Cessna Turbo 210L Service Bulletin

FAA approval has been obtained on technical data in this publication that affects airplane type design. For Reims Aviation airplanes; DGAC approval has been obtained on technical data in this publication that affects airplane type design. MAN-HOURS Approximately 1.5 to 2.6 man-hours per fuel filler port for Service Kit installation. Approximately 0.2 man-hours per fuel cap for airplanes requiring cap replacement only. MATERIAL The following parts are available from the Cessna Supply Division thru an appropriate Cessna Service Station for the suggested list price shown. PART NUMBER SK177-39D (See Note 1) SK177-40D (See Note1) SK182-85B (See Note 1&2) SK182-86C (See Note 1) C156003-0101 (See Note 3&5) 0709115-2 (See Note 4) 000001 DESCRIPTION Fuel Cap Modification Kit Standard Range Tanks Fuel Cap Modification - Kit Long Range Tanks Fuel Cap Modification Kit Bladder Fuel Cells - Fuel Cap Modification - Kit Integral Fuel Cells Fuel Cap QTY./ AIRPLANE PRICE * 1 $ 115.00 (✗) ea. - * 1 $ 112.00 (X) ea. * 1 $ 144.00 (X) ea. * 95.80 (X) ea. 2 * $ 25.90 (X) ea. * Fuel Cap Cover Door 2 $ 25.50 (X) ea. Avgas Placard - GAMA 2 $ 2.30 (PS) ea. (See Note 3) (80, 100LL, 100) Avgas Placard - GAMA (100LL, 100) Sealant (6 Oz. SemKit) Sealant (2.5 Oz. SemKit) S2608-1 (See Note 5) CMNP022CLASSB1/2 (Alternate PR1403G-B1/2) (See Note 1) CMNP021CLASSB1/2 (Alternate MILS8802||B1/2) (See Note 3&5) NOTE 1: Refer to the attached Fuel Cap Modification Service Kits installation instructions for appli- cable airplane model and serials. $ 1.50 (PS) ea. * 1 $ 27.30 (X) ea. * $ 20.90 (✗) ea. SEB92-27 September 4, 1992 Page 3 * NOTE 2: Airplanes with optional Auxiliary Refueling (4 fuel filler caps) will require 2 ea. per airplane. NOTE 3: For all serials of models 140A, 150, A150, F150, FA150, FRA150, 170, 172, F172, P172, FP172, 175 and 180 serials 30000 thru 50448 and 182 serials 33000 thru 51825. NOTE 4: Required only for initial installation of vented fuel caps, model 180 serials 30000 thru 50448 and model 182 serials 33000 thru 51825. NOTE 5: For all serials of models R172 and FR172 airplanes. The special below-cost price shown will remain in effect thru December 31, 1993. Thereafter, prices may increase to reflect cost increases to Cessna, but will remain specially priced to provide no profit to Cessna. ALL PRICES SUBJECT TO CHANGE WITHOUT NOTICE ACCOMPLISHMENT INSTRUCTIONS 1. For models 140A, 150, A150, F150, FA150, FRA150, 170 172, F172, P172, FP172, FR172, 175, 180 serials 30000 thru 50448 and 182 serials 33000 thru 51825: A. B. C. Remove existing fuel caps from airplane and replace with new C156003-0101 vented fuel caps. For vented fuel cap installations on models 140A, 150, A150, F150, FA150, FRA150, 170, 172, F172, P172, FP172, FR172 and 175, manufactured prior to 1972. 1. 2. If desired, the fuel filler neck may be rotated (tightened or loosened, as required) to align the fuel cap handles with the slipstream. After the fuel filler neck has been realigned, fillet seal the filler neck to fuel tank adapter plate joint with CMNP021CLASSB1/2 sealant or equivalent. For model 180 serials 30000 thru 50448 and model 182 serials 33000 thru 51825; remove existing fuel cap cover door and install new 0709115-2 cover door on initial installation of vented fuel caps. 2. D. Install the appropriate fuel grade GAMA placard next to each fuel filler port. E. Make an appropriate entry in the airplane logbook stating this Service Bulletin has been complied with and method of compliance. For models 177, 177RG, F177RG, 180 serials 50449 and On, 182 serials 51826 and On, R182, FR182, 185, 188, 205, 206, P206, U206, 207, 210 and T210. A. Service Kits SK177-39D, SK177-40D, SK182-85B and SK182-86C Fuel Cap Modification installation instructions are attached. CREDIT Not Applicable OWNER NOTIFICATION On September 11, 1992 a copy of this Service Bulletin less Service Kits installation instructions will be sent to applicable owners of record. Please contact a Cessna Single Engine Service Station for detailed information