets)that may cause scratches before a side-window maintenance.(2) Wash gently using 50% water and 50% isopropyl alcohol solution containinga mild liquid soap in a 2% to 5% concentration.NOTE: The mild liquid soap can be detergents formulated for washingdishes by hand. Dawn, Joy, Palmolive or Ivory are recommended.(3) Rinse thoroughly with clean water and dry with a damp chamois, sponge,or cloth.H. Job Close-up(1) Remove the adhesive tape from the aft baggage-compartment door.(2) Remove the adhesive tape from the forward baggage-compartment door.(3) Remove the adhesive tape from the main door.(4) Open the inlets and outlets of the refrigeration pack compartments sealedbefore.(5) Remove the adhesive tape and polyethylene film form the AOA vanes andfrom their attachment bases in the fuselage.EFFECTIVITY: ALL12-23-00-100-801-A/300Page 304NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOK(6) Remove these items of GSE: GSE 003, GSE 009 and GSE 030.CAUTION: TO PREVENT DAMAGE, EXAMINE ALL THE WORK AREASTO MAKE THAT YOU REMOVED ALL TOOLS AND EQUIP-MENT AFTER YOU COMPLETED THE WORK.(7) Remove from the work area all tools, equipment, and materials that youused.HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL12-23-00-100-801-A/300Page 305/306NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKGHSH TASK 12-23-00-100-802-A1. Internal Aircraft - CleaningA. General(1) This task gives the instructions for maintenance and cleaning of materialsand components of the aircraft interior.B. Job Set-UpWARNING: DURING THE CLEANING PROCEDURE, DO NOT LETTHE CLEANING SOLUTION TOUCH YOU AND DO NOTBREATHE ITS VAPORS OR MISTS. DO THEPROCEDURE IN AN AREA WITH A GOOD AIRFLOW.USE SAFETY CLOTHES, GOGGLES, AND GLOVES.WARNING: MAKE SURE THAT THE AIRCRAFT IS IN A SAFECONDITION BEFORE YOU DO THE MAINTENANCEPROCEDURES. THIS IS TO PREVENT INJURY TOPERSONS AND/OR DAMAGE TO THE EQUIPMENT.(1) Do the procedure to make the aircraft safe for maintenance.(2) Do the aircraft normal parking procedure.WARNING: MAKE SURE THAT THE LANDING GEAR SAFETY PINSARE INSTALLED. THIS IS TO PREVENT INJURIES TOPERSONS AND DAMAGE TO MATERIAL.(3) Make sure that the landing-gear safety pins are installed.C. Carpets - CleaningWARNING: DURING THE CLEANING PROCEDURE, DO NOT LETTHE CLEANING SOLUTION TOUCH YOU AND DO NOTBREATHE ITS VAPORS OR MISTS. DO THEPROCEDURE IN AN AREA WITH A GOOD AIRFLOW.PUT ON SAFETY CLOTHES, GOGGLES, AND GLOVES.CAUTION: FROM THE INSTALLATION OF THE CARPET, VACUUMTHE CARPET ONCE A WEEK MINIMUM TO REMOVE SOILAND OTHER PARTICLES BEFORE THEY ARE <strong>EMB</strong>EDDEDINTO THE PILE OF THE CARPET. IN HEAVY TRAFFIC,VACUUM THE CARPET MORE FREQUENTLY.(1) Do a regular cleaning as follows:(a) Remove all loose particles from the carpet with a vacuum cleaner.NOTE:Move the vacuum cleaner slowly to give time for dirtremoval.(b) Do not let the dust bag be more than half full.HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL12-23-00-100-802-A/300Page 301NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKNOTE: You cannot over-vacuum.HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.(c) Prepare the carpet cleaning-solution. Refer to the manufacture's instructions.(d) Apply it to the surface while you use a soft-bristle brush lightly.(e) Let the cleaned area dry.(f ) Clean the area with a vacuum cleaner to complete the cleaning.(2) Remove the general spots as follows:(a) Blot spills with white paper towels or a clean absorbent cloth.(b) Use a polyethylene spatula and a lint-free cloth to lightly clean thearea.(c) Do a visual check to see if the spot was removed.CAUTION: BEFORE YOU APPLY CLEANING CHEMICAL TO THECARPET, DO A TEST FOR COLORFASTNESS IN ASAMPLE OR IN A PART OF THE CARPET THAT CAN-NOT BE EASILY SEEN.CAUTION: MAKE SURE THAT ALL SOLUTIONS HAVE PHBETWEEN 4 AND 7.CAUTION: DO NOT SQUIRT SOLVENT INTO THE CARPET, ITCAN DISSOLVE THE BACKING MATERIALS.(d) Prepare the carpet cleaning solution. Use the treatments given inTable 301 to soak the area to remove the dirty spots.NOTE: • Use the manufacturer's instructions.• Use the same order of treatment as given in Table 301.(e) To remove these spots, use the order of the treatments given in thetable:SPOTAlcoholic Beverages Cold waterTable 301 – Carpet – Spot TreatmentORDER OF TREATMENTSTEP 1 STEP 2 STEP 3Carpet shampoo.This solution mustbe well rinsed withclear water.Bleach Cold water Ammonia solution White vinegar solutionBloodCold waterCarpet shampoo.This solution mustbe well rinsed withclear water.--EFFECTIVITY: ALL12-23-00-100-802-A/300Page 302NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKTable 301 - Carpet - Spot Treatment (Continued)ButterSPOTChewing GumChocolateCoffeeColas and SoftDrinksCooking OilsCreamORDER OF TREATMENTSTEP 1 STEP 2 STEP 3SolventChill withaerosolfreezingagent or icecubes in aplastic bag.Pick orscrape offgum.Carpetshampoo.This solutionmust be wellrinsed withclear water.Cold waterCold waterSolventCarpetshampoo.This solutionmust be wellrinsed withclean water.Carpet shampoo.This solution mustbe well rinsed withclear water.Solvent. -Ammonia solution.Carpet shampoo.This solution mustbe well rinsed withclean water.Carpet shampoo.This solution mustbe well rinsed withclean water.Carpet shampoo.This solution mustbe well rinsed withclean water.-White vinegar solution.Solvent.Solvent. ---HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL12-23-00-100-802-A/300Page 303NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKTable 301 - Carpet - Spot Treatment (Continued)HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.SPOTEggExcrementFloor WaxFruit JuiceFurniture PolishGravy and SaucesInk (fountain pen)Ink (ball point)ORDER OF TREATMENTSTEP 1 STEP 2 STEP 3Carpetshampoo.This solutionmust be wellrinsed withclean water.Cold waterSolventCold waterSolventWarm waterCold waterSolventCarpet shampoo.This solution mustbe well rinsed withclean water.Carpet shampoo.This solution mustbe well rinsed withclean water.Carpet shampoo.This solution mustbe well rinsed withclean water.Carpet shampoo.This solution mustbe well rinsed withclean water.Carpet shampoo.This solution mustbe well rinsed withclean water.Carpet shampoo.This solution mustbe well rinsed withclean water.Alcohol, methylatedspirits or mineralturpentine.- -Ammonia solution.Ammonia solution and--white vinegar solution.Carpet shampoo. Thissolution must be wellrinsed with cleanwater.--EFFECTIVITY: ALL12-23-00-100-802-A/300Page 304NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKSPOTInk (felt tip)KetchupLipstickMercurochromeORDER OF TREATMENTSTEP 1 STEP 2 STEP 3Warm waterWarm waterSolventCarpetshampoo.This solutionmust be wellrinsed withclean water.Carpet shampoo.This solution mustbe well rinsed withclean water.Carpet shampoo.This solution mustbe well rinsed withclean water.Carpet shampoo.This solution mustbe well rinsed withclean water.Milk Warm water. Solvent.MustardCarpetshampoo.This solutionmust be wellrinsed withclean water.Ammonia solution.Acetone.--White vinegar solution.Carpet shampoo. Thissolution must be wellrinsed with cleanwater.- -Nail Polish Acetone. Solvent. -Oil and GreasePaint (latex)Solvent.Cold water.Carpet shampoo.This solution mustbe well rinsed withclean water.Carpet shampoo.This solution mustbe well rinsed withclean water.Solvent.-HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL12-23-00-100-802-A/300Page 305NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKTable 301 - Carpet - Spot Treatment (Continued)SPOTORDER OF TREATMENTSTEP 1 STEP 2 STEP 3HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.Paint (oil)Alcohol,Carpet shampoo. Thismethylatedsolution must be wellspirits or mineralturpen-Solvent.rinsed with cleanwater.tine.RustSolvent.Carpet shampoo.This solution mustbe well rinsed withRust remover.clean water.Salad DressingCarpetshampoo.This solutionmust be wellSolvent. -rinsed withclean water.Shoe Polish Solvent.Carpet shampoo.This solution mustbe well rinsed with-clean water.Carpet shampoo.SootSolvent.This solution must Ammonia solution andbe well rinsed with white vinegar solution.clean water.Tar Solvent. - -Carpet shampoo.TeaCold water.This solution mustbe well rinsed withSolvent.clean water.Carpet shampoo.Urine (fresh) Cold water.This solution mustbe well rinsed withclean water.-EFFECTIVITY: ALL12-23-00-100-802-A/300Page 306NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKSPOTUrine (old)VomitWineUnknow MaterialEFFECTIVITY: ALLTable 301 - Carpet - Spot Treatment (Continued)(f) Lightly apply it to the surface with a soft-bristle brush.(g) Do the operation again until the surface is fully clean.NOTE: • Do not wet the carpet too much.• Clean from the edge of the spot to prevent too muchspread.(h) When the spot is removed, apply pressure with paper towels or dryabsorbent cloth to blot excessive moisture.(i) Use a clean cloth soaked in warm water again from the edge to thecenter.NOTE: Do not rub the carpet.ORDER OF TREATMENTSTEP 1 STEP 2 STEP 3Carpetshampoo.This solutionmust be wellrinsed withclean water.Carpetshampoo.This solutionmust be wellrinsed withclean water.Absorbentpowder (salt,talc or proprietaryabsorbentpowders).Solvent.Ammonia solution.Cold water.Absorbent cleaner(host or Dri-matic).(j) Apply pressure with paper towels or dry absorbent cloth to blot excessivemoisture.(k) After the removal of the spots, clean the surface.Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.White vinegar solution.- -Carpet shampoo. Thissolution must be wellrinsed with cleanwater.Carpet shampoo. Thissolution must be wellrinsed with cleanwater.12-23-00-100-802-A/300Page 307NOV 20/09HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.

