SERVICE BULLETIN. Citation CIB TITLE FUEL - FIREWALL SHUTOFF VALVE GROUND IMPROVEMENT

Similar documents
SERVICE BULLETIN. EFFECTIVITY SERIAL NUMBERS 680 (Citation Sovereign) thru (Citation Sovereign+) thru -0549

SERVICE BULLETIN REVISION TRANSMITTAL

SERVICE BULLETIN REVISION TRANSMITTAL

SERVICE BULLETIN. This service bulletin provides parts and instructions to install fuel caps that have a locking feature.

SERVICE BULLETIN SERIAL NUMBERS. The equivalent of this service bulletin has been incorporated on production airplanes and On.

SERVICE BULLETIN REVISION

SERVICE BULLETIN. COMPLIANCE MANDATORY. This service bulletin must be accomplished at the next 100-hour or 12-month (annual-type) inspection.

SERVICE BULLETIN. To prevent the wing fuel boost pump wiring from chafing on the wing structure and/or fuel tube assemblies.

SERVICE BULLETIN CERTIFICATION REQUIREMENTS - FOREIGN CERTIFICATION PLACARD INSTALLATION

SERVICE LETTER REVISION TRANSMITTAL

SERVICE BULLETIN SB

SERVICE LETTER. Single Engine SEL TITLE LANDING GEAR - DRAG LINK REPLACEMENT

SERVICE BULLETIN. The equivalent of this service bulletin has been incorporated on production airplanes and On.

SERVICE LETTER REVISION TRANSMITTAL

SERVICE BULLETIN REVISION

SERVICE BULLETIN SB

SERVICE BULLETIN SB

SERVICE BULLETIN. To prevent the wing fuel boost pump wiring from chafing on the wing structure and/or fuel tube assemblies.

SERVICE LETTER. Multi-engine TITLE NACELLES/PYLONS - NACELLE FITTING INSPECTION EFFECTIVITY

SERVICE BULLETIN REVISION TRANSMITTAL

ALERT SERVICE LETTER

SERVICE LETTER. COMPLIANCE DISCRETIONARY. This service letter should be accomplished at a scheduled Check 1, Check 2, or HSI. LABOR HOURS KEY WORD

SERVICE BULLETIN REVISION TRANSMITTAL

FAA approval has been obtained on technical data in this publication that affects airplane type design.

SERVICE BULLETIN. Citation SB TITLE DOORS - WIDE DOOR INSTALLATION MODIFICATION

It has been determined that some airplanes may have a hose plug installed in the inflatable belt assembly hose end.

SERVICE BULLETIN REVISION TRANSMITTAL

SERVICE LETTER SERIAL NUMBERS. 550/ thru -0505, thru -0733, thru -0969

SERVICE LETTER. SERIAL NUMBERS 210 & T thru P thru P

SERVICE BULLETIN. The equivalent of this service bulletin has been incorporated on production airplanes and On. REASON

SERVICE LETTER TITLE EXHAUST - TRANSMITTAL OF LYCOMING SERVICE BULLETIN NO 627C, EXHAUST SYSTEM INSPECTION SERIAL NUMBERS

Single Engine. Service Bulletin TITLE ELEVATOR TRIM TAB ACTUATOR ASSEMBLY INSPECTION EFFECTIVITY. Group A airplanes: Serial Numbers

SERVICE BULLETIN REVISION

Affected , RX, , and RX alternators in Service Station stock should be returned to Cessna.

Service Information Letter

SUBJECT: Single Engine Service Bulletin SB Revision 1: Cosmetic Window Repair

SERVICE BULLETIN MANDATORY. SB , Rev Planning Information

DESCRIPTION This service document provides instructions to inspect the Pre-2014 LH yokes.

ATTACHMENT. Orders for the required parts listed below must be placed by using this form only. Service Station/Company Code: Company Name:

Single Engine MODIFICATION KIT

This Service Bulletin is applicable only to airplanes equipped with placards that are written in English.

SERVICE BULLETIN TITLE ENGINE CONTROLS - FULL AUTHORITY DIGITAL ENGINE CONTROL (FADEC) SOFTWARE UPGRADE VERSION C10

SERVICE LETTER. REASON To incorporate new software changes to the engine electronic control and engine diagnostics unit.

Please replace any copy of SEB07-2 with the attached copy of SEB07-2 Revision 1 which is printed in its entirety.

SERVICE LETTER. Multi-engine MEL TITLE NACELLES/PYLONS - ENGINE BEAM INSPECTION

Single Engine. Service Bulletin TITLE ENGINE MOUNT BRACKET INSPECTION

The parts that follow are available from Cessna Parts Distribution through an appropriate Cessna Service Station.

