October - Cessna

DIRECTC I T A T I O N 

approach 

OCT 2011 

IN THIS ISSUE: 

A New Spin on NLG Wheel Removal/Installation Process 

Tailor Your Flight Manual with Configuration Codes 

Citation 500-Series Brakes Explained 

Conferences, Updates and more

in THIS 

Issue: 

1 

new & IMPROVED 

A NEW SPIN ON NLG WHEEL REMOVAL/INSTAL- 

LATION PROCESS (560XL) 

2 

TAILOR YOUR FLIGHT MANUAL WITH CONFIGURA- 

TION CODES (ALL MODELS) 

8-11 

SYNOPSIS OF SERVICE BULLETINS AND 

SERVICE LETTERS (ALL MODELS) 

12 

CESSNASUPPORT.COM WEBSITE GETS MORE 

PERSONALIZED (ALL MODELS) 

15 

CHILD SAFETY SEATS(s) AVAILABLE FOR 

YOUNG PASSENGERS (ALL MODELS) 

6 

TEST HARNESS INFO FOR CABIN PRESS TEST 

(525B) 

7 

SWITCH OFF ROSEN MONITORS BEFORE 

PLUGGING IN (525A, 525B, 560 and 560XL) 

13 

CITATION 500-SERIES BRAKES EXPLAINED 

(500, 510, 525, 525A, 525B, 525C, 550, S550, 

560 and 560XL) 

15 

technical INFO 

SAIB COVERS SEMI-SYNTHETIC JET 

FUEL FOR CITATIONS (ALL MODELS) 

16 

17 

in every ISSUE 

ASK THE EXPERT 

EVENTS CALENDAR 

THE DIRECT APPROACH IS PUBLISHED 

MONTHLY BY THE CESSNA CITATION CUSTOMER 

SERVICE ORGANIZATION. COMMENTS AND 

SUGGESTIONS ARE WELCOMED. 

PLEASE ADDRESS YOUR COMMENTS TO LOUIS BROWN 

316-517-3501 lhbrown@cessna.textron.com

560XL, ATA: 32-20 

A New Spin on NLG Wheel 

Removal/Installation Procedures 

Cessna has developed improved removal/installation procedures for the nose landing gear wheel (NLG) in Revision 

31 of the Model 560XL Maintenance Manual. The revision is expected to be released in a few weeks. 

Operators are provided new instructions to clean, inspect and disposition the serviceability of components that are 

accessible during a NLG wheel and tire removal. 

Operators should be aware that the maintenance manual revision also has changed the NLG wheel and tire installation 

procedures. Special attention to recommended lubrication requirements, updated torque values utilized, and 

installation of a new axle bolt is required with the new procedures. 

Questions, please contact: 

Team Excel 

316-517-1400 (Direct) 

1-877-560-3960 (WATS) 

teamxl@cessna.textron.com 

It’s time to stop thinking about a glass flight deck... 

...And start flying with one. 

G1000 is bright, precise, and reliable. It puts a wealth of 

flight-critical data at your crew’s fingertips. But, perhaps the 

greatest thing about the G1000 is it’s a perfect fit for your Citation. 

THE FUTURE OF AVIONICS, READY FOR YOU TODAY. 

To learn more, call 

877-G-1000-4-U (877-410-0048) 

to schedule your G1000 retrofit today. 

page 1 

www.citationservice.com

All Models, ATA: 99-00 

Tailor Your Flight Manual with 

Configuration Codes 

Some pages in your Airplane Flight Manual (AFM) may not be applicable to your aircraft. When Cessna issues 

revisions and temporary changes to the AFM, it may become unwieldy if pages are added that are not applicable 

to the airplane serial effectivity or configuration. Each of the pages in the AFM has a configuration code printed 

at the bottom center of the page with two letters such as “AB.” These codes and their definitions correspond to 

the aircraft serial range and/or configuration listed in Section I of the AFM. 

For some operators the process of identifying which configuration codes are applicable to their aircraft can appear 

to be challenging. To help operators with this issue, Cessna Publications began providing Microsoft Excel 

spreadsheets of Configuration Code Calculators some time ago. An operator can simply enter their aircraft serial 

number and view all service documents complying with the airplane, including options available. 

A current report from CAMP will list the service documents options and current avionics to properly configure 

the AFM. The operator can then determine which codes apply to the aircraft; adding applicable AFM pages, and 

removing irrelevant ones as the final process. 