GROUND HANDLING ANDSERVICING HANDBOOKHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.NOTE: Do not walk on moist areas of the carpet.(3) Remove the wool and sink spot as follows:CAUTION: FOR SILK CLEANING, AVOID USING WATER ANDWATER-BASED CLEANERS. USE DRY CLEANINGAGENTS ONLY.(a) Beverage:NOTE: Do not use metal bristles.1. Use a dry cloth towel to blot the spot.2. Apply pressure moderately. If the spot continues, use club soda tomake the area moist.3. Blot until the spot is removed.4. Use the CAPTURE to remove residual discoloration.NOTE: Use the manufacturer's instructions.(b) Food spill:1. Remove as solid matter as possible.2. Blot up as liquid matter as possible.3. For a wool spot, use a shop wipe soaked in club soda to make thearea moist and blot up again.4. Use CAPTURE for water based residual.CAUTION: DO NOT OVER-SPRAY THE CARPET. APPLY ZEP-X-OUT TO THE TOWEL THEN GENTLY WORK INTOCARPET.5. Use Zep-X-out II for grease or oil.NOTE: Use the manufacture's instructions.(c) Spill in the lavatory:1. Blot the area immediately2. Use a shop wipe soaked in club soda, and blot again.NOTE: • Use a tea spoon of white vinegar per 170 g (6 oz) clubsoda.• Do not use vinegar rinse on silk carpet.3. After the area is clean, use club soda and vinegar solution to blotagain.(d) Grease, Oil, Tar or Asphalt:1. Remove as much as possible but do not push it deeper into the pileor you will increase the spot.2. Apply 1:1:1 of trichloroethane volatile dry cleaning solvent to aclean dry towel.3. Rub the towel on the spot with a soft circular motion.EFFECTIVITY: ALL12-23-00-100-802-A/300Page 308NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOK4. Immediately blot with a dry part of the towel.5. Do these procedures again until the spot is removed.D. Seat Cover and Curtain Fabric - CleaningNOTE: When the fire-blocking fabric is dirty, use a commercially drycleaning agent (Solvent per MIL-PRF-680 Type I or equivalent).(1) To clean the seat cover and the curtains without their removal, do as follows:(a) Collect all loose particles with a vacuum cleaner.(b) For spots not easy to remove, you can use a soft-bristle brush.(c) Remove spots from the fabric and be careful not to soak the seatupholstery. See Table 301.(d) If necessary, remove the upholstery to do the cleaning procedure.(2) To clean the seat cover and curtains with their removal, do as follows:(a) Apply a matching-type Velcro tape to all Velcro tapes to prevent damageduring the cleaning.(b) Use a polyethylene spatula and a lint-free cloth to lightly clean thearea.(c) Prepare the carpet cleaning solution.NOTE: Follow the manufacture's instructions.(d) Apply it lightly to the surface with a soft-bristle brush.(e) Repeat the operation until the surface is fully clean.(f) Fully dry the surface with a lint-free cloth.(g) Make the area moist with a cleaning solution. Use the treatmentsgiven in Table 301 to soak the area to remove dirty spots.NOTE: • Use the manufacture's instructions• Use the same order of treatment as given in Table 301.(h) While the surface is wet, use a polyethylene spatula lightly on the dirtyarea.(i) After the removal of the spots, let the cleaned area dry.(j) Clean the area with a vacuum cleaner to complete the cleaning.(k) Turn the seat cover inside out.(l) Dry-clean it with a mixture of solvent MIL-PRF-680 Type I or equivalent,neutral detergent, and cold water. The solution must be in the proportionindicated by the detergent manufacturer and the temperaturemust not be higher than 22°C (72°F).NOTE: The solution must be cold and the water contents must notbe of more than 8% to prevent the cover from becomingshorter.(m) Dry the cover at a temperature not higher than 55°C (130°F).HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL12-23-00-100-802-A/300Page 309NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.(n) Remove the Velcro tape again.(o) Install the cover to the seat.E. Acrylic Parts - Cleaning(1) Lightly rub the surface with a lint-free cloth soaked in neutral detergent tofully clean the surface.(2) Use a lint-free cloth soaked in clean water to fully remove the detergent.(3) Rub the surface dry with a lint-free cloth.(4) If necessary, clean the surface with a lint-free cloth moist with Naphthaand detergent.NOTE: Do not let Naphtha touch the plastic surfaces. Naphtha cancause damage to them.(5) Rub the surface with a lint-free cloth soaked in neutral detergent to makesure that it is fully clean.(6) Fully remove all detergent with a soft cloth soaked in clean water.(7) Rub the surface dry with a lint-free cloth.F. Leathers - Cleaning(1) Do the regular Cleaning as follows:(a) Prepare the neutral detergent solution (refer to the manufacturer'sinstructions) and apply only foam to leather with a lint-free cloth.Lightly wipe with circular movements.(b) Remove all detergent with a lint-free cloth soaked in water.(c) Rub the surface dry with a lint-free cloth.(2) Remove the spots as follows:(a) Clean stains (coffee, milk, liqueur, etc.) with neutral detergent (Refer tothe manufacturer's instructions).(b) Clean stains (grease, oil, etc.) with a lint-free cloth soaked in MIL-PRF-680 Type I or equivalent.(c) Remove all detergent with a lint-free cloth moist with clean water.(d) Rub the surface with a dry lint-free cloth.G. Metal Surfaces - CleaningCAUTION: WHEN YOU SOAK THE CLOTH, DO NOT PUT IT OVERTHE SOLVENT CONTAINER MOUTH AND TURN THE CON-TAINER. THIS CAN CAUSE CONTAMINATION OF THE SOL-VENT SOURCE. ALWAYS POUR THE SOLVENT ONTO THECLOTH OR USE A DISPENSER CAN DESIGNED TO ISO-LATE CONTAMINATS.CAUTION: DO NOT LET SOLVENTS TOUCH THE DECOR MATERIAL ORPLASTIC COMPONENTS. MEK AND ACETONE CAN CAUSEDAMAGE TO SOME COMPONENTS AND MATERIALS.(1) Clean the metal surfaces with solvents as follows:EFFECTIVITY: ALL12-23-00-100-802-A/300Page 310NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKNOTE: • We recommend that you apply a corrosion inhibitor to metalsurfaces independently of the cleaning material that you use.Metal surfaces are normally treated or anodized to preventcorrosion. Normal wear and abnormal abuse cause corrosion,and it is always a factor that you must consider.• Do not scour or abrade surfaces. Corrosion protection is normallya thin layer of anodizing or organic agent. Abrasion canremove the protective film or coating.• Do not permit solvent to evaporate on the surface.• Do not use a cloth a second time because this can redepositcontaminants on the surface.(a) Dampen a clean dry cotton cloth with the solvent. Pour the solvent onthe cloth.(b) Wipe the metal surfaces with the solvent. Repeat the applications asnecessary to remove all dirt.NOTE: For oxidation, powdery white corrosion, use corrosioninhibitor/cleaner.(c) Dry the parts with a clean, dry cotton cloth.CAUTION: DO NOT USE BRULIN 815MX CLEANER UNDILUTED.SOLUTIONS STRONGER THAN SPECIFIED CAN DAMAGETHE DECORATIVE SURFACES.(2) Use BRULIN 815MX:NOTE: Cool water works best with normal dirt and dust. Warm waterworks better with oily surfaces.(a) Prepare a solution of BRULIN 815MX with cool or lukewarm waterbetween 32°C - 49°C (90°F - 120°F). Prepare a solution with 1 partBRULIN 815MX to 64 parts of water by volume, for light dirt. You canincrease the solution up to 1 part of BRULIN 815MX to 10 parts ofwater by volume.(b) Apply the solution with a spray bottle, soft-bristle brush, sponge or cottoncloth.(c) Rub the surface with a wet sponge or cotton cloth. You can also spraythe material on the surfaces and rub with a clean sponge or soft-bristlebrush. Do not permit excess to run off to adjacent surfaces.(d) Rub the dirty areas as necessary and repeat the application of thesolution to remove contamination.(e) Rinse the surface with a fresh sponge or a cloth dampened with cleanwater to remove residue.(f) Dry the surface with a clean, dry cotton cloth.HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL12-23-00-100-802-A/300Page 311NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.(3) Use CALLA 301-A LEMON:NOTE: Cool water works best with normal dirt and dust. Warm waterworks best with oily surfaces.(a) Prepare a solution of CALLA 301-A LEMON with cool or lukewarmwater within 32 °C - 49 °C (90 °F - 120 °F). Prepare a solution with 1part of CALLA 301-A LEMON to 4-8 parts of water by volume for normalcleaning. For concentrated dirt or spots, use full strength.(b) Apply the solution with a spray bottle, soft-bristle brush, or cotton cloth.(c) Spray the solution on the surface. Rub the surface with a clean cloth orsponge. Do not permit excess to run off to adjacent surfaces.NOTE: Make sure that no solution excess comes into contact withporous surfaces.(d) Rub the dirty area as necessary, and repeat the applications as necessaryto remove contamination.(e) Rinse the surface with a fresh sponge or a cloth dampened with cleanwater to remove residue.(f) Dry the surface with a clean, dry cotton cloth.H. Plastic or Vinyl Panels - Cleaning(1) Use of mild household detergent:(a) Prepare a solution of mild household detergent with lukewarm waterbetween 32 °C - 49 °C (90 °F - 120 °F). Prepare the solution with 1part detergent to 50 parts of water by volume.(b) Wet a cotton cloth or sponge with the solution.(c) Apply the solution to the surface. Use circular wipes. Do not permitexcess to run off to adjacent surfaces.(d) Rub the dirty area as necessary, and repeat the application of the solutionto remove contamination.(e) Rinse the surface with a fresh sponge or a cloth dampened with cleanwater to remove residue.(f) Dry the surface with a clean, dry cotton cloth.NOTE: Do not use BRULIN 815MX cleaner. Solutions strongerthan specified can damage the decorative surfaces.(2) Use of BRULIN 815MX:NOTE: Cool water works better with normal dirt and dust. Warm waterworks better with oily surfaces.(a) Prepare a solution of BRULIN 815MX with cool or lukewarm waterbetween 32 °C - 49 °C (90 °F - 120 °F). Prepare a solution with 1 partof BRULIN 815MX to 64 parts of water by volume, for light dirt. Youcan increase the solution up to 1 of BRULIN 815MX to 10 parts ofwater by volume.EFFECTIVITY: ALL12-23-00-100-802-A/300Page 312NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOK(b) Apply the solution with a spray bottle, soft-bristle brush, sponge or cottoncloth.(c) Spray the solution on the surface. Rub the surface with a clean cloth orsponge. Do not permit excess to run off to adjacent surfaces. Makesure that no excess comes into contact with porous surfaces.(d) Rub the dirty area as necessary and repeat the application of the solutionto remove contamination(e) Rinse the surface with a fresh sponge or a cloth dampened with cleanwater to remove residue.(f) Dry the surface with a clean, dry cotton cloth.(3) Use of CALLA 301-A LEMON:NOTE: Cool water works better with normal dirt and dust. Warm waterworks best with oily surfaces.(a) Prepare a solution of CALLA 301-A LEMON with cool or lukewarmwater between 32 °C - 49 °C (90 °F - 120 °F). Prepare a solution with 1part of CALLA 301-A LEMON to 4-8 parts of water by volume for normalcleaning. For concentrated dirt or spots, use full strength.(b) Apply the solution with a spray bottle, soft-bristle brush, or cotton cloth.(c) Spray the solution on the surface. Rub the surface with a clean cloth orsponge. Do not permit excess to run off to adjacent surfaces. Makesure that no excess comes into contact with porous surfaces.(d) Rub the dirty area as necessary and repeat the application of the solutionto remove contamination.(e) Rinse the surface with a fresh sponge or a cloth dampened with cleanwater to remove residue.(f) Dry the surface with a clean, dry cotton cloth.I. Ultrasuede - Cleaning(1) Do the regular maintenance as follows:(a) Vacuum the carpet to remove all loose particles.(b) To prepare the Ultrasuede cleaning-solution refer to the manufacturer'sinstructions.NOTE: You can remove stains with detergent. Use denaturedalcohol or a mild cleaning fluid when required. Refer toTable 302.(c) Apply it to the surface while you use a medium-bristle brush lightly.(d) Let the cleaned area dry.(e) Vacuum it to complete the cleaning.(2) Clean the everyday stains as follows:(a) Lightly use a spatula and a wiper to clean the area.(b) Prepare a solution of water and mild detergent.NOTE: You can remove stains with detergent. Use denaturedHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL12-23-00-100-802-A/300Page 313NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.alcohol or a mild cleaning fluid when required. Refer toTable 302.(c) Lightly apply it to the surface with a medium-bristle brush.(d) Repeat the operation until the surface is fully clean.(e) Remove the Ultrasuede cleaning solution with a cloth and water.(f) Use a heat gum to dry the area or dry naturally by air.(2) Extremely tough stains:(a) Lightly use a spatula and a wipe to clean the area.(b) Clean stains (grease, etc.) with a lint-free cloth soaked in solvent MIL-PRF-680 Type I or equivalent.(c) Lightly apply it to the surface with a medium-bristle brush.(d) Repeat the operation until the surface is fully clean.(e) Prepare the neutral detergent solution (refer to the manufacturer'sinstructions) and apply foam with a lint-free cloth. Lightly wipe with circularmovements.(f) Remove all detergent with a lint-free cloth soaked in clean water.(g) Rub the surface with a dry lint-free cloth.(3) To remove a specific stain from Ultrasuede, use these materials indicatedin the table to do a spot treatment:Table 302 - Ultrasuede - Spot TreatmentSTAINCoffee, Tea, Bear, Wine, Liquor, Milk,Ketchup, Steak Sauce.Mayonnaise, Butter, Salad Oil, Chocolate,Cosmestic Foundation, Lipstick, Face Cream,Suntain Oil/Lotion, ball Point Pen (Ink), ShoePolish, UrineMachine OilDetergent.SPOT TREATMENTSTEP 1Detergent and denatured alcoholDenatured alcoholJ. Painted Surfaces - Cleaning(1) Apply neutral detergent to the dirty area with a soft cloth.(2) Rub the surface with a soft clean soaked in clean water to remove thedetergent.(3) Rub the surface dry with a soft clean cloth.CAUTION: DO NOT USE CHLORINATED AND FLUORCARBON SOL-VENTS IN AREAS PAINTED WITH WATER-BASE PAINTS.(4) If necessary, rub the surface with a cloth dampened with solvent MIL-PRF-680 Type I or equivalent.(5) Apply neutral detergent to the dirty area with a soft cloth.(6) Rub the surface with a soft clean cloth soaked in water to remove theEFFECTIVITY: ALL12-23-00-100-802-A/300Page 314NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKdetergent.(7) Rub the surface dry with a soft clean cloth.K. Decals - CleaningCAUTION: DO NOT USE ORGANIC SOLVENTS (METHYL-KETONE,ALCOHOL, CHLORINATED SOLVENTS, FLUORINATEDSOLVENTS, ETC.). THE MATERIAL IS NOT RESISTANT TOORGANIC SOLVENTS.(1) Rub the decal with a soft clean cloth soaked in neutral detergent (Refer tothe manufacturer's instructions).(2) Remove all detergent with a soft cloth soaked in clean water.(3) Rub the surface dry with a soft clean cloth.L. Wooden Surfaces - CleaningNOTE: These steps are not applicable to the areas that had lightscratches removed. These areas must be re-sanded with Scotchbrite(white) sponge.(1) Carefully wipe the panel with a shop wipe to make sure that there is nodebris on the surface that can scratch the finish.(2) Mix the cleaning solution, which must have 90 parts of warm clean waterand 10 parts of mild liquid soap.NOTE: You can use Windex to clean the surface as an alternative.(3) Lightly soak a shop wipe in soap solution and clean the surface in a circularsoft motion.NOTE: Turn the cloth frequently to prevent the dirt from redeposit.M. Formica Surfaces - Cleaning(1) Lightly rub the surface with a wiper cloth soaked in neutral detergent tofully clean the surface.(2) Use a wiper cloth soaked in clean water to fully remove the neutral detergent.(3) Rub the surface dry with a wiper cloth.(4) If necessary, clean the surface with a wiper cloth moist with water andneutral detergent.(5) Rub the surface with a wiper cloth soaked in neutral detergent to makesure that it is fully clean.(6) Fully remove all neutral detergent with a cloth soaked in clean water.(7) Rub the surface dry with a wiper cloth.N. Decorative Platings - Cleaning(1) This procedure is applicable to decorative platings of a distinct variety ofmaterials. These include gold, nickel, copper, brass, chrome, smokenickel, rose gold, silver and platinum.HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL12-23-00-100-802-A/300Page 315NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.CAUTION: IT IS RECOMMENDED THAT PLATED SURFACE CON-TACTED BY MOISTURE (ESPECIALLY WATER, TOMATOAND ORANGE JUICE, CARBONATED SOFT DRINKS, ANDALCOHOL) BE WIPED IMMEDIATELY AFTER EACHFLIGHT.CAUTION: DO NOT PERMIT WATER TO DRY ON THE PARTS. THEMINERAL CONTENT IN SOME WATER WILL LEAVEDEPOSITS THAT CAN BE DIFFICULT TO REMOVE.CAUTION: WHEN YOU SOAK THE CLOTH, DO NOT PUT IT OVERTHE SOLVENT CONTAINER MOUTH AND TURN THE CON-TAINER. THIS CAN CAUSE CONTAMMINATION OF THESOLVENT SOURCE. ALWAYS POUR THE SOLVENT ONTOTHE CLOTH OR USE A DISPENSER CAN DESIGNED TOISOLATE CONTAMINANTS.CAUTION:DO NOT LET SOLVENTS TOUCH THE DECOR MATERIALOR PLASTIC COMPONENTS. MEK AND ACETONE CANCAUSE DAMAGE TO SOME COMPONENTS AND MATE-RIALS.(2) Use of solvents:NOTE: • We recommend that you apply a corrosion inhibitor to metalsurfaces independently of the cleaning material that you use.Metal surfaces are normally treated or anodized to preventcorrosion. Normal wear, and abnormal abuse cause corrosion,and it is always a factor that you must consider.• Do not scour or abrade surfaces. Corrosion protection is normallya thin layer of anodizing or organic agent. Abrasion canremove the protective film or coating.• Do not permit solvent to evaporate on the surface.• Do not use cloth a second time because this can redepositcontaminants on the surface.• Keep the platings away from the sun. Long exposures discolorthe finish.• You must clean the platings every two weeks.• Avoid spills on the finished surface. If it occurs clean immediately.(a) Dampen a clean dry cotton cloth with Windex. Pour it on the cloth.CAUTION: DO NOT USE HARSH OR AMMONIATED CLEANINGAGENTS ON A FINISH WHICH WAS SEALED BY AEFFECTIVITY: ALL12-23-00-100-802-A/300Page 316NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKEFFECTIVITY: ALLCLEAR COAT.CAUTION: DO NOT USE FORCE DURING CLEANING PROCE-DURES.CAUTION: USE ONLY SOFT NON-SCRATCHING CLOTH.(b) Lightly dust the metal surfaces with the Windex. Repeat the applicationsas necessary to remove all dirt. For oxidation, powdery white corrosion,use corrosion inhibitor/cleaner.(c) Use a new soft paper towel and gently dust the surface to make surethat it is dried.NOTE: If the parts remain slightly wet, stains appears.(d) Use a clean cloth to apply a thin layer of turtle liquid wax to the platings.NOTE: The turtle liquid wax protects the plated surfaces.(e) Gently wipe the turtle liquid wax off in a circular motion until the wax disappears.O. Windshield - CleaningCAUTION: DO NOT LET CLEANING PRODUCTS (SOLVENTS) TOUCHPAINT-FINISHED SURFACES, PLASTICS, OR SEALANTBEADS TO PREVENT DAMAGE.CAUTION: • DO NOT PUT CLEANING CLOTHS, BRUSHES, ORSPONGES IN A SOLVENT CONTAINER. THIS IS TOPREVENT SOLVENT CONTAMINATION.• CONTAMINATED SOLVENT CAN DAMAGE THEEQUIPMENT.CAUTION: DO NOT LET CLEANING PRODUCTS (SOLVENTS) TOUCHSEALANT BEADS, LENSES, POLYCARBONATE WIN-DOWS, WINDSHIELDS, PAINTED SURFACES, ANDACRYLIC PARTS. SOLVENTS CAN CAUSE DAMAGE TOTHESE SURFACES.CAUTION: DO NOT PUT ON WATCHES, BRACELETS, RINGS, ORCLOTHES WITH ZIP FASTENERS WHEN YOU CLEAN WIN-DOWS. DO NOT USE METAL TOOLS TO CLEAN WIN-DOWS.METAL OBJECTS CAN SCRATCH THETRANSPARENCY AND CAUSE OPTICAL DISTORTION.CAUTION: DO NOT USE ABRASIVE MATERIALS TO CLEAN WIN-DOWS. ABRASIVE MATERIALS CAN SCRATCH THETRANSPARECNCY AND CAUSE OPTICAL DISTORTION.(1) Remove all excess amounts of dirt and other foreign matter from the glasssurface with clean water. Preferred initial application is by spraying orCopyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.12-23-00-100-802-A/300Page 317NOV 20/09HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.

