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

Transcription

1 TITLE DOORS - CABIN DOOR SUPPORT STRUT FITTING MODIFICATION EFFECTIVITY MODEL SERIAL NUMBERS 680 (Citation Sovereign) thru (Citation Sovereign+) thru REASON The equivalent of this service bulletin has been incorporated on production airplanes and On. NOTE: Textron Aviation-owned Service Centers are the only facilities that can complete this service bulletin. Heavy foot traffic can cause the outer cabin door frames to crack under the support strut fittings. DESCRIPTION This service bulletin provides parts and instructions to replace the support strut fittings and inspect the outer door frames for cracks. If the outer door frame has a crack, this service bulletin provides instructions to replace the door frame with a Cessna Engineering Drawing. 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 Textron Aviation-owned Citation Service Center. February 9, 2016 Page 1 of 6 Cessna Aircraft Company, Cessna Customer Service, P.O. Box 7706, Wichita, KS 67277, U.S.A 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 2016

2 APPROVAL Cessna received FAA approval for the technical data in this publication that changes the airplane type design. FLIGHT CREW OPERATIONS No Changes CONSUMABLE MATERIAL You must use the consumable materials that follow, or their equivalent, to complete this service bulletin. NAME NUMBER MANUFACTURER USE Color Chemical Film U Corrosion Resistant Primer Textron Aviation Parts Distribution 7121 Southwest Boulevard Wichita, KS To prepare aluminum surface for intermediate primer. K Textron Aviation Parts Distribution Final finish for aluminum. Sealant (Type X) U544067S Textron Aviation Parts & Distribution To prevent dissimilar metal corrosion. WEIGHT AND BALANCE INFORMATION Negligible REFERENCES Cessna Model 680 Maintenance Manual Cessna Model 680 Structural Repair Manual NOTE: To install the new cabin door support fittings on your airplane, you must get the engineering documents that follow. You must use the most recent revision and all of the applicable drawing change notices (DCN) for each engineering document. DOCUMENT NUMBER TITLE CAB DOOR SUPT STRUT FITT FIELD PUBLICATIONS AFFECTED None 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 batteries. (2) Disconnect external electrical power. D. Attach maintenance warning tags to the batteries and external power receptacle that have "DO NOT CONNECT ELECTRICAL POWER - MAINTENANCE IN PROGRESS" written on them. Page 2 February 9, 2016

3 2. Remove the forward and aft support strut fittings. (Refer to Cessna Engineering Drawing ) NOTE: Review all of the Modification Notes and Flag Notes on the engineering drawing. A. Remove the cabin door steps. (Refer to the Model 680 Maintenance Manual, Chapter 52, Cabin Door Step - Maintenance Practices.) B. Remove the forward and aft cabin door step closeout panels. C. Support the cabin door with a padded stand. D. Remove the forward and aft cabin door support strut from the fittings on the cabin door. E. Remove the forward and aft cabin door strut support fittings from the cabin door. F. Remove the sealant, if sealant is present, from the frame under the strut fittings. 3. Do an inspection of the outer door frame. A. Do a visual inspection of the forward and aft outer door frames for cracks under the cabin door support strut fittings. B. Complete Step 4 if the forward outer door frame has cracks. C. Complete Step 5 if the aft outer door frame has cracks. D. Go to Step 7 if the forward and aft outer door frames do not have cracks. CAUTION: Do not remove the forward and aft outer door frames at the same time. Removing both outer door frames at the same time can cause the remaining door structure to shift and cause issues with rigging, opening, and closing the door. 4. Replace the forward outer door frame. (Refer to Cessna Engineering Drawing ) NOTE: Review all of the Modification Notes and Flag Notes on the engineering drawing. NOTE: Touch up all bare material with color chemical film treatment and corrosion resistant primer to protect all bare material before the frame is installed. (Refer to the Model 680 Structural Repair Manual, Chapter 51, Protective Treatment of Metal - Description and Operation.) 5. Replace the aft outer door frame. (Refer to Cessna Engineering Drawing ) NOTE: Review all of the Modification Notes and Flag Notes on the engineering drawing. NOTE: Touch up all bare material with color chemical film treatment and corrosion resistant primer to protect all bare material before the frame is installed. (Refer to the Model 680 Structural Repair Manual, Chapter 51, Protective Treatment of Metal - Description and Operation.) 6. (If the cabin door was removed in Step 4 or 5.) Install the cabin door. (Refer to the Model 680 Maintenance Manual, Chapter 52, Cabin Door - Maintenance Practices.) 7. Install the forward and aft support strut fittings. A. Replace the forward and aft outer door frame support strut fitting. (Refer to Cessna Engineering Drawing ) NOTE: Review all of the Modification Notes and Flag Notes on the engineering drawing. (1) Fay seal the face and each countersink of the and Fittings with Type X, Class B sealant. (Refer to Cessna Engineering Drawing , Flag Note 3.) (a) After the fittings are installed, wipe away excess sealant from the screw heads. B. Install the Driver Arm Assembly. (Refer to Cessna Engineering Drawing ) C. Install the cabin door steps. (1) Install the forward and aft cabin door support struts to the fittings on the cabin door. February 9, 2016 Page 3