Note: It is important not to discard the removed pages as they may be later required if a service document is 

complied with. 

The AFM Configuration Code Calculators are available on CessnaSupport.com. Operators must first log into the 

Customer Access page followed by selecting the Technical Publications tab at the top of the screen. The AFM 

Configuration Code Calculator link can then be selected afterwards. 

Cessna recently released calculators for the following manuals: 

525CFM Rev 03 

525FMB (CJ1+) Rev 2 

55FMA (Citation II 0550 thru 0626) Rev 02 

55FMB (Citation II 0627 and on) Rev 05 

56FMA (Ultra) Rev 13 

56FMC (Encore+) Rev 01 

65C7FM (Citation VII) Rev 10 

65C6FM (Citation VI) Rev 04 

680FM Rev 10 

75FM (Citation X Pre-BPC) Rev 11 

These spreadsheets are an addition to the calculators already posted on our website. We will continue to develop 

new calculators until all models are covered, and revise the existing postings as new revisions to the AFMs are 

released. 

Questions, please contact; 

Pilot Services 

316-517-7717 

page 2

page 3 


page 4

page 5 


525B, ATA: 21-30 

CJ3 operators performing cabin pressurization tests have a new tool available to simplify aircraft 

pressurization procedures during ground maintenance or tests. The Ground Pressurization Harness P/N 

6388016-1 can be installed between the pressurization controller and the existing aircraft wiring. With the 

harness installed, the DIVE and CLIMB signals from the controller and primary outflow valve are reversed— 

making it possible to command the outflow valves to close by using the cabin dump switch. 

Note: Instructions for using the Ground Pressurization Harness exist in the Chapter 21, Pressurization Control- 

Adjustment/Test procedures of the Model 525B Maintenance Manual. 

The new wire harness can be manufactured locally however, when Revision 14 of the maintenance manual 

was released, the fabrication instructions for the harness were not included. A change request has been 

submitted and the harness fabrication procedures are currently in development. 

Until the next maintenance manual revision is released, operators who wish to have the new harness have 

two options: 

• Team CJ can be contacted for information to create the harness 

• The order desk at Cessna Service Parts and Programs (CSP&P) can be contacted to purchase the 

P/N 6388016-1 Ground Pressurization Harness 

The order desk can be contacted at: 

316-517-7602 (Local) 

866-206-4158 (WATS) 

316-517-5606 (International) 

316-517-7711 (FAX) 

cpdretail@cessna.textron.com 

Test Harness Info for Cabin Press 

Leak Test 

Note: CSP&P will need time to build the harness so it is highly encouraged to submit the order with adequate 

scheduling before the tool would be needed. 


Team CJ 

1-800-835-4090 

hotline@cessna.textron.com 

page 6

525A, 525B, 560 and 560XL, ATA: 25-20 

Switch Off Rosen Monitors 

before Plugging In 

Operators of Citations equipped with older Rosen P/N 5601-111 Side ledge Monitors should be aware the 

ON/OFF switch of the monitors should be in the OFF position before plugging into the side ledge monitor 

receptacle(s). 

Failure to place the monitor switch in the OFF position can cause an unwanted voltage spike, potentially 

damaging other components within the electrical circuit. 

Citation Customer Services has received reports of Rosen monitors causing damage to Mid-Continent P/N 

103006-1 Video Distribution Amplifiers. 


Team CJ 

1-800-835-4090 


Or: 

Team Legacy 

1-800-835-4090 


Or: 

Team Excel 

316-517-1400 (Direct) 

1-877-560-3960 (WATS) 


page 7 


Synopsis of Service Bulletins and Service Letters Released 

Released September 2011 

Note: There were no Service Bulletins or Letters for Model 500 released in September 2011. 

Note: There were no Service Bulletins for the Model 510 released in September 2011. 

Note: There were no Service Bulletins for the Models 525, 525A, 525B and 525C released in September 2011. 


Note: There were no Service Bulletins or Letters for the Model S550 released in September 2011. 

Note: There were no Service Bulletins for the Model 560XL released in September 2011. 