GROUND HANDLING ANDSERVICING HANDBOOKHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.flooding the surface to wash away any abrasive materials. If spraying orflooding is impractical, a clean sponge or wipe cloth should be used.NOTE: Remove or cover/protect watches, rings, and other metalobject on person (belt buckle, rivets on jeans, tools in pockets)that may cause scratches before any windshield maintenance.(2) Wash gently with 50% water and 50% alcohol TT-I-735 solution containing amild liquid soap in a 2% to 5% concentration.NOTE: The mild liquid soap can be detergents formulated for washingdishes by hand. Dawn, Joy, Palmolive or Ivory are recommended.(3) Rinse thoroughly with clean water and dry with a damp chamois, sponge,or wipe cloth.P. Side Window - CleaningCAUTION: DO NOT LET CLEANING PRODUCTS (SOLVENTS) TOUCHPAINT-FINISHED SURFACES, PLASTICS, OR SEALANTBEADS TO PREVENT DAMAGE.CAUTION: • DO NOT PUT CLEANING CLOTHS, BRUSHES, ORSPONGES IN A SOLVENT CONTAINER. THIS TOPREVENT SOLVENT CONTAMINATION.• CONTAMINATED SOLVENT CAN DAMAGE THEEQUIPMENT.CAUTION: DO NOT LET CLEANING PRODUCTS (SOLVENTS) TOUCHSEALANT BEADS, LENSES, POLYCARBONATE WIN-DOWS, WINDSHIELDS, PAINTED SURFACES, ANDACRYLIC PARTS. SOLVENTS CAN CAUSE DAMAGE TOTHESE SURFACES.CAUTION: DO NOT PUT ON WATCHES, BRACELETS, RINGS, ORCLOTHES WITH ZIP FASTENERS WHEN YOU CLEAN WIN-DOWS. DO NOT USE METAL TOOLS TO CLEAN WIN-DOWS. METAL OBJECTS CAN SCRATCH THETRANSPARENCY AND CAUSE OPTICAL DISTORTION.CAUTION: DO NOT USE ABRASIVE MATERIALS TO CLEAN WIN-DOWS. ABRASIVE MATERIALS CAN SCRATCH THETRANSPARENCY AND CAUSE OPTICAL DISTORTION.(1) Remove all excess amounts of dirt and other foreign matter from theacrylic surface with clean water. Preferred initial application is by sprayingor flooding the surface to wash away any abrasive materials. If spraying orflooding is impractical, a clean sponge or wipe cloth should be used.NOTE: Remove or cover/protect watches, rings, and other metalEFFECTIVITY: ALL12-23-00-100-802-A/300Page 318NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKobject on person (belt buckle, rivets on jeans, tools in pockets)that may cause scratches before any windshield maintenance.(2) Wash gently with 50% water and 50% alcohol TT-I-735 solution containing amild liquid soap in a 2% to 5% concentration.NOTE: The mild liquid soap can be detergents formulated for washingdishes by hand. Dawn, Joy, Palmolive or Ivory are recommended.(3) Rinse thoroughly with clean water and dry with a damp chamois, sponge,or wipe cloth.Q. Job Close-UpCAUTION: TO PREVENT DAMAGE, EXAMINE ALL THE WORK AREASTO MAKE SURE THAT YOU REMOVED ALL TOOLS ANDEQUIPMENT AFTER YOU COMPLETED THE WORK.(1) Remove from the work area all tools, equipment and materials that youused.HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL12-23-00-100-802-A/300Page 319/320NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKGHSH TASK 20-00-00-910-801-A1. Aircraft Maintenance Safety ProceduresA. General(1) This task gives the usual safety procedure for the aircraft maintenance.(2) The functions of this task are to configure the aircraft before the maintenanceprocedures and to restore the aircraft after the maintenance procedures.(3) We recommend the use of a hangar for maintenance procedures.B. Aircraft Safety Procedures for Maintenance Services - MaintenancePractices.(1) For the maintenance procedures, do as follows:WARNING: MAKE SURE THAT THE FLIGHT CONTROLS WILLNOT BE OPERATED WHEN THERE ARE PERSONSNEAR THESE SURFACES.(a) Make sure that the flaps are retracted.(b) Put a warning notice in the cockpit to tell people not to operate the aircraftflight control surfaces.CAUTION: THE EFFECT OF THE PARKING BRAKE CONTINUESFOR 48 HOURS AFTER THEY ARE SET. AFTER THISYOU MUST RELEASE THE EMERGENCY PARKINGBRAKE HANDLE. IF YOU DO NOT OBEY THIS PRE-CAUTION, THE BRAKE PADS MAY STICK TO THEBRAKE DISC AND DAMAGE TO THE EQUIPMENT CANOCCUR.(c) Apply the emergency/parking.WARNING: MAKE SURE THAT THE LANDING GEAR SAFETYPINS ARE INSTALLED. THIS IS TO PREVENTINJURIES TO PERSONS AND DAMAGE TOMATERIAL.(d) Install the LG (Landing Gear) safety pins (GHSH TASK 32-00-00-910-801-A/200).(e) Put the wheel chocks against the LG wheels.CAUTION: THE MODULE OR UNIT CONTAINS ELECTROSTATICDISCHARGE SENSITIVE (ESDS) ITEMS. OBEY THEAPPROVED INDUSTRY PRECAUTIONS WHEN YOUTOUCH, REMOVE, OR INSTALL PARTS OR ASSEM-BLIES. DAMAGE CAN OCCUR FROM ELECTRO-STATIC DISCHARGE.(f) When you work with electronic equipment, obey the ESD (ElectrostaticEFFECTIVITY: ALLCopyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.20-00-00-910-801-A/200Page 201NOV 20/09HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.

GROUND HANDLING ANDSERVICING HANDBOOKHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.Discharge Sensitive) rules (GHSH TASK20-40-00-910-801-A/200).(g) Use the approved platforms to get access to the aircraft.(h) Keep the area around the aircraft free from residues, grease, oil andfuel.(i) Put "NO SMOKING" placards around the maintenance area.WARNING: DO NOT GET HYDRAULIC FLUID, FUEL, OR VAPOURCYCLE REFRIGERANT FLUID ON YOUR SKIN, INYOUR EYES, OR MOUTH. PUT ON APPROVEDPROTECTIVE CLOTHING, GLOVES AND GOGGLES.THESE FLUIDS ARE TOXIC AND CAN CAUSEINJURIES TO YOU(j) Use the correct containers to collect/drain fluids.(k) To prevent accidents, circulation areas outside the work place must beavailable for persons who are not included in the maintenance procedures.(l) If possible, do the maintenance procedures in an isolate area. Let aradius of at least 3m from other aircraft.WARNING: MAKE SURE THAT THERE ARE NO PERSONS OREQUIPMENT IN THE RANGE OF TRAVEL OF THELANDING GEAR. INJURY TO PERSONS OR DAMAGETO EQUIPMENT CAN OCCUR IF THE AREA IS NOTCLEAR.(m) If necessary to retract and extend the nose landing gear and the mainlanding gears, isolate the area around them to prevent injures to personsand damage to the system.WARNING: OBEY THE FUEL SYSTEM SAFETY PRECAUTIONS.THIS IS TO PREVENT INJURY TO PERSONS ANDDAMAGE TO THE EQUIPMENT.(n) When you work with fuel system, obey the safety precautions given inGHSH TASK 28-00-00-910-801-A/200.(2) Before you do maintenance operations near the wings, attach a blanket ofbubble plastic over the deicer with adhesive tape.C. Aircraft Restore Procedures for Maintenance Services - MaintenancePractices(1) To restore the aircraft after the maintenance procedure, do as follows:(a) Remove the warning notice in the cockpit that tells people not to operatethe aircraft flight controls.(b) Remove all circuit breaker ring and tag that you installed in the CBP.CAUTION: TO PREVENT DAMAGE, EXAMINE ALL THE WORKAREAS TO MAKE SURE THAT YOU REMOVED ALLEFFECTIVITY: ALL20-00-00-910-801-A/200Page 202NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKTOOLS AND EQUIPMENT AFTER YOU COMPLETEDTHE WORK.(c) Remove the platforms, safety devices, tools, equipment and unwantedmaterials from the work area.HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL20-00-00-910-801-A/200Page 203NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.ABAAWHEELCHOCKSEMERG/PARKBRAKE HANDLEBEM500ENGHSH200001A.DGNEFFECTIVITY: ALLAircraft Safe for Maintenance - Maintenance PracticesFigure 201Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.20-00-00-910-801-A/200Page 204NOV 20/09

GROUND HANDLING ANDSERVICING HANDBOOKGHSH TASK 20-40-02-910-801-A1. Static Grounding - Standard PracticesA. General(1) The aircraft has one grounding point on the undersurface of each wing leadingedge and one grounding point on the nose landing gear.(2) Bonding is the process of connecting two or more conductive objects witha conductor to make sure that there is the same electrical potentialbetween them.(3) Grounding is the process of connecting two or more conductive objectswith a conductor to the ground.(4) Static Grounding is mandatory in the following situations:(a) Maintenance in the aircraft with power tools, lights or any other equipmentconnected to a power source.(b) Maintenance or servicing operations outside the aircraft, during electricalstorms.(5) For fuel system servicing, the electrical bonding between the aircraft andthe refueling equipment is necessary to prevent sparks generatedbecause of differential potential between them. Static Grounding is recommended.(6) For oxygen system servicing, there are two options to prevent sparkscaused by static charges:(a) Static grounding of the aircraft and oxygen system servicing equipmentare necessary, or;(b) Electrical bonding between the aircraft and the oxygen system servicingequipment is necessary. Static Grounding is recommended.B. Static Grounding - Standard Practices (Figure 201) (Figure 202)WARNING: DURING ATMOSPHERIC ELECTRICAL DISTURBANCES,DO NOT WEAR HEADSET, TOUCH EQUIPMENTELECTRICALLY CONNECTED TO THE AIRCRAFT, ORHOLD A GROUND CONNECTION. A LIGHTNING STRIKECAN CAUSE SEVERE INJURY TO PERSONS.(1) Make sure that the aircraft is parked adjacent to an approved and identifiedgrounding point.NOTE: The approved and identified grounding points can be locatedin the parking surface or another fixed location.(2) Examine the static discharge cable for damage and make sure that theend-fittings are correctly attached.NOTE: • For static grounding with the use of the wing leading edgepoints, use a flexible grounding cable with a plug or with agrounding clamp.EFFECTIVITY: ALLCopyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.20-40-02-910-801-A/200Page 201Rev.01 - MAY 28/10HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.