Revision Transmittal Sheet

ATTACHMENT DAMAGE REPORT FORM. Page: 1 of Pages Includes this cover sheet Date: (month/day/year) This form is for the: Left Wing: Right Wing: Other:

PROPELLERS - PROPELLER SLIP RING MOUNTING PLATE INSPECTION AND REPAIR

SERVICE BULLETIN. NO.: 0713 Revision C. All Garmin Aviation Service Centers and Aircraft OEM Service Centers DATE: 29 May 2007

EFFECTIVITY Serial Numbers thru , 698

SERVICE BULLETIN TITLE AIR CONDITIONING - R134A AIR CONDITIONER SYSTEM INSTALLATION FOR AIRPLANES EQUIPPED WITH G1000 AND 867 SHP ENGINE

ALERT SERVICE LETTER ASL

Alert Service Bulletin

September 8, Cessna Distributors, Authorized Service Facilities, CPC's, CSTARS, ASR's, and affected Owners of Record

Cessna Distributors and Single Engine Authorized Service Facilities and CPC's

NOTE: SB is a WAAS only supported build. If the autopilot is not WAAS equipped, the unlock card cannot be used at this time.

Single Engine. Service Bulletin TITLE PILOT AND COPILOT SECONDARY SEAT STOP INSTALLATION

201F Fuel Pump Valve Housing Cap Screw Replacement

SERVICE LETTER. Hartzell Alert Service Bulletin No. 069, 200F, 201F, 202F Fuel Pump Leak Inspection And Diaphragm

FORM: 2391 DRAWING NO: ICA-680A Cessna Aircraft Company P.O Box 7704 WICHITA, KS 67277

SERVICE BULLETIN. 560XL (Citation XLS+) thru -6055, thru -6066, thru -6071, thru -6077

FAA approval has been obtained on technical data in this publication that affects airplane type design.

AVIAT AIRCRAFT INC. P.O. Box South Washington Afton, WY USA Fax:

AVIAT AIRCRAFT INC. P.O. Box South Washington Afton, WY USA Fax:

TEMPORARY REVISION NUMBER

The engine cowling installation and firewall should be inspected and modified as specified in this Service Bulletin.

FOR THE MOST RECENT REVISION LEVEL OF THIS SERVICE BULLETIN.

Table 1: Alternator Models ES (CMI ), ALX-9524 (CMI ), ALX-9524R, & ALV-9610 Affected Serial Numbers

SERVICE BULLETIN FLIGHT CONTROLS - INSTALL FLAP INSPECTION ACCESS PANELS ON CERTAIN AERO CENTER PRODUCTS

TEMPORARY REVISION NUMBER

CIRRUS SR2X SB 2X Service Bulletin. Issued: February 27, SNS SUBJECT: TEMPERATURE CONTROL - Cabin Air Coupler Actuator Rigging

Cessna Aircraft Company: Amendment ; Docket No. FAA ; Directorate Identifier 2012-NM-020-AD.

MODIFICATION KIT. Serial Numbers 300 (LC40-550FG) thru (LC42-550FG) thru (LC41-550FG) thru

201F Fuel Pump Shaft Seal Leak

ALERT SERVICE BULLETIN NO.

CIRRUS SR2X SB 2X R2. Service Bulletin. Issued: Revised: June 26, 2012 July 31, 2012

Revision Transmittal Sheet

TEMPORARY REVISION NUMBER

*MANDATORY SERVICE BULLETIN*

MANDATORY SERVICE BULLETIN

Service Bulletin. ATA 27-00: Flight Controls Rudder-Aileron Interconnect Modification

Service Bulletin No: Ref No: 49 Modification No: EC ATA Chapter: 32

ROTORCRAFT FLIGHT MANUAL TEMPORARY REVISION FOR 4 AXIS AUTOPILOT OPERATIONS, INTRODUCTION OF.

Service Bulletin No.: D42L Rev 2 Date Issued: 05 October 2012 Title: ADF System Improvements Page: 1 of 16

POWER TURBINE RPM (N2) STEADY STATE OPERATION AVOIDANCE, INTRODUCTION OF.

41001 thru incorporating a retrofitted LA nose strut,

201F Fuel Pump Valve Assembly Leakage

SUBJECT: ELECTRICAL POWER SYSTEM UNIT AND ROTORCRAFT FLIGHT MANUAL TEMPORARY REVISION, CANCELLATION OF

Service Bulletin No: Ref No: 165 Modification No: EC ATA Chapter: 21

ALERT SERVICE BULLETIN PSL September 2015 Revision A, 6 October 2017

S E R V I C E B U L L E T I N

Service Bulletin. Service Bulletin No. 064 Alternator Model ALV-9610 Series Through Bolt Inspection for Proper Torque

Service Bulletin No: Ref No: 331 Modification No: EC , EC ATA Chapter: 27

SUBJECT: MAIN ROTOR DRIVE, ENGINE-TO- TRANSMISSION DRIVE SHAFT RETAINING NUTS INSPECTION/REPLACEMENT

SUBJECT: FUEL FITTING P/N AND , VERIFICATION OF.