---------------------------------------------------510------------------------------------------------ 

Number: SL510-11-02 

Type: Recommended 

Title: Power J-Box Placard Inspection 

Effectivity: 510-0033, -0043, -0054, -0065, -0094, -0100, -0116, -0117, -0134, 

-0195, -0214, -0246, -0268, -0269, -0294, -0300, -0312, -0319, -0326, -0339, -0343, -0347, and -0358 

Description: A potential exists that placards installed in the aft J-box may have incorrect information regarding 

the HF FUSE LIMITER (option). This recommended service letter provides instructions to inspect and replace 

the placards if necessary. This letter should be accomplished at a scheduled maintenance period or inspection. 


Type: Mandatory 

Title: Transmittal of Intertechnique Service Bulletin MXH-35-240 

Effectivity: 510-0001 thru -0376 

Description: A latent potential exists for the inflatable harness on the crew oxygen mask(s) to rupture when 

inflated. This mandatory service letter transmits the Intertechnique service bulletin instructions to inspect and 

replace the inflatable harness of the oxygen mask(s). This letter must be accomplished within 1,200 flight hours 

or by May 31, 2013, whichever occurs first. 

Number: SL510-55-02-R2 


Title: Horizontal Stabilizer Sealant Inspection 


Description: Water can enter the vertical and horizontal stabilizers and freeze making the elevator trim difficult 

to adjust. This mandatory service bulletin provides instructions to inspect areas around the tail for missing sealant. 

Revision 2 revises the serial effectivity section to include all serial numbers from 510-0001 thru -0372, but 

does not affect airplanes that have previously complied with the service bulletin. 

---------------------------------------------------525------------------------------------------------ 



Title: Transmittal of L-3 Communications Alert Bulletin No. Cessna SB 001 

Effectivity: 525-0482, -0485, -0490, -0497, -0502, -0504, -0508, -0511, -0514, 

-0515, -0518, -0520 thru -0522, -0529, -0531, -0538, -0539, -0546 thru -0548, 

-0551, -0552, -0554, -0555, -0557, -0558, -0600 thru -0602, -0604, -0606, -0607, 

-0615 thru -0619, -0621 thru -0623, -0626, -0627, -0629 thru -0631, -0638, -0640 thru -0699 

Description: L-3 Communications has issued an alert bulletin requiring an inspection of four hardware nuts on 

the Crash Survivable Memory Unit that are suspected to be manufactured of non-conforming material. A suspect 

range of serial numbers is included with the bulletin. This mandatory service letter transmits the L-3 bulletin 

page 8 

PLEASE SEE NEXT PAGE

All Models Except Mustang, ATA: 56-00 

instructions, and must be accomplished within 500 flight hours or 12 months from the date of receipt, whichever 

occurs first. 

---------------------------------------------------525A--------------------------------------------- 

Number: SL525A-31-05 



Effectivity: 525A-0056, -0058, -0059, -0061, -0062, -0065, -0078, -0081, -0084, 

-0086, -0092, -0094, -0096, -0105, -0109, -0110, -0114, -0117, -0118, -0120, -0127, 

-0129, -0132, -0135 thru -0137, -0139 thru -0141, -0145, -0147, -0149, -0152, 

-0154, -0155, -0157, -0158, -0163, -0164, -0171, -0172, -0180 thru -0182, -0184, 

-0190, -0191, -0198, -0203, -0207, -0209, -0211, -0213, -0215, -0222, -0225, -0227, -0228, -0235, -0237, -0238, 

-0241, -0243, -0244, -0300, -0301, -0303, -0306, -0310, -0314 thru -0316, -0319 thru -0321, -0324, -0325, -0327, 

-0333, -0337 thru -0339, 

-0341, -0342, -0344, -0346, -0348 thru -0377 





occurs first. 

Number: SL525A-35-02 



Effectivity: 525A-0001 thru -0427 





---------------------------------------------------525B--------------------------------------------- 

Number: SL525B-31-03 



Effectivity: 525B-0006, -0008, -0010, -0012, -0014, -0018, -0019, -0022, -0023, 

-0027 thru -0039, -0041, -0043 thru -0045, -0047, -0048, -0050 thru -0052, -0055, 

-0059, -0061, -0062, -0065, -0066 thru -0075, -0077, -0081 thru -0355 





occurs first. 