GROUND HANDLING ANDSERVICING HANDBOOKHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.• For static grounding with the use of the nose landing gearpoint, use only a flexible grounding cable with a groundingclamp.WARNING: ALWAYS ATTACH THE GROUNDING CABLE TO THEGROUNDING CONNECTION FIRST. DO NOT ATTACHTHE CABLE TO THE AIRCRAFT AND THEN TO THEGROUNDING CONNECTION.(3) For aircraft static grounding, use one of the two options that follow:(a) For the grounding point on the undersurface of the wings:1. Connect the grounding cable end to a grounding point in the hangar,and the grounding cable clamp/plug to the static grounding point onthe undersurface of the left/right wing leading edge (Figure 201);(b) For the grounding point on the nose landing gear:1. Connect the grounding cable to a grounding point in the hangar andattach the grounding clamp to the nose landing gear groundingpoint (Figure 202).(4) For oxygen or fuel system servicing, do the electrical bonding of the aircraftto servicing equipment as follows:(a) Connect the bonding cable to the servicing equipment.(b) Connect the grounding clamp/plug of the bonding cable to the approvedstatic grounding point on the aircraft (Figure 201) (Figure 202).EFFECTIVITY: ALL20-40-02-910-801-A/200Page 202Rev.01 - MAY 28/10Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKZONES541641AAGROUNDINGPOINTATYPICALHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.BEM500ENGHSH200005B.DGNEFFECTIVITY: ALLWing Ground PointsFigure 20120-40-02-910-801-A/200Page 203Rev.01 - MAY 28/10Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKAZONE711HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.GROUNDINGPOINTGROUNDINGCLAMPBAEND CONNECTED TO THESERVICING EQUIPMENTOR AT AN APPROPRIATEGROUNDING POINTBEM500ENGHSH200004A.DGNEFFECTIVITY: ALLLanding Gear Ground PointFigure 20220-40-02-910-801-A/200Page 204NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKGHSH TASK 24-36-01-000-801-A1. Main Battery - RemovalA. General(1) This task gives the procedure to remove the main batteries.(2) There are 2 batteries. Battery 1 is installed in the RH (Right Hand) forwardcompartment, and battery 2 is installed in a non-controlled environmentcompartment in the RH (Right Hand) wing-to-fuselage aft.B. Job Set-UpWARNING: MAKE SURE THAT THE AIRCRAFT IS IN A SAFECONDITION BEFORE YOU DO THE MAINTENANCEPROCEDURES. THIS IS TO PREVENT INJURY TOPERSONS AND/OR DAMAGE TO THE EQUIPMENT.(1) Do the procedure to make the aircraft safe for maintenance (GHSH TASK20-00-00-910-801-A/200).(2) On the ELECTRICAL control panel, put a DO NOT OPERATE, tag on theBATT 1 and BATT 2 switches. Refer to Figure 401.(3) To get access to battery 1, do as follows:(a) Open the forward baggage door.(b) Remove the access panel 212CZ.(4) To get access to battery 2, do as follows:(a) Open the access door 195FR.C. Main Battery - Removal(1) Remove battery 1 as follows: (Refer to Figure 402)(a) Loosen the clamp that attaches the air-escape hose to battery 1.(b) Move the clamp to the center of the air-escape hose.(c) Pull the air-escape hose from the battery 1 outlet.(d) Remove the clamp from air-escape hose.WARNING: USE EYE PROTECTION WHEN YOU REMOVE ORINSTALL LOCK WIRE OR SAFETY CABLE. IF YOUDO NOT USE EYE PROTECTION, PIECES OF WIRECAN HIT YOUR EYES AND CAUSE INJURY TO THEM.(e) Cut the lock wire from the electrical connector.(f) Disconnect the electrical connector from the connector of the battery 1.(g) Put a protective cap on the electrical connector and on the connectorof the battery 1.(h) Carefully pull and remove the battery 1 from the aircraft.(2) Remove battery 2 as follows: (Refer to Figure 403)HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL24-36-01-000-801-A/400Page 401NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKWARNING: USE EYE PROTECTION WHEN YOU REMOVE ORINSTALL LOCK WIRE OR SAFETY CABLE. IF YOUDO NOT USE EYE PROTECTION, PIECES OF WIRECAN HIT YOUR EYES AND CAUSE INJURY TO THEM.HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.(a) Cut the lock wire from the electrical connector.(b) Disconnect the electrical connector from the connector of the battery 2.(c) Put a protective cap on the electrical connector and on the connectorof the battery 2.(d) Loosen the self-locking retainer.(e) Carefully pull and remove the battery 2 from the aircraft.EFFECTIVITY: ALL24-36-01-000-801-A/400Page 402NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKAGEN 1BATT 1AUTOOFFONOFFELECTRICALGPUBUS TIEAUTO1 OPEN 2 OPENELEC EMERGEN 2BATT 2AUTOOFFONOFFHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.ELECTRICAL CONTROLPANELAEM500ENGHSH240007A.DGNElectrical Control Panel - LocationFigure 401EFFECTIVITY: ALL24-36-01-000-801-A/400Page 403NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKZONE212AB212 CZHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.CELECTRICALCONNECTORBBATTERY 1CACLAMPAIRESCAPEHOSEEM500ENGHSH240008A.DGNMain Battery 1 - Removal/InstallationFigure 402EFFECTIVITY: ALL24-36-01-000-801-A/400Page 404NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKZONE195AELECTRICALCONNECTORBATTERY 2BAHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.BSELF−LOCKINGRETAINER (2x)EM500ENGHSH240009A.DGNMain Battery 2 - Removal/InstallationFigure 403EFFECTIVITY: ALL24-36-01-000-801-A/400Page 405/406NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKGHSH TASK 24-36-01-000-802-A1. Main Battery - DisconnectionA. General(1) This task gives the procedure to disconnect the main batteries from theelectrical bus.(2) There are 2 batteries. Battery 1 is installed in the RH (Right Hand) forwardcompartment, and battery 2 is installed in a non-controlled environmentcompartment, in the RH (Right Hand) aft wing-to-fuselage fairing.B. Job Set-UpWARNING: MAKE SURE THAT THE AIRCRAFT IS IN A SAFECONDITION BEFORE YOU DO THE MAINTENANCEPROCEDURES. THIS IS TO PREVENT INJURY TOPERSONS AND/OR DAMAGE TO THE EQUIPMENT.(1) Do the procedure to make the aircraft safe for maintenance (GHSH TASK20-00-00-910-801-A/200).(2) On the ELECTRICAL control panel, put a DO NOT OPERATE tag on theBATT 1 and BATT 2 switches.(3) To get access to battery 1, do as follows:(a) Open the forward baggage door.(b) Remove the access panel 212CZ.(4) To get access to battery 2, do as follows:(a) Open the access door 195FR.C. Main Battery - Disconnection(1) Disconnect battery 1 from the electrical bus as follows: (Refer to figure 402)(a) Disconnect the electrical connector from the battery connector.(b) Put a protective cap on the electrical connector and on the battery connector.(2) Disconnect battery 2 from the electrical bus as follows: (Refer to figure 403)(a) Disconnect the eletrical connector from the battery connector.(b) Put a protective cap on the electrical connector and on the battery connector.HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL24-36-01-000-802-A/400Page 401Rev.10 - AUG 27/10Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKAHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.GEN 1BATT 1AUTOOFFONOFFELECTRICALGPUBUS TIEAUTO1 OPEN 2 OPENELEC EMERGEN 2BATT 2AUTOOFFONOFFELECTRICAL CONTROLPANELAEM500ENGHSH240007A.DGNElectrical Control Panel - LocationFigure 401EFFECTIVITY: ALL24-36-01-000-802-A/400Page 402NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKZONE212AB212 CZCBBATTERYCONNECTORAMAIN BATTERYHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.ELECTRICALCONNECTORCEM500ENGHSH240010A.DGNEFFECTIVITY: ALLMain Battery 1 - Disconnection/ConnectionFigure 402Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.24-36-01-000-802-A/400Page 403NOV 20/09

GROUND HANDLING ANDSERVICING HANDBOOKZONE195AHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.ELECTRICALCONNECTORBATTERY 2SELF−LOCKINGRETAINER (2x)B195FRABEM500ENGHSH240011A.DGNMain Battery 2 - Disconnection/ConnectionFigure 403EFFECTIVITY: ALL24-36-01-000-802-A/400Page 404NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKGHSH TASK 24-36-01-400-801-A1. Main Battery - InstallationA. General(1) This task gives the procedure to install the main batteries.(2) There are 2 batteries. Battery 1 is installed in the RH (Right Hand) forwardcompartment, and battery 2 is installed in a non-controlled environmentcompartment in the RH (Right Hand) wing-to-fuselage aft fairing.B. Job Set-Up(1) Make sure that the aircraft is in the same configuration as it was at the endof the removal task (GHSH TASK 24-36-01-000-801-A/400).C. Main Battery - Installation(1) Install the battery 1 as follows: (Refer to figure 402)(a) Carefully put the battery 1 in its installation position.(b) Put the clamp to the air-escape hose.(c) Install the air-escape hose to battery 1 outlet.NOTE: • Before the installation of the air-escape hose, make surethat its interior and outlets are dry and clear of unwantedmaterial.• Make sure that there are no kinks in the air-escape hosethat can prevent airflow.(d) Tighten the hose clamp.(e) Remove the protective cap from the electrical connector and from theconnector of the battery 1.(f) Connect the electrical connector to the battery 1.(g) Safety the electrical connector with lock wire.(2) Install the battery 2 as follows: (Refer to figure 403)(a) Carefully put the battery 2 in its installation position.(b) Tighten the self-locking retainers.(c) Remove the protective cap from the electrical connector and from theconnector of the battery 1.(d) Connect the electrical connector to the battery 1.(e) Safety the electrical connector with lock wire.D. Job Close-Up(1) Remove all tools, equipment and unwanted materials from the work area.(2) For battery 1:(a) Install the access panel 212CZ.(b) Close the forward baggage-compartment door.(3) For battery 2, close the access door 195FR.HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL24-36-01-400-801-A/400Page 401NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKZONE212AB212 CZHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.CELECTRICALCONNECTORBBATTERY 1CACLAMPAIRESCAPEHOSEEM500ENGHSH240008A.DGNMain Battery 1 - Removal/InstallationFigure 401EFFECTIVITY: ALL24-36-01-400-801-A/400Page 402NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKZONE195AELECTRICALCONNECTORBATTERY 2BAHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.BSELF−LOCKINGRETAINER (2x)EM500ENGHSH240009A.DGNEFFECTIVITY: ALLMain Battery 2 - Removal/InstallationFigure 402Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.24-36-01-400-801-A/400Page 403/404NOV 20/09