PILATUS AIRCRAFT LTD. CH-6371 STANS, SWITZERLAND SERVICE BULLETIN SERVICE BULLETIN NO: REF NO: 184 MODIFICATION NO: ATA CHAPTER: 32

SNS SUBJECT: NOSE GEAR - Nose Landing Gear Assembly Inspection and Reinforcement

Part A Describes the procedure for the replacement of the Mitchell type tachometer. These parts are supplied in Kit A as described below.

Transcription:

TITLE FUEL - FIREWALL SHUTOFF VALVE GROUND IMPROVEMENT EFFECTIVITY MODEL SERIAL NUMBERS 525 (CJ1+) -0680, -0685 thru -0799 525A (CJ2+) -0417, -0439 thru -0524 525B (CJ3) -0263, -0294 thru -0414 REASON There is a ground wire missing for the right firewall shutoff valve relay. DESCRIPTION This service bulletin provides parts and instructions to add a ground wire to the right firewall shutoff valve relay. COMPLIANCE RECOMMENDED. This service bulletin should be accomplished at a scheduled maintenance period or inspection. A service bulletin published by Cessna Aircraft Company may be recorded as "completed" in an aircraft log only when the following requirements are satisfied: 1) The mechanic must complete all of the instructions in the service bulletin, including the intent therein. 2) The mechanic must correctly use and install all applicable parts supplied with the service bulletin kit. Only with written authorization from Cessna Aircraft Company can substitute parts or rebuilt parts be used to replace new parts. 3) The mechanic or airplane owner must use the technical data in the service bulletin only as approved and published. 4) The mechanic or airplane owner must apply the information in the service bulletin only to aircraft serial numbers identified in the "Effectivity" section of the bulletin. 5) The mechanic or airplane owner must use maintenance practices that are identified as acceptable standard practices in the aviation industry and governmental regulations. No individual or corporate organization other than Cessna Aircraft Company is authorized to make or apply any changes to a Cessna-issued service bulletin, service letter, or flight manual supplement without prior written consent from Cessna Aircraft Company. Cessna Aircraft Company is not responsible for the quality of maintenance performed to comply with this document, unless the maintenance is accomplished at a Cessna-owned Service Center. APPROVAL Cessna received FAA approval for the technical data in this publication that changes the airplane type design. FLIGHT CREW OPERATIONS No Changes May 29, 2014 Page 1 of 6 Cessna Aircraft Company, Cessna Customer Service, P.O. Box 7706, Wichita, KS 67277, U.S.A. 1-316-517-5800 This document contains technical data and is subject to U.S. export regulations. This information has been exported from the United States in accordance with export administration regulations. Diversion contrary to U.S. law is prohibited. ECCN: 9E991 COPYRIGHT 2014

WEIGHT AND BALANCE INFORMATION Negligible REFERENCES Cessna Model 525 Maintenance Manual Cessna Model 525A Maintenance Manual Cessna Model 525B Maintenance Manual Cessna Model 525 Wiring Diagram Manual Cessna Model 525A Wiring Diagram Manual Cessna Model 525B Wiring Diagram Manual PUBLICATIONS AFFECTED Cessna Model 525 Wiring Diagram Manual Cessna Model 525A Wiring Diagram Manual Cessna Model 525B Wiring Diagram Manual ACCOMPLISHMENT INSTRUCTIONS 1. Prepare the airplane for maintenance. A. Make sure that the airplane is electrically grounded. B. Make sure that all switches are in the OFF/NORM position. C. Disconnect electrical power from the airplane. (1) Disconnect the airplane battery. (2) Disconnect external electrical power. D. Attach maintenance warning tags to the battery and external power receptacle that have "DO NOT CONNECT ELECTRICAL POWER - MAINTENANCE IN PROGRESS" writtenonthem. 2. Get access to the aft power J-Box. A. (Model 525 airplanes) Open aft baggage compartment panels 321A and 322A and remove the cover from the aft side of the J-Box. (Refer to the Model 525 Maintenance Manual, Chapter 6, Access Plates and Panels Identification - Description and Operation.) B. (Model 525A and 525B airplanes) Open aft baggage compartment panel 321CC. (Refer to the applicable Maintenance Manual, Chapter 6, Access Plates and Panels Identification - Description and Operation.) 3. (Refer to Figure 1, Detail A.) Get access to the firewall shutoff valve relay wiring. A. Remove the cover from the forward side of the aft power J-Box. (Refer to the applicable Maintenance Manual, Chapter 24, DC Electrical Load Distribution - Maintenance Practices.) B. (Refer to Figure 2.) Disconnect electrical connector PZ102. 4. (Refer to Figure 2.) Modify the wiring. A. Install the electrical wire from BBPT041 to BBPZ102 using one 204814-1 Connector and one S2099-6 Contact and MS3367-1-0 Tie Straps as necessary. (Refer to the applicable wiring diagram manual, Chapter 20, Wiring - Maintenance Practices.) NOTE: Cut the BBPT041-BBPZ102 Electrical Wire as necessary to fit the model of airplane being modified. 5. (Refer to Figure 2.) Connect electrical connector PZ102. Page 2 May 29, 2014