Number: SL525B-35-02 



Effectivity: 525B-0001 thru -0388 





page 9 


---------------------------------------------------525C--------------------------------------------- 

Number: SL525C-31-01 



Effectivity: 525C-0001 thru -0022 and -0029 

Description: L-3 Communications has issued an alert bulletin requiring an inspection of four hardware nuts on the 

Crash Survivable Memory Unit that are suspected to be manufactured of non-conforming material. A suspect range 

of serial numbers is included with the bulletin. This mandatory service letter transmits the L-3 bulletin instructions, 

and must be accomplished within 500 flight hours or 12 months from the date of receipt, whichever occurs first. 

---------------------------------------------------550----------------------------------------------- 





Description: A latent potential exists for the inflatable harness on the crew oxygen mask(s) to rupture when inflated. 

This mandatory service letter transmits the Intertechnique service bulletin instructions to inspect and replace 

the inflatable harness of the oxygen mask(s). This letter must be accomplished within 1,200 flight hours or by May 

31, 2013, whichever occurs first. 

--------------------------------------------------S550---------------------------------------------- 

Number: SB560-34-150-R3 Type: Recommended 

Title: Collins FMS-3000 Software Upgrade 


Description: An option is available to enable WAAS capability. This recommended service bulletin provides parts 

and instructions to replace existing the equipment modify the wire harnesses for a Collins FMS-3000 Software Upgrade. 

Revision 3 makes some changes to the accomplishment instructions, but does not affect airplanes that have 

previously complied with the service bulletin. 

-------------------------------------------------------------------------------------------------------- 









-------------------------------------------------560XL---------------------------------------------- 

Number: SL560XL-35-04 



Effectivity: 560XL-5002 thru -5830, -6002 thru -6080, -6083 thru -6085 





page 10 


Number: SL560XL-53-16 


Title: Fastener Inspection/Installation 

Effectivity: 560XL-6059 thru -6063, -6065, -6066, -6069 thru -6071, -6073 thru 

-6077 

Description: The right frame and outer frames of the right lower skin bond assembly in the cockpit may be 

missing some fasteners. This mandatory service letter provides instruction to inspect and correct the missing 

fasteners if discovered. This letter must be accomplished within 500 flight hours or 12 months from the date of 

receipt, whichever occurs first. 

---------------------------------------------------650------------------------------------------------ 









---------------------------------------------------680------------------------------------------------ 




Effectivity: 680-0001 thru -0289, -0291 thru -0306, -0308, -0309, -0311, -0312, and -0314 





---------------------------------------------------750------------------------------------------------ 




Effectivity: 750-0001 thru -0306, and -0308 





page 11 



CessnaSupport.com Website 

Gets More Personalized 

Cessna is pleased to announce new enhancements to CessnaSupport.com making the website more personalized 

and user-friendly. Web browsers will notice a new My Information box in the upper left corner of the homepage. 

The new addition offers a My Aircraft Info link that directly ties the customer to their subscription information, serialized 

service document search listing, serialized flight documents and current contact information. Social Media 

buttons are also provided for Cessna’s Twitter, Facebook, and YouTube sites. 

With the My Subscriptions box, owner/operators will not be “out-of-sync’ with their current subscription(s) and a 

link for information is provided to keep customers savvy as what additional subscriptions are available. 

For the serialized documents, owner/operators can instantly access the Flight Manual Temporary Changes or Supplements, 

Emergency and Normal Procedures Checklists. This function also includes a serialized service documents 

search report applicable to your specific aircraft. 

For the My Contact Information box, owners/operators can make sure personal contact information is an accurate 

source for Cessna to make contact for any issues related to their aircraft. 

Operators of legacy and production Citations and Propeller aircraft alike will benefit from the Aircraft Publications 

page, which provides a search engine for all service bulletins and letters including service kits and Instructions for 

Continued Airworthiness (ICA) documents. 


Cessna Customer Care 

316-517-5800 

Customercare@cessna.textron.com 

page 12

500, 510, 525, 525A, 525B, 525C, 550, S550, 560 and 560XL ATA: 32-40 

Citation 500-Series Brakes Explained 

Since the initial production of the Citation 500-series family of airplanes, the braking systems have changed 

from model to model. For the benefit of Citation operators, the information provided below describes some of the 

operational differences for maintenance and flight crew “feel” of the braking systems. 