GROUND HANDLING ANDSERVICING HANDBOOKGHSH TASK 24-36-01-400-802-A1. Main Battery - ConnectionA. General(1) This task gives the procedure to connect the main batteries.(2) There are 2 batteries. Battery 1 is installed in the RH (Right Hand) forwardcompartment, and battery 2 is installed in a non-controlled environmentcompartment, in the RH (Right Hand) wing-to-fuselage aft fairing.B. Job Set-Up(1) Make sure that the aircraft is in the same configuration as it was at the endof the removal task (GHSH TASK 24-36-01-000-802-A/400).C. Main Battery - Connection(1) Connect battery 1 as follows: (Refer to Figure 401)(a) Remove the protective cap from the electrical connector and from thebattery connector.(b) Connect the electrical connector to the battery connector.(2) Connect battery 2 as follows: (Refer to Figure 402)(a) Remove the protective cap from the electrical connector and from thebattery connector.(b) Connect the electrical connector to the battery connector.D. Job Close-Up(1) Remove all tools, equipment and unwanted materials from the work area.(2) For battery 1:(a) Install the access panel 212CZ.(b) Close the forward baggage-compartment door.(3) For battery 2, close the access door 195FR.(4) On the ELECTRICAL control panel, remove the DO NOT OPERATE tagfrom the BATT 1 and BATT 2 switches.HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL24-36-01-400-802-A/400Page 401Rev.10 - AUG 27/10Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKZONE212AB212 CZHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.CBBATTERYCONNECTORAMAIN BATTERYELECTRICALCONNECTORCEM500ENGHSH240010A.DGNMain Battery 1 - Disconnection/ConnectionFigure 401EFFECTIVITY: ALL24-36-01-400-802-A/400Page 402NOV 20/09CCopyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKZONE195AELECTRICALCONNECTORBATTERY 2SELF−LOCKINGRETAINER (2x)B195FRABEM500ENGHSH240011A.DGNHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.Main Battery 2 - Disconnection/ConnectionFigure 402EFFECTIVITY: ALL24-36-01-400-802-A/400Page 403NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKAHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.GEN 1BATT 1AUTOOFFONOFFELECTRICALGPUBUS TIEAUTO1 OPEN 2 OPENELEC EMERGEN 2BATT 2AUTOOFFONOFFELECTRICAL CONTROLPANELAEM500ENGHSH240007A.DGNElectrical Control Panel - Disconnection/ConnectionFigure 403EFFECTIVITY: ALL24-36-01-400-802-A/400Page 404NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKGHSH TASK 24-41-00-860-801-A1. Energization of the Aircraft with an External DC Power Supply - Aircraft/System ConfigurationA. General(1) This task gives the procedure to supply electrical power to the aircraft withan external DC (Direct Current) power supply.(2) The 28 V DC (Volt Direct Current), external power supply is connected tothe aircraft through the receptacle installed on the left side of the rear fuselage.B. Job Set-UpWARNING: MAKE SURE THAT IT IS SAFE TO ENERGIZE THEAIRCRAFT. CIRCUITS THAT ARE NOT SAFE CANCAUSE INJURY TO PERSONS AND/OR DAMAGE TOEQUIPMENT.(1) Make sure that the external power supply operates correctly before yousupply power to the aircraft.(2) Do the procedure to make the aircraft safe for maintenance (GHSH TASK20-00-00-910-801-A/200).(3) If the conditioned air is not necessary, open these circuit breakers andattach a circuit breaker ring and tag to each one of them:• TEMP PWR 1-LHCBP (EMERGENCY BUS 1 AIR COND)• TEMP PWR 2-RHCBP (DC BUS 2 AIR COND PRESN)(4) On the LH (Left Hand) lateral console, on the ELECTRICAL control panel,make sure that these switches are set to these positions:• BUS TIE - AUTO• ELEC EMER - unlatched (off)• BATT 1 - OFF• BATT 2 - OFF(5) Set the GPU (Ground Power Unit) (GSE 016) to ON. Refer to the GSEAppendix.(6) Adjust the output voltage of the external DC power supply to 28 V DC.(7) Set the GPU (GSE 016) to OFF. Refer to the GSE Appendix.(8) Open the access door 195CL to get access to the external DC power-supplyreceptacle.C. Energization of the Aircraft with an External DC Power Supply - MaintenancePractices(1) Connect the GPU (GSE 016) to the external DC power-supply receptacle.Refer to the GSE Appendix.(2) Set the GPU (GSE 016) to ON. Refer to the GSE Appendix.(3) On the ELECTRICAL control panel, do the steps that follow:HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL24-41-00-860-801-A/200Page 201NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOK• Set the BATT 2 switch to ON.• Set the BATT 1 switch to ON.(4) Make sure that the AVAIL lamp in the GPU pushbutton comes on.(5) Set the GPU pushbutton to the latched (on) position.Result:• The AVAIL lamp in the GPU pushbutton goes off.• The IN USE lamp in the GPU pushbutton comes on.(6) On the MFD (Multi Function Display), on the ELEC page, make sure thatthe electrical synoptic status shows as follows:HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.Table 201 - ELECTRICAL SYNOPTIC STATUSBUS/LINE STATUS COLORAll Buses Energized GreenCENTRAL BUS to DC BUS 1 Energized GreenCENTRAL BUS to DC BUS 2 Energized GreenCENTRAL BUS to DC BUS 2 De-energized WhiteEFFECTIVITY: ALL24-41-00-860-801-A/200Page 202NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKAGEN 1BATT 1AUTOOFFONOFFELECTRICALGPUBUS TIEAUTO1 OPEN 2 OPENELEC EMERGEN 2BATT 2AUTOOFFONOFFHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.ELECTRICAL CONTROLPANELAEM500ENGHSH240007A.DGNElectrical Control Panel - LocationFigure 201EFFECTIVITY: ALL24-41-00-860-801-A/200Page 203NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKAZONE195HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.BABEXTERNAL DCPOWER RECEPTACLEEM500ENGHSH240012A.DGNEnergization of the Aircraft with anExternal DC Power Supply - Maintenance PracticesFigure 202EFFECTIVITY: ALL24-41-00-860-801-A/200Page 204NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKGHSH TASK 24-41-00-860-802-A1. Aircraft De-energization - Aircraft/System ConfigurationA. General(1) This task gives the procedure to remove the electrical power from the aircraftsupplied by an external DC (Direct Current) power supply.(2) The 28 V DC (Volt Direct Current), external power supply is connected tothe aircraft through the receptacle installed on the left side of the rear fuselage.B. Job Set-UpWARNING: MAKE SURE THAT THE AIRCRAFT IS IN A SAFECONDITION BEFORE YOU DO THE MAINTENANCEPROCEDURES. THIS IS TO PREVENT INJURY TOPERSONS AND/OR DAMAGE TO THE EQUIPMENT.(1) Make sure that the aircraft is in the same configuration as it was at the endof the energization task (GHSH TASK 24-41-00-860-801-A/200).C. Aircraft De-energization - Maintenance Practices(1) Do these procedures to de-energize the aircraft:(a) On the ELECTRICAL control panel, set the BATT 1 and BATT 2switches to OFF.(b) On the ELECTRICAL control panel, set the GPU pushbutton to thelatched-out (off) position.Result:1. The IN USE lamp in the GPU pushbutton goes off.2. The AVAIL lamp in the GPU pushbutton comes on.(c) Set the GPU (GSE 016) to OFF. Refer to the GSE Appendix.Result:1. On the ELECTRICAL control panel, the AVAIL lamp in the GPUpushbutton goes off.WARNING: REMOVE THE ELECTRICAL POWER FROM THEEXTERNAL POWER CABLE BEFORE YOU REMOVEIT FROM THE AIRCRAFT. IF YOU DO NOT OBEY THISPRECAUTION, AN ELECTRIC SHOCK CAN OCCURAND CAUSE INJURY TO PERSONS.(d) Disconnect the GPU (Ground Power Unit) (GSE 016) from the externalDC power receptacle. Refer to the GSE Appendix.D. Job Close-Up(1) Close access door 195CL.(2) If applicable, remove the circuit breaker ring and tag from these circuitbreakers and close them:HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL24-41-00-860-802-A/200Page 201NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOK• TEMP PWR 1-LHCBP (EMERGENCY BUS 1 AIR COND)• TEMP PWR 2-RHCBP (DC BUS 2 AIR COND PRESN)(3) Remove from the work area all tools, equipment, and materials that youused.HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL24-41-00-860-802-A/200Page 202NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKAGEN 1BATT 1AUTOOFFONOFFELECTRICALGPUBUS TIEAUTO1 OPEN 2 OPENELEC EMERGEN 2BATT 2AUTOOFFONOFFHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.ELECTRICAL CONTROLPANELAEM500ENGHSH240007A.DGNElectrical Control Panel - LocationFigure 201EFFECTIVITY: ALL24-41-00-860-802-A/200Page 203NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKAZONE195HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.BABEXTERNAL DCPOWER RECEPTACLEEM500ENGHSH240012A.DGNDe-energization of the Aircraft with anExternal DC Power Supply - Maintenance PracticesFigure 202EFFECTIVITY: ALL24-41-00-860-802-A/200Page 204NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKGHSH TASK 27-04-01-710-801-A1. Trim Actuator Controller - Operational TestA. General(1) This task gives the procedure to do the operational check of trim actuatorcontroller (TAC).B. Job Set-UpWARNING: MAKE SURE THAT THE AIRCRAFT IS IN A SAFECONDITION BEFORE YOU DO THE MAINTENANCEPROCEDURES. THIS IS TO PREVENT INJURY TOPERSONS AND/OR DAMAGE TO THE EQUIPMENT.(1) Energize the aircraft with an external DC power supply (GHSH TASK 24-41-00-860-801-A/200).C. Trim Actuator Controller - Operational Test(1) Do the operational check of the roll trim system as follows:(a) On the TRIM control panel, turn the roll trim switch and do a full traveltest.NOTE: If you operate the trim switch for more than 3 seconds, theTAC automatically stops the motion.(b) Make sure that the roll trim indication on the MFD (Multi-Function Display)makes a full travel.(2) Do the operational test of the yaw trim system as follows:(a) On the TRIM control panel, push the yaw trim switch and do a fulltravel test.NOTE: If you operate the trim switch for more than 3 seconds, theTAC automatically stops the motion.(b) Make sure that the yaw trim indication on the MFD makes a full travel.D. Job Close-Up(1) De-energize the aircraft (GHSH TASK 24-41-00-860-802-A/200).(2) Remove from the work area all tools, equipment, and materials that youused.HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL27-04-01-710-801-A/500Page 501NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.TRIMSAROLLYAWMFD DISPLAYTRIM INDICATIONSAPITCH20BTRIMYAWLEFTRIGHTROLLLWDRWDPITCH BKPDNUPMODEBKPOFFYAW TRIMSWITCHROLL TRIMSWITCHBACKUP PITCHTRIM SWITCHBEM500ENGHSH270002A.DGNEFFECTIVITY: ALLTrim Actuator Controller - Operational TestFigure 501Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.27-04-01-710-801-A/500Page 502NOV 20/09