6. Do an functional test of the firewall shutoff valve. (Refer to the applicable Maintenance Manual, Chapter 28, Fuel Distribution - Adjustment/Test.) 7. Install the cover on the forward side of the aft power J-Box. (Refer to the applicable Maintenance Manual, Chapter 24, DC Electrical Load Distribution - Maintenance Practices.) 8. Install the removed access panels. A. (Model 525 airplanes) Install the cover on the aft side of the J-Box and close aft baggage compartment panels 321A and 322A. (Refer to the Model 525 Maintenance Manual, Chapter 6, Access Plates and Panels Identification - Description and Operation.) B. (Model 525A and 525B airplanes) Close aft baggage compartment panel 321CC. (Refer to the applicable Maintenance Manual, Chapter 6, Access Plates and Panels Identification - Description and Operation.) 9. Record that this service bulletin has been completed. A. Complete a Maintenance Transaction Report. B. Put a copy of the completed Maintenance Transaction Report in the airplane logbook. C. Send a copy of the completed Maintenance Transaction Report to: CESCOM C/O Camp Systems International Incorporated, 8201 East 34th Street North, Building 1100 Suite 1101 Wichita, KS 67226. May 29, 2014 Page 3

Figure 1. Firewall Shutoff Valve Relay Removal/Installation (Sheet 1) Page 4 May 29, 2014

Figure 2. Fuel Firewall Shutoff Valve Relay Ground Wire Installation (Sheet 1) May 29, 2014 Page 5

MATERIAL INFORMATION Order the kit below to install this modification. NEW P/N QUAN- TITY 1 Kit, consisting of the following parts: M81044/12-20-9 130 inches Electrical Wire (Marked BBPT041-BBPZ102) KEY WORD OLD P/N INSTRUCTIONS/ DISPOSITION None S2099-6 1 Contact None MS3367-1-0 15 Tie Strap None 204814-1 1 Connector None 1 Instructions Page 6 May 29, 2014

OWNER ADVISORY TITLE FUEL - FIREWALL SHUTOFF VALVE GROUND IMPROVEMENT TO: Cessna Aircraft Owner REASON There is a ground wire missing for the right firewall shutoff valve relay. COMPLIANCE RECOMMENDED. This service bulletin should be accomplished at a scheduled maintenance period or inspection. LABOR HOURS WORK PHASE MAN-HOURS Modification 2.0 MATERIAL AVAILABILITY PART NUMBER AVAILABILITY COST * * WARRANTY This bulletin is recommended. Eligible airplanes may qualify for parts and labor coverage, as described below. May 29, 2014 Page 1 of 2 Cessna Aircraft Company, Cessna Customer Service, P.O. Box 7706, Wichita, KS 67277, U.S.A. 1-316-517-5800 This document contains technical data and is subject to U.S. export regulations. This information has been exported from the United States in accordance with export administration regulations. Diversion contrary to U.S. law is prohibited. ECCN: 9E991 COPYRIGHT 2014

OWNER ADVISORY Eligibility: Parts Coverage: Labor Coverage: Credit Application: s identified within the serial number effectivity of this service bulletin which are within the five-year/5,000 hour warranty period on the original issue date of this bulletin. Cessna-owned and Cessna-authorized Service Facilities, operators, or other maintenance facilities may submit a Credit Claim Form for the parts required to accomplish this bulletin. Cessna-owned and Cessna-authorized Service Facilities may submit a Credit Claim Form for the labor necessary to accomplish this service bulletin. Please note Manpower Requirements for coverage guidelines. All work must be completed and the Credit Claim Form submitted before the date shown below. Send the Credit Claim, along with any required parts (see Material Information), to the point of purchase. Parts to be returned to Cessna Service Parts & Programs should be forwarded to: Warranty Administration 7121 Southwest Boulevard Wichita, KS USA 67215 Expiration: June 30, 2016 NOTE: As a convenience, service documents are now available online to all our customers through a simple, free-of-charge registration process. If you would like to sign up, please visit the "Customer Access" link at www.cessnasupport.com to register. Page 2 May 29, 2014