Models 500/501 (Citation I), 525 (CitationJet, CJ1 and CJ1+), 550/551 (Citation II and Citation II Classic), S550 

(Citation SII), and 560 (Citation V and Ultra) 

• Pilot builds pressure to the antiskid servo valve by pressing the brake pedals and activating the hydraulic 

master cylinders 

• The antiskid servo valve has two shuttle valves that allow hydraulic fluid to bypass through the servo valve 

to the brakes without electrical power 

• If there is no electrical power to the brake system, the hydraulic braking pressure can still be increased 

by pumping the pedals 

Models 550 (Bravo) and 560XL (Excel) 

• Pilot builds pressure to the antiskid servo valve by pressing the brake pedals and activating the hydraulic 

master cylinders 

• The antiskid servo valve does not have shuttle valves and, as a result, there are two hydraulic circuits 

separated by the antiskid servo valve 

• Because the antiskid servo valve is electrically controlled there is no braking ability without electrical 

power 

Models 510 (Mustang), 525A (CJ2 and CJ2+), 525B (CJ3), 525C (CJ4), 560 (Encore and Encore+), and 560XL (XLS 

and XLS+) 

• The brake pedals are spring-loaded with constant “feel” of pressure, however movement of the pedals 

does not build any hydraulic braking system pressure 

• There are no master cylinders with the brake pedals and the brake metering/antiskid servo valve is con 

nected by cables 

• There is only one hydraulic circuit 

• Because the brake metering/antiskid servo valve is electrically controlled there is no braking ability with 

out electrical power 

Caution: In the rare event of brake system failure, operators must immediately use the emergency braking system 

to stop the airplane in all Citation models. 


Team Legacy 

1-800-835-4090 


Or: 

Team Mustang 

316-517-5490 (Direct) 

1-877-832-6510 (WATS) 

teammustang@cessna.textron.com 

page 13 

Team CJ 

1-800-835-4090 


Or: 

Team Excel 

316-517-1400 (Direct) 

1-877-560-3960 (WATS) 



THE CITATION EXPERIENCE 

Your Citation is more than just a fair-weather friend. 

Show us the four seasons of Citation. 

Send your photos of winter, spring, summer, and fall to 

the Citation Experience. 

Citation is an aircraft for all seasons. We’re asking you to prove it by showing us 

your Citation in each of the four seasons. 

From budding tulips to tropical summer beaches to autumn foliage to winter 

wonderlands, we want to see how you enjoy your Citation all year long. 

Send your photos to http://www.citationexperience.com. And share a year in the 

life of your Citation for all the world to see. 

Questions? Comments? Scheduling? 

Call 877-360-EXPERIENCE (877-360-3973) 

International: 316-517-5800 

page 14


SAIB Covers Semi-Synthetic Jet 

Fuel for Citations 

The FAA issued a Special Airworthiness Information Bulletin (SAIB) NE-11-56 to inform operators that jet fuel 

blended with synthetic components meeting ASTM International Standard D7566 is acceptable for use on aircraft 

certified for operation with D1655 fuel identified as Jet A or Jet A-1 

The SAIB says the FAA relies on American Society for Testing and Materials (ASTM) to develop fuel specifications 

that applicants can designate as operating limitations for approved products. 

The FAA document recommends that the operating limitations in Aircraft Flight Manuals, Pilot Operating Instructions, 

or Type Certificate Data Sheets that specify ASTM D1655 Jet A or Jet A-1 fuel are acceptable for use with 

these fuels. 

All Citation aircraft have been approved for use of Jet A and/or Jet A-1 and therefore operators can use semi-synthetic 

jet fuels. Operators can refer to the existing FUEL LIMITS or FUEL LIMITATIONS of the OPERATING LIMITA- 

TIONS procedures in Section II of the applicable AFM. 


Customer Service Hot Line 

1-800-835-4090 

316-517-6261 (International) 



Child Safety Seat(s) Available 

for Young Passengers 

Citation Customer Service occasionally receives inquiries regarding availability of child safety seats for aircraft 

use. Cessna Service Parts & Programs (CSP&P) offers CRS-2000 PlaneSeat products manufactured by Astronics. 

The certified child safety seat system folds for easy storage, features a five-point quick release harness, and is built 

to comfortably seat infants up to 20 pounds, and toddlers up to 40 pounds or 40 inches in height. 