GROUND HANDLING ANDSERVICING HANDBOOKGHSH TASK 28-00-00-910-801-A1. Fuel - Maintenance and Servicing PracticesA. General(1) This task gives procedures and information related to the maintenanceand servicing of the fuel system.B. General Warnings for the Fuel System Maintenance and Servicing ProceduresWARNING: • FOR CORRECT AND CAREFUL HANDLING OF FUELAND SUPPORT EQUIPMENT, MAINTENANCEPERSONNEL MUST KNOW THE SYSTEM AND ITSSAFETY CONDITIONS. MAKE SURE THAT ONLYTRAINED AND APPROVED PERSONNEL DO THE FUELSYSTEM MAINTENANCE.• IF FUEL GETS INTO YOUR EYES, WASH THE EYESIMMEDIATELY WITH A LARGE QUANTITY OF WATER.GET MEDICAL AID IMMEDIATELY.• IMMEDIATELY REMOVE CLOTHING THAT IS WET WITHFUEL. ALL JET FUELS CAN CAUSE INJURY TO THESKIN. FULLY FLUSH THE RELATED SKIN AREA. DONOT LET THESE FUELS TOUCH YOU.• DO NOT WEAR CLOTHING MADE OF SYNTHETICMATERIAL OR CLOTHING WITH METAL ZIPPERS ORBUTTONS. THESE ITEMS CAN CAUSE A SPARK. ASRESULT, A FIRE OR EXPLOSION CAN OCCUR.• WHEN YOU DO MAINTENANCE ON THE FUELSYSTEM, YOU MUST DISCHARGE THE STATICELECTRICITY FROM YOUR BODY. FOR THIS, YOUMUST TOUCH A STATIC GROUND CABLE ORGROUNDED OBJECT BEFORE YOU START THEOPERATION.• DO THE FUEL SYSTEM MAINTENANCE ONLY IN ANAREA THAT PERMITS FREE MOVEMENT AND ACCESSOF FIRE FIGHTING EQUIPMENT AND PERSONNEL.MAKE SURE THAT FIRE EXTINGUISHERS WITH AMINIMUM OF 55 LB (25 KGF) OF CARBON DIOXIDE, OREQUIVALENT, ARE AVAILABLE AND READY FOR USEIN AN EMERGENCY SITUATION. USE ONLYEXPLOSION-PROOF EQUIPMENT WHEN YOU DOTASKS AT LESS THAN 15 M (50 FT) AWAY FROM ANHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL28-00-00-910-801-A/200Page 201NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALLOPEN TANK OR HAZARDOUS LOCATIONS.• ALWAYS DO MAINTENANCE ON THE FUEL SYSTEM INAN AREA THAT HAS A GOOD AIRFLOW. NO FUELVAPOR CONCENTRATION IS PERMITTED. THIS IS TOPREVENT A FIRE OR EXPLOSION.• ALL SUPPORT EQUIPMENT NOT NECESSARY FORTHESE TASKS MUST BE AT A MINIMUM DISTANCE OF15 M (50 FT) FROM THE AIRCRAFT.• MAKE SURE THAT THERE ARE NO PERSONS WITHLIT CIGARETTES OR OTHER SOURCES OF SPARKSOR OPEN FLAMES IN A RADIUS OF 15 M (50 FT) FROMTHE AREA WHERE THE MAINTENANCE IS DONE.• INSTALLATION OR REMOVAL OF THE BATTERIES ORRELATED EQUIPMENT IS NOT PERMITTED.• STATICALLY GROUND THE ELECTRIC EQUIPMENT TOPREVENT A HIGH CONCENTRATION OF STATICELECTRICITY WHEN YOU USE THE EQUIPMENT.• ALL EXTERNAL LIGHT SOURCES MUST BE AWAYFROM THE AIRCRAFT BEFORE YOU START TO DOTHE TASKS.• DO NOT USE HEAT GUNS AT LESS THAN 35 M (100 FT)FROM THE AIRCRAFT WHEN YOU REFUEL ORDEFUEL THE TANK. OBEY THE SAME DISTANCEWHEN THE FUEL LINES ARE OPEN. IF YOU DO NOTOBEY THIS PRECAUTION, AN EXPLOSION CANOCCUR IN THE FUEL TANK.(1) Obey these safety precautions and warnings when you do maintenance orservicing procedures in the fuel system.C. Specific Warnings for Servicing ProceduresWARNING: • DO NOT DO THE REFUELING PROCEDURE IN AHANGAR OR AT LESS THAN 30 M (100 FT) FROMHANGARS.• DURING THE PRESSURE REFUELING PROCEDURE,KEEP THE AREAS AROUND THE FUEL TANKS ANDVENTS WITH NO VEHICLES AND EQUIPMENT.• DURING THE REFUELING OPERATION, MAKE SURETHAT NO HIGH-FREQUENCY RADIO TRANSMITTER ISIN OPERATION AT LESS THAN 60M (200 FT) FROM THEAIRCRAFT. NO RADAR EQUIPMENT MUST BE IN28-00-00-910-801-A/200Page 202NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKOPERATION AT 120 M (400 FT) FROM THE AIRCRAFT.THIS IS TO PREVENT A FIRE OR EXPLOSION.• MAKE SURE THAT THE AIRCRAFT IS PARKED ATRAMP LEVEL AND INTO THE WIND.• DO NOT REFUEL THE AIRCRAFT IF THERE IS ANOVERHEAT INDICATION IN THE AIRCRAFT.• DO NOT FILL OR CHANGE THE OXYGEN BOTTLEDURING THE REFUELING PROCEDURES.• PREVENT FUEL SPILLAGE. IF FUEL SPILLAGEOCCURS, CLEAN THE AREA IMMEDIATELY.• WHEN YOU REFUEL THE AIRCRAFT, MAKE SURETHAT THE FUEL QUANTITY UNIT IS CORRECT. ANINCORRECT READING OF THE FUEL QUANTITY CANCAUSE AN AIRCRAFT ACCIDENT.• MAKE SURE THAT THE FUEL LEVEL IN THE TANKS ISSYMMETRICAL AFTER THE REFUELING OPERATIONIS COMPLETE.• STOP THE REFUELING PROCEDURE WHEN THEREARE THUNDERSTORMS OR LIGHTNING AT ADISTANCE OF LESS THAN 16 KM (10 MILES).(1) Obey these safety precautions and warnings when you do the servicingprocedures in the fuel system.HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL28-00-00-910-801-A/200Page 203/204NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKGHSH TASK 29-10-00-910-801-A1. Main Hydraulic System - DepressurizationA. General(1) This task gives the procedure to release the pressure from the hydraulicsystem.B. Job Set-UpWARNING: MAKE SURE THAT THE AIRCRAFT IS IN A SAFECONDITION BEFORE YOU DO THE MAINTENANCEPROCEDURES. THIS IS TO PREVENT INJURY TOPERSONS AND/OR DAMAGE TO THE EQUIPMENT.(1) Do the procedure to make the aircraft safe for maintenance (GHSH TASK20-00-00-910-801-A).(2) Remove access panel 242AZ to get access to the RPDU.(3) Open these circuit breakers and put a circuit breaker ring and tag on eachone of them:• SC1 AUX CTRL-LPDU (CENTRAL BUS)• SC2 AUX CTRL-RPDU (CENTRAL BUS)C. Depressurization of the Hydraulic SystemWARNING: DO NOT TOUCH THE EXHAUST DUCT AND ENGINECOMPONENTS UNTIL THEY ARE COOL. THETEMPERATURE CAN STAY HIGH FOR A LONG TIMEAFTER THE ENGINE STOPS. IF YOU DO NOT OBEY THISPRECAUTION, YOU CAN BURN YOURSELF.(1) If the engines are in operation, stop the engine (AMM TASK 71-00-01-910-804-A/200 ).(2) If a Hydraulic Test Stand is installed on the aircraft, remove it.(3) Look at the MFD and make sure the hydraulic pressure is close to zero (0).(4) Release the pressure from the emergency/parking brake line as follows:(a) Slowly push and pull the emergency/parking brake T-handle (7 completecycles).(b) The EMERG/PRKG BRAKE lamp will be off after the emergency/parking brke cycles.(5) If you removed the Hydraulic Test Stand, do the servicing of the hydraulicreservoir as follows:CAUTION:MAKE SURE THAT FLUIDS OF DIFFERENT BRANDS ARENOT MIXED IN THE SYSTEM. IF YOU ARE NOT SURE OFWHICH BRAND OF HYDRAULIC FLUID IS IN USE, FLUSHTHE SYSTEM OUT BEFORE YOU FILL IT WITH NEW FLUID.IF YOU MIX FLUIDS OF DIFFERENT BRANDS, THE CHARAC-HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL29-10-00-910-801-A/200Page 201NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.TERISTICS OF THE FLUIDS CAN CHANGE AND PUT THEPERFORMANCE AND SAFETY OF THE SYSTEM AT RISK.(6) The list of approved hydraulic fluid is:• ROYCO 777• Hydraulic fluid Aeroshell Fluid 51(7) The fluids presented in the current revision of the QPL-87257 are consideredalternatives of the recommended fluids.(8) Open access door 195DL.(9) Make sure that the LG is extended, wheels chocked, multifunction spoilersand thrust reversers (optional) stowed, stick pusher and rudder springactuator inactive and brakes released.(10)On the reservoir visual level indicator, make sure that the hydraulic fluidlevel in the reservoir is between the FULL and the OVER FULL lines.Refer to Figure 201.(11)If the fluid level is not between the REFILL and the OVERFULL lines (inthe green area) do the following steps:(a) Do the hydraulic reservoir servicing as follows:CAUTION: MAKE SURE THAT THE FLUID USED ON THEHYDRAULIC SYSTEM IS A SYNTHETIC HYDROCAR-BON BASE HYDRAULIC FLUID PER MILPRF-87257. IFYOU DO NOT OBEY THIS PRECAUTION, DAMAGE TOTHE EQUIPMENT CAN OCCUR.CAUTION: MAKE SURE THAT FLUIDS OF DIFFERENT BRANDSARE NOT MIXED IN THE SYSTEM. IF YOU ARE NOTSURE OF WHICH BRAND OF HYDRAULIC FLUID IS INUSE, FLUSH THE SYSTEM OUT BEFORE YOU FILL ITWITH NEW FLUID. IF YOU MIX FLUIDS OF DIFFERENTBRANDS, THE CHARACTERISTICS OF THE FLUIDSCAN CHANGE AND PUT THE PERFORMANCE ANDSAFETY OF THE SYSTEM AT RISK.(b) Make sure that the hydraulic fluid used in the servicing proceduremeets the specification described above and is of the same brand asthat already in the system.(c) Use a coupling assembly (dash 4) to the suction refill hose.(d) Remove the suction refill quick-disconnect cap.(e) Install the auxiliary hose of the hydraulic reservoir servicing unit to thesuction refill quick-disconnect.(f) Operate the hand pump with an approved hydraulic fluid until the reservoirlevel indicator shows full.NOTE:Make sure that the hydraulic reservoir service unit is filledwith sufficient hydraulic fluid to replenish the aircraftEFFECTIVITY: ALL29-10-00-910-801-A/200Page 202NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKhydraulic fluid reservoirs. If not, air could go into thehydraulic system.(g) Remove the auxiliary hose from the suction refill quick-disconnect.(h) Install the cap on suction refill quick-disconnect.(12)Bleed the air from the hydraulic system as follows:(a) This task gives the procedure to bleed the air from the hydraulic fluid inthe hydraulic system.(b) The bleed of air is necessary when you do:1. A repair in the hydraulic system.2. A task for removal/installation of a component of the hydraulic system.(c) If you removed component(s) from one of these systems:• Spring Loaded Rudder Booster System.• Stick Pusher Actuator.• MultiFunction Spoiler Hydraulic Power Control Unit.• Main Landing Gear.• Nose Landing Gear.• Extension and retraction system.• Main Brake System.• Emergency/Parking Brake System.• Wheel and Brakes.WARNING: MAKE SURE THAT THE AIRCRAFT IS IN A SAFECONDITION BEFORE YOU DO THE MAINTENANCEPROCEDURES. THIS IS TO PREVENT INJURY TOPERSONS AND/OR DAMAGE TO THE EQUIPMENT.(14)Do the procedure to make the aircraft safe for maintenance (GHSH TASK20-00-00-910-801-A/200 ).(15)Pressurize the hydraulic system (GHSH 29-10-00-910-802-A).(16)Cycle at least two of the hydraulic users as necessary to send the airentrapped in the hydraulic lines to the hydraulic reservoir.(17)Open these access doors:• 194EL• 195DL(18)Make sure that the level is correct in the hydraulic reservoir.(19)Do the Bleed of Air of the Hydraulic System as follow (Figure 202):(a) Put a stainless steel container below the work area. The hydraulic fluidwill come out from the hydraulic hose.(b) Push and turn the bleed valve until all the air is removed from thereservoir.NOTE: Use a flashlight while you work on this compartment(c) Wait until all the air is removed, then make sure that the oil that comesHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL29-10-00-910-801-A/200Page 203NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.out is free of bubbles.(d) Use a wiper cloth to clean all the hydraulic fluid from the work area.(20)Make sure that the level is correct in the hydraulic reservoir(21)Close these access doors:• 194EL• 195DL(22)Remove the circuit breaker ring and tag from these circuit breakers andclose them:• SC1 AUX CTRL-LPDU (CENTRAL BUS)• SC2 AUX CTRL-RPDU (CENTRAL BUS)CAUTION: EXAMINE ALL THE WORK AREAS TO MAKE SURE THATYOU REMOVED ALL TOOLS AND EQUIPMENT AFTERYOU COMPLETED THE WORK. THIS IS TO PREVENTINJURY TO PERSONS AND/OR DAMAGE TO THE EQUIP-MENT.(23)Remove from the work area all tools, equipment, and materials that youused.EFFECTIVITY: ALL29-10-00-910-801-A/200Page 204NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOK195DLABZONE194RESERVOIR WITHINTEGRATED MANIFOLD(LH VIEW)HIDRAULICHOSE (REF.)C194ELASUCTION REFILLQUICK−DISCONNECTBCAPBLEEDVALVEHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.CHOSEHYDRAULIC RESERVOIRSERVICE UNIT (REF.)EM500ENGHSH290002A.DGNHydraulic System Reservoir - ServicingFigure 201EFFECTIVITY: ALL29-10-00-910-801-A/200Page 205NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOK195DLABZONE194HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.HYDRAULICMANIFOLD (REF.)HYDRAULICHOSE194ELBLEEDVALVEABEM500ENGHSH290003A.DGNBleed of Air of the Hydraulic SystemFigure 202EFFECTIVITY: ALL29-10-00-910-801-A/200Page 206NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKGHSH TASK 29-10-00-910-802-A1. Main Hydraulic System - Hydraulic System Pressurization with a HydraulicTest Stand (HTS).A. General(1) This task gives the procedure to pressurize the hydraulic system with thehydraulic power unit.(2) The person who will operate the hydraulic ground power unit must beapproved to do it.B. Job Set-UpWARNING: MAKE SURE THAT THE AIRCRAFT IS IN A SAFECONDITION BEFORE YOU DO THE MAINTENANCEPROCEDURES. THIS IS TO PREVENT INJURY TOPERSONS AND/OR DAMAGE TO THE EQUIPMENT.(1) Do the procedure to make the aircraft safe for maintenance (GHSH TASK20-00-00-910-801-A).(2) Open access door 195DL.(3) Energize the aircraft with an external DC power supply (GHSH TASK 24-41-00-860-801-A).C. Hydraulic System-Pressurization with Hydraulic Power Unit(1) Put a stainless steel container below the work area.(2) Remove the dust caps from the pressure and return quick disconnect couplings.(3) Connect the pressure and return hoses of the hydraulic power unit with thepressure (coupling assembly (dash 4)) and return (coupling assembly(dash 6)) quick disconnect couplings to the hydraulic manifold.(4) Energize the hydraulic power unit and start to operate it.NOTE: The hydraulic power unit will drain the hydraulic fluid from thesystem reservoir. Make sure that the hydraulic power unit hasthe capacity to hold the reservoir hydraulic fluid.(5) Set the hydraulic power unit to 20,684 kPa (3,000 psi) and 4.2 l/min (1.1gal/min).NOTE: You can adjust the flow as necessary to do the related task.(6) On the MFD, make sure that the hydraulic pressure increases to 3,000 ±50 psi.(7) When you stop the use of the hydraulic power unit, turn it off and de-energizeit.(8) Disconnect the pressure and return hoses of the hydraulic power unit fromthe pressure and return quick disconnect couplings (1 and 2) of thehydraulic manifold.HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL29-10-00-910-802-A/200Page 201Rev.10 - AUG 27/10Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.(9) Install the dust caps on the pressure and return quick disconnect couplingsof the hydraulic manifold.D. Job Close-Up(1) De-energize the aircraft (GHSH TASK 24-41-00-860-802-A).(2) Do the servicing of the hydraulic reservoir as follows:CAUTION: MAKE SURE THAT FLUIDS OF DIFFERENT BRANDSARE NOT MIXED IN THE SYSTEM. IF YOU ARE NOTSURE OF WHICH BRAND OF HYDRAULIC FLUID IS INUSE, FLUSH THE SYSTEM OUT BEFORE YOU FILL ITWITH NEW FLUID. THIS IS BECAUSE, IF YOU MIXFLUIDS OF DIFFERENT BRANDS, THECHARACTERISTICS OF THE FLUIDS CAN CHANGEAND PUT THE PERFORMANCE AND SAFETY OF THESYSTEM AT RISK.(3) The list of approved hydraulic fluid is:• ROYCO 777• Hydraulic fluid Aeroshell Fluid 51(4) The fluids presented in the current revision of the QPL-87257 are consideredalternatives of the recommended fluids.(5) Release the pressure from the hydraulic system (GHSH TASK 29-10-00-910-801-A ).(6) Make sure that the LG is extended, wheels chocked, multifunction spoilersand thrust reversers (optional) stowed, stick pusher and rudder springactuator inactive and brakes released.(7) On the reservoir visual level indicator, make sure that the hydraulic fluidlevel in the reservoir is between the REFILL and the OVERFILL lines (inthe green area). Refer to Figure 202.(8) If the fluid level is not between the REFILL and the OVERFILL lines (in thegreen area) do the following steps:CAUTION: MAKE SURE THAT THE FLUID USED ON THEHYDRAULIC SYSTEM IS A SYNTHETIC HYDROCAR-BON BASE HYDRAULIC FLUID PER MILPRF-87257. IFYOU DO NOT OBEY THIS PRECAUTION, DAMAGE TOTHE EQUIPMENT CAN OCCUR.CAUTION:MAKE SURE THAT FLUIDS OF DIFFERENT BRANDS ARE NOTMIXED IN THE SYSTEM. IF YOU ARE NOT SURE OF WHICHBRAND OF HYDRAULIC FLUID IS IN USE, FLUSH THE SYS-TEM OUT BEFORE YOU FILL IT WITH NEW FLUID. THIS ISBECAUSE, IF YOU MIX FLUIDS OF DIFFERENT BRANDS, THECHARACTERISTICS OF THE FLUIDS CAN CHANGE AND PUTTHE PERFORMANCE AND SAFETY OF THE SYSTEM AT RISK.EFFECTIVITY: ALL29-10-00-910-802-A/200Page 202Rev.10 - AUG 27/10Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOK(a) Make sure that the hydraulic fluid used in the servicing proceduremeets the specification described above and is of the same brand asthat already in the system.(b) Use a coupling assembly (dash 4) to the suction refill hose.(c) Remove the suction refill quick-disconnect cap.(d) Install the auxiliary hose of the hydraulic reservoir servicing unit to thesuction refill quick-disconnect.(e) Operate the hand pump with an approved hydraulic fluid until the reservoirlevel indicator shows full.NOTE:Make sure that the hydraulic reservoir service unit is filledwith sufficient hydraulic fluid to replenish the aircrafthydraulic fluid reservoirs. If not, air could go into thehydraulic system.(f) Remove the auxiliary hose from the suction refill quick-disconnect.(g) Install the cap on suction refill quick-disconnect.(14)Remove from the work area all tools, equipment, and materials that youused.HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL29-10-00-910-802-A/200Page 203Rev.10 - AUG 27/10Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKACESSDOOR (REF.)HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.03HYDRAULICGROUNDPOWER UNITAZONE19401 DUSTCAP0203QUICK DISCONNECTCOUPLING(RETURN LINE)USED TO ADAPT/CONNECT A HYDRAULIC GROUND−POWER−UNITPRESSURE SOURCE TO THE HYDRAULIC SYSTEMSHYDRAULICPRESSURECOUPLINGUSED TO PRESSURIZE, DRAIN, BLEED, OR FLUSH THE HYDRAULIC SYSTEMS0102BA01BQUICKDISCONNECTCOUPLING(PRESSURE LINE)EM500ENGHSH290001A.DGNHydraulic System-Pressurization with Hydraulic Power UnitFigure 201EFFECTIVITY: ALL29-10-00-910-802-A/200Page 204Rev.10 - AUG 27/10Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOK195DLABZONE194RESERVOIR WITHINTEGRATED MANIFOLD(LH VIEW)HIDRAULICHOSE (REF.)C194ELASUCTION REFILLQUICK−DISCONNECTBCAPBLEEDVALVEHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.CHOSEHYDRAULIC RESERVOIRSERVICE UNIT (REF.)EM500ENGHSH290002A.DGNHydraulic System Reservoir - ServicingFigure 202EFFECTIVITY: ALL29-10-00-910-802-A/200Page 205/206Rev.10 - AUG 27/10Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKGHSH TASK 32-00-00-910-801-A1. Landing-Gear Safety Pin - Standard PracticesA. General(1) The landing-gear safety pins must be installed while the aircraft is parked,during maintenance procedures, and during the towing of the aircraft.B. Job Set-UpWARNING: MAKE SURE THAT THE AIRCRAFT IS IN A SAFECONDITION BEFORE YOU DO THE MAINTENANCEPROCEDURES. THIS IS TO PREVENT INJURY TOPERSONS AND/OR DAMAGE TO THE EQUIPMENT.(1) Make sure that the landing gear control lever is in the DOWN position.C. Landing-Gear Safety Pin - Location(1) Use the landing-gear safety pins to lock the nose and main landing gearsdown.(2) Make sure that personnel can see the red REMOVE-BEFORE-FLIGHTstreamer clearly.HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL32-00-00-910-801-A/200Page 201NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKCAHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.ZONE711BZONES721731CACSAFETY PINBTYPICALEM500ENGHSH320026A.DGNEFFECTIVITY: ALLLanding-Gear Safety Pin - LocationFigure 20132-00-00-910-801-A/200Page 202NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKGHSH TASK 32-45-00-210-801-A1. NLG and MLG Tires - General Visual InspectionA. General(1) This task gives the procedure to do an inspection of the tires of the NLG(Nose Landing Gear) and MLG (Main Landing Gear). This inspection isavisual examination of the tires for wear, damage, and general condition.(2) When you must replace a tire, before you disassemble the wheel assembly,make a mark with a chalk in the damaged area.B. Job Set-UpWARNING: MAKE SURE THAT THE AIRCRAFT IS IN A SAFECONDITION BEFORE YOU DO THE MAINTENANCEPROCEDURES. THIS IS TO PREVENT INJURY TOPERSONS AND/OR DAMAGE TO THE EQUIPMENT.(1) Install the landing-gear safety pins (GHSH TASK 32-00-00-910-801-A/200).C. Nose and Main Wheel Tire - Inspection (Figure 201)WARNING: DO NOT GO NEAR HOT TIRES INSTALLED ON THEAIRCRAFT. IF IT IS NECESSARY TO MEASURE THE TIRETEMPERATURE, GO NEAR THE TIRE FROM ITS FRONT,NOT FROM ITS SIDE. HIGH TEMPERATURE CAN CAUSETIRE EXPLOSION.(1) Examine the tires of the NLG and MLG. Replace the wheel if you find on atire one or more of the conditions that follow:(a) Cut into the casing plies.(b) For NLG tires, damage, cut, or wear on the chine.(c) Cut across the tread rib to the fabric.(d) Rib undercutting.(e) Tread worn, with top fabric worn through for more than 1/8 of the circumferenceof the tire or more than 1 in. (25 mm) wide.EFFECTIVITY: ALLNOTE: Tires within these limits can continue in service no longerthan necessary to be replaced. Tires worn beyond this limitmay be unsafe.NOTE: • For MLG, 1/8 of circumference of the tire is equal to 9.8 in.(250 mm).•For NLG, 1/8 of circumference of the tire is equal to 5.9in. (150 mm).(f) Tread or sidewall bulge.(g) Peeled rib.(h) Thrown tread.(i) Open tread splice.Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.32-45-00-210-801-A/600Page 601Rev.03- FEB 24/11HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.