4 8. Do the steps that follow if the cabin door was removed. A. Adjust the cabin door. (Refer to the Model 680 Maintenance Manual, Chapter 52, Cabin Door - Adjustment/Test.) B. Adjust the cabin door latching/locking system. (Refer to the Model 680 Maintenance Manual, Chapter 52, Cabin Door Latching/Locking System - Adjustment/Test.) C. Adjust the cabin door closing handle, handrail, and support strut. (Refer to the Model 680 Maintenance Manual, Chapter 52, Cabin Door Closing Handle, Handrail, and Support Strut - Adjustment/Test.) 9. Install the cabin door steps and closeout panels. (Refer to the Model 680 Maintenance Manual, Chapter 52, Cabin Door Step - Maintenance Practices.) 10. Remove the maintenance warning tags and connect the airplane batteries. 11. 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 MATERIAL INFORMATION (All airplanes) Order the kit below to install this modification. NEW P/N QUAN- TITY -0 1 Kit, consisting of the following parts: KEY WORD OLD P/N INSTRUCTIONS/ DISPOSITION Screw Same Discard Forward Fitting Discard Aft Fitting Discard Driver Arm Discard MS Snap Ring Same Ring MS20426A8-8 4 Rivet NAS7504U5 andms21048l4 Discard MS20426B3-5 8 Rivet NAS1399C3-3 Discard NAS7504U5 4 Bolt Same Discard S Washer 1 Instructions Page 4 February 9, 2016

5 Order the kit that follows to replace the forward outer door frame. NOTE: All driven rivets necessary to accomplish this service bulletin have been excluded from the material information section and will be installed at the Service Center. NEW P/N QUAN- TITY -1 1 Kit, consisting of the following parts: KEY WORD OLD P/N INSTRUCTIONS/ DISPOSITION Forward Outer Frame HL10VBJ4-2 2 Pin Same Discard HL10VBJ5-5 2 Pin Same Discard HL11VBJ Pin Same Discard HL11VBJ5-4 2 Pin Same Discard HL11VBJ Pin Same Discard HL Collar Same Discard HL97DU4 2 Collar Same Discard HL97DU5 30 Collar Same Discard MS21047L3 2 Nutplate Same Discard MS21047L4 1 Nutplate Same Discard MS21048L4 2 Nutplate Same Discard MS24694-C52 2 Screw Same Discard MS24694-C99 1 Screw Same Discard NAS1399C3-2 4 Rivet Same Discard NAS Screw Same Discard NAS Screw Same Discard NAS Screw Same Discard S Rivet Same Discard S Rivet Same Discard 1 Instructions February 9, 2016 Page 5

6 Order the kit that follows to replace the aft outer door frame. NOTE: All driven rivets necessary to accomplish this service bulletin have been excluded from the material information section and will be installed at the Service Center. NEW P/N QUAN- TITY -2 1 Kit, consisting of the following parts: KEY WORD OLD P/N INSTRUCTIONS/ DISPOSITION Aft Outer Frame HL10VBJ4-2 2 Pin Same Discard HL11VBJ Pin Same Discard HL11VBJ5-4 2 Pin Same Discard HL11VBJ Pin Same Discard HL Collar Same Discard HL97DU4 2 Collar Same Discard HL97DU5 30 Collar Same Discard MS21047L3 2 Nutplate Same Discard MS21047L4 1 Nutplate Same Discard MS21048L4 2 Nutplate Same Discard MS24694-C52 2 Screw Same Discard MS24694-C99 1 Screw Same Discard NAS1399C3-2 4 Rivet Same Discard NAS Screw Same Discard NAS Screw Same Discard NAS Screw Same Discard NAS Screw Same Discard S Rivet Same Discard S Rivet Same Discard 1 Instructions Page 6 February 9, 2016

7 OWNER ADVISORY TITLE DOORS - CABIN DOOR SUPPORT STRUT FITTING MODIFICATION TO: REASON Cessna Aircraft Owner Heavy foot traffic can cause the outer cabin door frames to crack under the support strut fittings. COMPLIANCE RECOMMENDED. This service bulletin should be accomplished at a scheduled maintenance period or inspection. LABOR HOURS WORK PHASE MAN-HOURS Cabin Door Support Struts Fitting Modification 9.0 Forward or Aft Outer Door Frame Replacement MATERIAL AVAILABILITY 100 (per frame) PART NUMBER AVAILABILITY COST -0 * * -1 * * -2 * * * Please contact Textron Aviation Parts Distribution for current cost and availability of parts listed in this service bulletin. Phone at (Domestic) or (International). Send to: dirop@txtav.com or telefax at Based on availability and lead times, parts will require advanced scheduling. February 9, 2016 Page 1 of 2 Cessna Aircraft Company, Cessna Customer Service, P.O. Box 7706, Wichita, KS 67277, U.S.A 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 2016

8 OWNER ADVISORY WARRANTY This bulletin is recommended. Eligible airplanes may qualify for parts and labor coverage, as described below. Eligibility: Parts Coverage: Labor Coverage: Credit Application: All Citations identified within the serial number effectivity of this service bulletin. Cessna-owned and Cessna-authorized Citation Service Facilities, operators, or other maintenance facilities may submit a Citation Claim Form for the parts required to accomplish this bulletin. Cessna-owned and Cessna-authorized Citation Service Facilities may submit a Citation 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 Citation Claim Form submitted before the date shown below. Send the Citation Claim, along with any required parts (see Material Information), to the point of purchase. Parts to be returned to Textron Aviation Parts Distribution should be forwarded to: Citation Warranty Administration 7121 Southwest Boulevard Wichita, KS USA Expiration: February 9, 2018 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 to register. Page 2 February 9, 2016