Operators can refer to the CessnaSupport.com website at: 

http://www.cessna.com/customer-service/parts-programs/crs2000-planeseat.html 

page 15 


ask THE EXPERTS 

EXPERTS FROM THE CESSNA SUPPORT TEAM 

SHARE ADVICE AND SHED LIGHT 

ANSWERS 

Question 

Answer 

On a Primus 1000 equipped Citation aircraft, the pilots or copilots air data information (airspeed, 

altitude, vertical speed) are red X’d. The Air Data Computers were swapped but the condition remained 

on the original side. What could be the cause? 

One possible cause for this condition could be the PFD bezel controller on the side which is experiencing 

the failure. If the tach-generator of the baro set knob fails, the air data computer has 

no baro reference, and will red X the air data information on that PFD. Try swapping the bezel 

controllers to see if the condition follows. Another possible cause could be that one of the “Unit 

ID Straps” is not connected due to a broken wire or loose ground block connection. Refer to the 

Aircraft Avionics Wiring Diagram to determine the pin outs for the Unit ID and SDI wires, and 

verify they are properly grounded. The ADC’s use this strapping to tell them which side they are 

on, and report their data to the Display System. Without it, the system sees the data from the unit 

as invalid and will display the red X’s. 

How To 

submit comments and 

ask THE EXPERTS 

THE DIRECT APPROACH IS PUBLISHED MONTHLY BY THE 

CESSNA CITATION CUSTOMER SERVICE ORGANIZATION. 

ASK THE EXPERTS AT: 

asktheexpert@cessna.textron.com 

Our experts will do their best to provide answers to your questions. 

Even if your question is not posted in the publication, you will 

receive an e-mailed answer. 

page 16

WWW.FLIGHTSAFETY.COM 

CONTACT US AT: 

800-491-9796 

OR 316-220-3520 

4TH QUARTER - 2011 

Citation X (750) Initial 

Citation Sovereign (680) Avionics 

Citation III/VI/VII (650) OMP 

Citation XL/XLS/XLS+ (560) Initial 

Citation XL/XLS/XLS+ (560) Adv. T/S 

Citation Bravo/Encore/Encore+ (550/560) 

Citation I/II/SII/Bravo (500/550) Update 

Citation I/II/SII/Bravo (500/550) OMP 

Citation Mustang (510) Initial 

CitationJet 4 (525C) Initial 

CitationJet 4 (525C) MX Adv. 

CitationJet 3 (525B) MX Adv. 

CitationJet 3 (525B) Alt. T/S 

CitationJet (525/525A) Alt. T/S 

MAINTENANCE TRAINING 

Oct 24 - Nov 11 

Oct 27 - Nov 4 

Oct 10 - 14 

Oct 24 - Nov 10 

Oct 10 - 14 


Oct 17 - 21 

Oct 10 - 14 

Oct 17 - 27 


Oct 31 - Nov 11 

Oct 10 - 21 


Oct 24 - 28 

events CALENDAR 

HERE’S EVERYTHING YOU SHOULD BE 

IN THE KNOW ABOUT! 

NBAA Convention - Las Vegas, NV 

Oct 10 - 12, 2011 

CJP Owners Convention - Amelia Island, FL 

Oct 26 - 29, 2011 

Dubai Airshow - Dubai, UAE 

Nov 13 - 17, 2011 

WORLD’S LEADING AVIATION TRAINING COMPANY 

NBAA M&O Sessions 

Although Cessna will not be presenting 

M&O sessions at this year’s NBAA, we 

will still have Customer Service personnel 

available in Las Vegas to discuss any technical 

or support issues. 

Additionally, we will present webinars in 

the last quarter of 2011 to keep operators 

informed of current field programs. We 

regret that Citation Customer Service will 

not present M&O sessions at the upcoming 

NBAA Annual Convention. However, 

we feel that time and money required to 

support these sessions can be better used 

in the support of programs that help the 

greatest number of customers. 

THANKS for taking time to read our publication! We appreciate your readership 

and will do our best to continue to present you with the latest Citation related 

news, products & happenings throughout the year. 

page 17 


CESSNA CONNECTS YOU 

TO THE WORLD OF BUSINESS... 

even when you’re 

flying high above it. 

Maybe the only business tool that moves faster than your Citation is the web. 

So don’t let lift off kick you off line. A High-Speed Internet retrofit from your 

Citation Service Center keeps you connected via your laptop, Smartphone, 

iPad, or whatever you’re using - quickly and easily. 

Keep your business lifeline up and running. 

Call 877-941-DATA 

(877-941-3282) 

to learn more about High-Speed Internet.

October - Cessna

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