GROUND HANDLING ANDSERVICING HANDBOOKHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.(j) Heat damage in bead.(k) Impact break.(l) One or more of the conditions that follow with exposed fabric:1. Groove cracking.2. Dry braking flat spot.3. Tread chunking.4. Chevron cutting.5. Sidewall crack.6. Sidewall cut or snag.7. Radial or circumferential crack.(m) If balance is affected because of wet braking flat spot or dry brakingflat spot.NOTE: Uneven wear - if you find irregular wear, the tire can be disassembledand turned in the opposite direction if there isno fabric that can be seen.D. Job Close-Up(1) Put the aircraft back to its initial condition.EFFECTIVITY: ALL32-45-00-210-801-A/600Page 602Rev.03- FEB 24/11Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKAZONE711TREAD010202AZONES721731SIDEWALLBEADCUT ACROSS TREAD RIBS1/8 OF THECIRCUNFERENCE1 inTREAD WORN01CHINEAPPLICABLE ONLY TO THE NLG TIRE.TOP FABRICTREADGROOVECASING PLIES(FABRIC)ATYPICALTREADRIBRIB UNDERCUTTINGTREAD OR SIDEWALL BULGE1/8 OF THE CIRCUNFERENCE = 9.8 in (250 mm) FOR MAIN LANDING GEAROR 5.9 in (150 mm) FOR NOSE LANDING GEAREM500ENGHSH320021D.DGNHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.Nose and Main Wheel Tires - InspectionFigure 201, Sheet 1 of 3EFFECTIVITY: ALL32-45-00-210-801-A/600Page 603Rev.03- FEB 24/11Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.PEELED RIBOPEN TREAD SPLICETHROWN TREADHEAT DAMAGEIMPACT BREAKGROOVE CRACKINGEM500ENGHSH320022C.DGNNose and Main Wheel Tires - InspectionFigure 201, Sheet 2 of 3EFFECTIVITY: ALL32-45-00-210-801-A/600Page 604Rev.02 - AUG 27/10Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKDRY−BRAKING FLAT−SPOTCHEVRON CUTTINGSIDEWALL CRACKSTREAD CHUNKINGCUT OR SNAGHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.RADIAL OR CIRCUMFERENTIAL CRACKWET BRAKING FLAT−SPOTEM500ENGHSH320027B.DGNNose and Main Wheel Tires - InspectionFigure 201, Sheet 3 of 3EFFECTIVITY: ALL32-45-00-210-801-A/600Page 605/606Rev.02 - AUG 27/10Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKGHSH TASK 71-00-01-910-803-A1. Engine Start Procedure (Dry Motoring)A. General(1) This task gives the instructions necessary to do an engine dry motoring.(2) The dry motoring is used to clear the engine during ground operation if it isnecessary to purge the engine of internally trapped fuel and/or fuel fumescaught after an unsatisfactory start, such as prior to checking for igniterfunction. Air passing through the engine will remove fuel or vapor from thecombustion section area, turbines and engine exhaust nozzle.B. Job Set-UpWARNING: MAKE SURE THAT THE AIRCRAFT IS IN A SAFECONDITION BEFORE YOU DO THE MAINTENANCEPROCEDURES. THIS IS TO PREVENT INJURY TOPERSONS AND/OR DAMAGE TO THE EQUIPMENT.(1) Do the procedure to make the aircraft safe for maintenance (GHSH TASK20-00-00-910-801-A).(2) Use a workstand to get access to the engine.(3) Examine the engine air inlet for blockage and unwanted objects.(4) Examine the nacelle assembly for oil or fuel leakage.(5) Make sure that the LG safety pins are installed (GHSH TASK 32-00-00-910-801-A).(6) Install wheel chocks to the MLG wheels.(7) Apply the parking brake.(8) Make sure that there are fire fighting equipment and personnel available.(9) Before you energize the aircraft, set/keep these switches and controls asfollows:SWITH/CONTROLLanding Gear LeverThrust Lever AngleReversionary PanelElectrical fuel pumpPOSITIONDOWNIDLENORMOFFHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.(10)Open these circuit breakers and put a circuit breaker ring and tag on eachone of them:• TEMP PWR 1-LHCBP (DC BUS 1 AIR COND/PRESN)• TEMP PWR 2-RHCBP (DC BUS 2 AIR COND PRESN)(11) Do a check of the engine oil level (GHSH TASK 12-12-00-210-801-A). Ifnecessary, add oil to the engine (GHSH TASK 12-12-00-612-801-A).(12)Energize the aircraft with an external DC power supply (GHSH TASK 24-41-00-860-801-A).EFFECTIVITY: ALL71-00-01-910-803-A/200Page 201NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOK(13)Do a check of the fuel quantity in the engine indication field of the MFD.Replenish as necessary (GHSH TASK 12-11-00-650-801-A).(14)Make sure that all switches/controls of the systems not used for theengine start are OFF/CLOSED.CAUTION: DO NOT OPERATE THE FUEL PUMP WITHOUT FUEL (DRYOPERATION). DRY OPERATION WILL CAUSE DAMAGE TOTHE SYSTEM.(15) Set/keep these switches and controls as follows:HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.SWITH/CONTROLElectrical PowerThrust Lever AngleFADEC Fault IndicationFADEC PowerElectrical Fuel Boost PumpUnnecessary Accessory LoadsIgnitionEngine Bleed AirEngine StarterFuel Cross FeedPOSITIONONIDLECHECKONAUTO or ONOFFOFFOFFSTOPOFF(16)If it is necessary to keep data in the CVDR, open this circuit breaker andput a circuit breaker ring and tag, as applicable:• VOICE/DATA RECORDER-RHCBP (EMERGENCY BUS)(17)Close the windows and doors.(18)Open these circuit breakers and put a circuit breaker ring and tag on eachone of them:• E1 FIREX-LHCBP (HOT BATT BUS 1)• E2 FIREX-RHCBP (HOT BATT BUS 2)(19)On the FIRE/ENG/TRIM control panel, lift the guard and push the SHUT-OFF 1 and SHUTOFF 2 push buttons to close the fuel shutoff valves.NOTE: If you need to discharge the engine fire extinguishing bottleduring the dry motoring procedure, remove the circuitbreaker ring and tag and close the circuit breakers E1FIREX-LHCBP (HOT BATT BUS 1) and E2 FIREX-RHCBP(HOT BATT BUS 2).C. Engine Dry Motoring(1) Make sure that the indication "IGN OFF" shows on the EICAS. If this indicationdoes not show, do not do the dry motoring before you make surethat the ignition system is not on.EFFECTIVITY: ALL71-00-01-910-803-A/200Page 202NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKCAUTION: • ABORT THE DRY MOTORING CYCLE IF YOU SEE THATTHE N2 DOES NOT INCREASE OR THERE IS NO OILPRESSURE INDICATION.• FOR ENGINE GROUND-RUN PROCEDURES, OBEY THEPOWERPLANT OPERATING LIMITATIONS. THIS IS TOPREVENT DAMAGE TO THE EQUIPMENT.(2) Set the ENG START/STOP switch to RUN and momentarily set it toSTART.(3) After the engine stabilizes at idle speed, monitor the engine parameters(ITT, oil pressure and temperature, N2, and fuel flow) on the EICAS. Makesure that the N2 indication increases and the fuel flow indication stays atZERO.D. Job Close-Up(1) On the FUEL control panel, set the DC PUMP 1 or 2 switch to AUTO.(2) On the ELECTRICAL and on the ICE PROTECTION control panels, setthe switches as applicable.(3) Set the ENG START/STOP 1 or 2 switch to STOP.(4) If applicable, remove the circuit breaker ring and tag from each of thesecircuit breakers, and close them:• TEMP PWR 1-LHCBP (DC BUS 1 AIR COND/PRESN)• TEMP PWR 2-RHCBP (DC BUS 2 AIR COND PRESN)• VOICE/DATA RECORDER-RHCBP (EMERGENCY BUS)• E1 FIREX-LHCBP (HOT BATT BUS 1)• E2 FIREX-RHCBP (HOT BATT BUS 2)(5) On the FIRE/ENG/TRIM control panel, lift the guard and push the SHUT-OFF 1 and SHUTOFF 2 push buttons again to open the fuel shutoffvalves.(6) On the HYD PUMP control panel, set the SOV 1 and SOV 2 switches tothe CLOSED position.(7) On the HYD PUMP control panel, set the SOV 1 and SOV 2 switches tothe OPEN position.(8) De-energize the aircraft (GHSH TASK 24-41-00-860-802-A)(9) Remove from the work area all tools, equipment, and materials that youused.HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL71-00-01-910-803-A/200Page 203/204Rev.01 - MAY 28/10Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKAPPENDIXHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.

GROUND HANDLING ANDSERVICING HANDBOOKGROUND SUPPORTEQUIPMENTAPPENDIXHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.

GROUND HANDLING ANDSERVICING HANDBOOKGHSH GSE APPENDIX - TABLE OF CONTENTSGround SupportEquipment AppendixSUBJECT GSE NUMBER PAGECover, Pitot-static ......................................... GSE 003 1Cover-pitot.................................................... GSE 009 1Ground Power Unit....................................... GSE 016 1Sampler, Fuel............................................... GSE 022 1Tool, Defueling ............................................. GSE 023 1Towbar Head................................................ GSE 026 1Towbar.......................................................... GSE 027 1Set-transparency Shade,Cockpit ......................................................... GSE 029 1Cover, Engine............................................... GSE 030 1HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALLGHSH GSE Appendix - Table of ContentsPage TOC-1/2NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKGSE NUMBER: 003ITEM NAME: PITOT-STATIC COVERPURPOSE AND USE: Used to protect the pitot-static port.PART NUMBER: KPC3-640-35 (Figure 1)1. MANUFACTURERSESAME TECHNOLOGIES INC.2. TECHNICAL SPECIFICATIONSA. The cover is made of red KevlarB. It withstands temperatures of 427ºC (800ºF)3. BRIEF OPERATION DESCRIPTIONNot applicable.4. TOOL CONSISTS OFNot applicable.5. REPLACEMENT PARTS LISTNot applicable.6. QUANTITY17. DIMENSIONS AND WEIGHT120 x 15 mm (4.72 x 0.60 in); 0.1 kg (0.22 lb)8. SUPPORTING TOOLSNot applicable.9. GSE MAINTENANCEKeep the cover clean and protected against rain, sun, and dust.10. TOOL HISTORYNot applicable.HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL GSE 003Page 1NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.AAEM500ENGHSH000001A.DGNPitot-Static CoverFigure 1EFFECTIVITY: ALL GSE 003Page 2NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKGSE NUMBER: 008ITEM NAME: PLUG-PROTECTION, STATIC PORTPURPOSE AND USE: Used to protect the static ports.PART NUMBER: AGE-05118-401 (Figure 1)1. MANUFACTURER<strong>EMB</strong>RAER2. TECHNICAL SPECIFICATIONSIt is a pair of machined nylon plugs equipped with a "REMOVE BEFOR FLIGHT" flag.3. BRIEF OPERATION DESCRIPTIONNot applicable.4. TOOL CONSISTS OFNot applicable.5. REPLACEMENT PARTS LISTItem Nomenclature P/N Quantity1 Plug AGE-05118-901 22 Flag PE915103-5NF 16. QUANTITY27. DIMENSIONS AND WEIGHT38 x 16 mm (1.5 x 0.63 in); 0.1 kg (0.22 lb)NOTE: The dimensions above refer to the nylon plug.8. SUPPORTING TOOLSNot applicable.9. GSE MAINTENANCEKeep the plugs clean and protected against rain, sun, and dust.Before and after using the plugs, make sure that they are in perfect conditions.10. TOOL HISTORYNot applicable.HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL GSE 008Page 1NOV 20/09Copyright © 2010 by <strong>EMB</strong>RAER - Empresa Brasileira de Aeronaútica S.A. All rights reserved.

GROUND HANDLING ANDSERVICING HANDBOOKHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.ANEMOMETRIC STATICPORTS 1 AND 3ATYPICALA21AANEMOMETRIC STATICPORTS 2 AND 4EM500ENGHSH000008A.DGNPlug-Protection, Static PortFigure 1EFFECTIVITY: ALL GSE 008Page 2NOV 20/09Copyright © 2010 by <strong>EMB</strong>RAER - Empresa Brasileira de Aeronaútica S.A. All rights reserved.

GROUND HANDLING ANDSERVICING HANDBOOKGSE NUMBER: 009ITEM NAME: PITOT COVERPURPOSE AND USE: Used to protect the pitot pressure ports.PART NUMBER: KPC3-480-325 (Figure 1)1. MANUFACTURERSESAME TECHNOLOGIES INC.2. TECHNICAL SPECIFICATIONSA. The cover is made of red KevlarB. It withstands temperatures of 427ºC (800ºF)3. BRIEF OPERATION DESCRIPTIONNot applicable.4. TOOL CONSISTS OFNot applicable.5. REPLACEMENT PARTS LISTNot applicable.6. QUANTITY27. DIMENSIONS AND WEIGHT115 x 12 mm (4.52 x 0.47 in); 0.1 kg (0.22 lb)8. SUPPORTING TOOLSNot applicable.9. GSE MAINTENANCEKeep the covers clean and protected against rain, sun, and dust.10. TOOL HISTORYNot applicable.HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL GSE 009Page 1NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.ABBAEM500ENGHSH000002A.DGNPitot CoverFigure 1EFFECTIVITY: ALL GSE 009Page 2NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKGSE NUMBER: 016ITEM NAME: UNIT, GROUND POWERPURPOSE AND USE: Used to supply electrical power on the ground for startingthe engines and servicing the electrical and avionics systems.PART NUMBER: 11A6647-1010 (Figure 1)1. MANUFACTURERTRONAIR2. TECHNICAL SPECIFICATIONSA. A solid state rectifier 28.5 V DC, nominal current 600 A, input voltage 200 to230 V AC 3-phase, 50/60 Hz and 56 A (power 20 Kva)B. Three-position current limit control with DC on/off switchC. Adjustable voltage control from 20 to 31 V DC located on the control panel(digital LED)D. DC ripple voltage (with filter)

8. SUPPORTING TOOLSNot applicable.9. GSE MAINTENANCEGROUND HANDLING ANDSERVICING HANDBOOKFor information on maintenance, refer to the vendor's documentation.10. TOOL HISTORYNot applicable.HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL GSE 016Page 2NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKAZONE195AHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EM500ENGHSH000014A.DGNGround Power UnitFigure 1EFFECTIVITY: ALL GSE 016Page 3/4NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKGSE NUMBER: 022ITEM NAME: FUEL SAMPLERPURPOSE AND USE: Used to take fuel samples for visual analysis.PART NUMBER: CCA-39680 (Figure 1)1. MANUFACTURERCurtis Superior Valve Company2. TECHNICAL SPECIFICATIONSA transparent plastic cup, provided with a stainless steel drain rod.3. BRIEF OPERATION DESCRIPTIONThe fuel drain valve is actuated by means of the steel rod of the drain cup. As thedrain valve poppet is pushed by the rod, fuel is allowed to flow into the plasticcup.4. TOOL CONSISTS OFNot applicable.5. REPLACEMENT PARTS LISTNot applicable.6. QUANTITY17. DIMENSIONS AND WEIGHT45 x 80 mm (1.8 x 3.1 in)8. SUPPORTING TOOLSNot applicable.9. GSE MAINTENANCENot applicable.10. TOOL HISTORYNot applicable.HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL GSE 022Page 1NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKAHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.AEM500ENGHSH000003A.DGNFuel SamplerFigure 1EFFECTIVITY: ALL GSE 022Page 2NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKGSE NUMBER: 023ITEM NAME: TOOL, DEFUELINGPURPOSE AND USE: Used to connect the aircraft dump valve to permit defuelingof the fuel tanks by gravity.PART NUMBER: 3V98-005 (Figure 1)1. MANUFACTURERINTERTECHNIQUE.2. TECHNICAL SPECIFICATIONSDevice made of aluminum, consisting of a tubular frame that couples to thedump valve.3. BRIEF OPERATION DESCRIPTIONNot applicable.4. TOOL CONSISTS OFNot applicable.5. REPLACEMENT PARTS LISTFor information on parts, refer to the vendor's documentation.6. QUANTITY17. DIMENSIONS AND WEIGHT89 x 48 x 48 mm (3.50 x 1.89 x 1.89 in); 0.0034 kg (0.075 lb)8. SUPPORTING TOOLSNot applicable.9. GSE MAINTENANCEFor information on maintenance, refer to the vendor's documentation.10. TOOL HISTORYNot applicable.HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL GSE 023Page 1NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKAHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.ZONES532632BABEM500ENGHSH000015A.DGNTool, DefuelingFigure 1EFFECTIVITY: ALL GSE 023Page 2NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKGSE NUMBER: 026ITEM NAME: TOWBAR HEADPURPOSE AND USE: Used to attach the towbar to the aircraft NLG for towing.PART NUMBER: 01-0601-0000 (Figure 1)1. MANUFACTURERTRONAIR2. TECHNICAL SPECIFICATIONSA. Features:- Torsional and tension/compression shear protection: a shear pin breaks incase of tension/compression overload.- Attachment safety: a safety bolt keeps the towbar head attached to the towbarso as to maintain aircraft control and avoid unintentional free movements.B. Specifications:- Tension/Compression Shear Load: 12,000 N (2,698 lb)- Torsional (radial) Shear Moment: 1,200 N.m (10,620 lb.in)3. BRIEF OPERATION DESCRIPTIONNot applicable.4. TOOL CONSISTS OFNot applicable.5. REPLACEMENT PARTS LISTFor information on parts, refer to the vendor's documentation.6. QUANTITY17. DIMENSIONS AND WEIGHT584 x 159 x 102 mm (23.00 x 6.25 x 4.00 in); 10.4 kg (23 lb)8. SUPPORTING TOOLSUsed in conjunction with GSE 027 - TOWBAR.9. GSE MAINTENANCEFor information on maintenance, refer to the vendor's documentation.10. TOOL HISTORYNot applicable.HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL GSE 026Page 1NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKBHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.AAGSE 027(REF.)BEM500ENGHSH000004A.DGNTowbar HeadFigure 1EFFECTIVITY: ALL GSE 026Page 2NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKGSE NUMBER: 027ITEM NAME: TOWBARPURPOSE AND USE: Used to tow, push, and steer the aircraft.PART NUMBER: 01-1202-0000 (Figure 1)1. MANUFACTURERTRONAIR2. TECHNICAL SPECIFICATIONSA. Capacity: 30,000 kg (66,000 lb)B. Main tube made of heavy duty aluminumC. Standard 2 3/16 in towing eyeNOTE: To substitute the towing eye for a 2 2/8 in. one, insert a letter "A" inplace of the first dash (third digit) of the part number.D. Characteristics:- Shock absorber to protect the NLG during towing operations.- Casters and handles for easier movement and attachment.- Pneumatic wheels to absorb towing speed shock.3. BRIEF OPERATION DESCRIPTIONNot applicable.4. TOOL CONSISTS OFNot applicable.5. REPLACEMENT PARTS LISTFor information on parts, refer to the vendor's documentation.6. QUANTITY17. DIMENSIONS AND WEIGHT3230 x 560 mm (127 x 22 in); 42 kg (92 lb)8. SUPPORTING TOOLSUsed in conjunction with GSE 026 - TOWBAR HEAD.9. GSE MAINTENANCEFor information on maintenance, refer to the vendor's documentation.10. TOOL HISTORYNot applicable.HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL GSE 027Page 1NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.AAGSE 026(REF.)EM500ENGHSH000005A.DGNTowbarFigure 1EFFECTIVITY: ALL GSE 027Page 2NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKGSE NUMBER: 029ITEM NAME: SET - TRANSPARENCY SHADE, COCKPITPURPOSE AND USE: Used to protect the cockpit equipment from solar radiation.PART NUMBER: AGE-04712-401 (Figure 1)1. MANUFACTURERSOUTHERN CROSS AVIATION LLC2. TECHNICAL SPECIFICATIONSA. The GSE consists of conveniently shaped pleated aluminum-lined cardboardsinstalled on the inside face of the cockpit windshield.B. An elastic band keeps the GSE collapsed for ease of stowage.3. BRIEF OPERATION DESCRIPTIONNot applicable.4. TOOL CONSISTS OFNot applicable.5. REPLACEMENT PARTS LISTITEM NAME P/N QUANTITY1 Sun Shade-lateral Prot, Cockpit AGE-04963-901 12 Sun Shade-lateral Prot, Cockpit AGE-04962-901 13 Sun Shade-lateral Prot, Cockpit AGE-04962-902 14 Sun Shade-lateral Prot, Cockpit AGE-04963-902 16. QUANTITY17. DIMENSIONS AND WEIGHTITEMS 1 and 4: 632 x 372 mm (24.8 x 14.6 in); 0.1 kg (0.22 lb)ITEMS 2 and 3: 726 x 649 mm (28.6 x 25.6 in); 0.2 kg (0.44 lb)8. SUPPORTING TOOLSNot applicable.9. GSE MAINTENANCEKeep the set clean and protected against rain, sun, and dust.10. TOOL HISTORYNot applicable.HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL GSE 029Page 1NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKAAHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.AEM500ENGHSH000006A.DGNSet-Transparency Shade CockpitFigure 1EFFECTIVITY: ALL GSE 029Page 2NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKGSE NUMBER: 030ITEM NAME: PLUGS, ENGINEPURPOSE AND USE: Used to protect the engine (air inlet/exhaust and starter generator air inlet/exhaust).PART NUMBER: AGE-04955-401 (Figure 1)1. MANUFACTURERSOUTHERN CROSS AVIATION LLC2. TECHNICAL SPECIFICATIONSA. All plugs are internally-stuck foam cushions (plug-type), covered with PVCimpregnatedpolyamide cloth.B. The engine air inlet, the starter generator air inlet and exhaust plugs are connectedto each other with stripes.3. BRIEF OPERATION DESCRIPTIONIt covers the engine air inlet/exhaust and the starter generator air inlet/exhaust toprevent unwanted material from entering the engine through them.4. TOOL CONSISTS OFNot applicable.5. REPLACEMENT PARTS LISTITEM NOMENCLATURE P/N QUANTITY1 Plug-Air Inlet, Engine AGE- 05108-901 12 Plug-Exhaust Outlet, Engine AGE- 05109-901 16. QUANTITY27. DIMENSIONS AND WEIGHTITEM 1: 433 x 45 x 433 mm (17 x 1.8 x 17 in); 0.5 kg (1.1 lb)ITEM 2: 350.5 x 22 x 350.5 mm (13.80 x 0.87 x 13.80 in); 0.2 (0.44 in)8. SUPPORTING TOOLSNot applicable.9. GSE MAINTENANCEKeep the plugs clean and protected against rain, sun, and dust.10. TOOL HISTORYNot applicable.HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.EFFECTIVITY: ALL GSE 030Page 1NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKAHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.ABBEM500ENGHSH000007A.DGNPlugs, EngineFigure 1EFFECTIVITY: ALL GSE 030Page 2NOV 20/09Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

GROUND HANDLING ANDSERVICING HANDBOOKCONSUMABLEPRODUCTSAPPENDIXHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.

Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.EFFECTIVITY: ALL CONSUMABLE PRODUCTS APPENDIXPage CON-1NOV 20/09PART NUMBER SPECIFICATION DESIGNATION SUPPLIERDiethyleneGlycol MonomethylEtherHoney BeeCleaner 60ASTM D4171AMS 1640Anti-Ice Fuel Aditive(DI-EGME)Disinfectant, Cleaner,Aircraft LavatorySystemSHELF LIFE(days)JET A ASTM D 1655 Jet Fuel Local Supplier 0JET A-1 ASTM D 1655 Jet Fuel Local Supplier 0JP-8 MIL-DTL-83133 Jet Fuel Local Supplier 0LEAK-TEC16-OXMIL-I-25017DANGER CLASSSTORAGECODE- - - -Local Supplier 720 Toxic Substance 12Non-DangerousMaterialNon-DangerousMaterialNon-DangerousMaterialMIL-PRF-25567 Leak Test SolutionAMERICAN GASAND CHEMICAL3600 Miscellaneous 99MIL-PRF-25567 Leak Test Solution PACAERO 3600 Miscellaneous 99MIL-PRF-25567 Leak Test SolutionCBOLCORPORATION3600 Miscellaneous 99MIL-PRF-25567 Leak Test SolutionTIERNAYAEROSPACE 3600 Miscellaneous 99SERVICESMIL-PRF-25567 Leak Test SolutionDAVID HSUTHERLAND3600 Miscellaneous 99MIL-PRF-25567 Leak Test SolutionFIRST WAVEAVIATION3600 Miscellaneous 99MIL-PRF-25567 Leak Test Solution AGS US 3600 Miscellaneous 99MIL-I-25017Corrosion Inhibitor/Lubricity Additive- - - -999999GROUND HANDLING ANDSERVICING HANDBOOKHARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.

HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.EFFECTIVITY: ALL CONSUMABLE PRODUCTS APPENDIXPage CON-2NOV 20/09PART NUMBER SPECIFICATION DESIGNATION SUPPLIERMIL-PRF-680Type IREMOVEGRAXMLS-12MIL-PRF-680TYPE IMEP 21-018MEP 21-018MEP 21-018MEP 21-018MEP 21-018MEP 21-018MEP 21-018SUPERSOL-10 MEP 21-015Cleaning CompoundSolventBiodegradableDetergentBiodegradableDetergentBiodegradableDetergentBiodegradableDetergentBiodegradableDetergentBiodegradableDetergentBiodegradableDetergentConcentrate LiquidDetergentLocal Supplier<strong>EMB</strong>RAEREMPRESA BRASILE-IRA DE AERON<strong>EMB</strong>RAERAIRCRAFTCUSTOMERSERVICES<strong>EMB</strong>RAERAVIATIONINTERNATIONALSAS<strong>EMB</strong>RAERAIRCRAFTCORPORATION<strong>EMB</strong>RAERAVIATIONINTERNATIONALSASCLARUSTECHNOLOGY DOBRASIL LTDAINTERTURBINELOGISTIK GMBHSHELF LIFE(months)Refer toManufacturer360360360360360360360- 720DANGER CLASSSTORAGECODEFlammable Liquid 2Non-DangerousMaterialNon-DangerousMaterialNon-DangerousMaterialNon-DangerousMaterialNon-DangerousMaterialNon-DangerousMaterialNon-DangerousMaterialCorrosiveMaterial444444408GROUND HANDLING ANDSERVICING HANDBOOK

logo

products

Resources

Company

Terms of service
Privacy policy
Cookie policy
Cookie settings
Imprint
Change language
Made with love in Switzerland
© 2024 Yumpu.com all rights reserved

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!