regarding specific parts requirements and the accomplishment of this Service Bulletin on your airplane. Page 4 * * * SEB92-27 September 4, 1992 Single-Engine SERVICE KIT TITLE REDUCED DIAMETER FUEL CAP MODIFICATION (STANDARD TANKS) Cessna SK177-39D EFFECTIVITY MODEL(S) 177 177RG F177RG SERIAL NUMBERS 17700001 thru 17702752 177RG0001 thru 177RG0282 F177RG0001 thru F177RG0062 DESCRIPTION The following procedures provide instructions to replace existing flush type fuel cap with a protruding reduc reduced diameter fuel cap and a new adapter filler door. APPROVAL FAA approval has been obtained on technical data in this publication that affects airplane type design. For Reims Aviation airplanes: DGAC approval has been obtained on technical data in this publication that affects airplane type design. |that REFERENCE SEB92-27 CHANGE IN WEIGHT AND BALANCE WEIGHT INCREASE ARM RESULTANT MOMENT MOMENT/1000 0.6 pounds 40.6 inches 24.3 inch/pounds 0.024 October 5, 1984 Revised September 4, 1992 SK177-39 Page 1 of 4 To obtain satisfactory results, procedures specified in this publication must be accomplished in accordance with accepted methods and prevailing government regulations. The Cessna Aircraft Company cannot be responsible for the quality of work performed in accomplishing the requirements of this publication. The Cessna Aircraft Company, Product Support, P.O. Box 7706, Wichita, Kansas 67277, U.S.A. (316) 941-7550, Telex 4319022, Facsimile (316) 942-9006 COPYRIGHT © 1992 SERVICE KIT SK177-39D MATERIAL INFORMATION PART NUMBER SK177-39D C156003-0101 C156001-0104 S2608-1 000001 2009015-4 QUANTITY 122222- DESCRIPTION Kit, consisting of the following parts: Cap Assembly Chain Assembly Placard - GAMA Avgas, 100/100LL Placard GAMA Avgas, 80/100LL/100 Filler Door Assembly Instructions NOTE: In addition to the parts provided in this Service Kit, the following additional parts must be available for installation of this service kit. PART NUMBER CMNP022CLASSB1/2 Various QUANTITY 1 As Required DESCRIPTION - Sealant Low Adhesion (6 Oz. SemKit) (Alternate PR1403G-B1/2 or equivalent) Placards (to replace those removed during installation of this kit). (Refer to appropriate Parts Catalog.) ACCOMPLISHMENT INSTRUCTIONS 1. Description of Installation. A. Draining fuel from tanks. B. C. Removing existing fuel filler door assemblies with cap and adapter assemblies. Installing and sealing new filler door assemblies furnished in kit. D. 2. Installing placards removed for this installation. Installation Instructions. A. (Refer to Figure 1.) Fuel Cap and Adapter Modification. | (1) Drain fuel from both RH and LH wing tanks. (2) Remove existing filler door assembly, which includes cap, adapter and chain assembly, discard filler door assembly, retain screws (3). (3) Clean off all old sealer remaining on the filler door assembly cavity, on leading edge upper skin (4). NOTE: Be sure and check fuel cell for dirt, old sealer, etc. that may have fallen into fuel cell. Clean or vacuum as required. (4) Apply CMNP022CLASSB1/2 sealer per instructions on container and appropriate Service Manual sealing procedures, to the faying surface (6) on door assembly (7). Cure time for sealer is 24 hours at approximately 77° F (25° C) and 50% relative humidity. NOTE: Be sure and position the filler door assembly with the slotted opening of the indicator guard forward. (5) Install new filler door assembly (7) and secure with retained screws (3). October 5, 1984 Revised September 4, 1992 SK177-39 Page 2 3. SERVICE KIT (6) Attach chain assembly (2) to filler door assembly (7) and cap assembly (1). NOTE: SK177-39D Replace all placards removed during this modification. Refer to the appropriate Parts Catalog for part numbers. Install appropriate GAMA fuel placard near fuel filler. (7) Repeat these same procedures for the opposite wing. (8) After completion of this modification, refuel airplane. Make an entry in the airplane logbook stating this service kit has been installed. October 5, 1984 Revised September 4, 1992 SK177-39 Page 3 SERVICE KIT KIT SK177-39D A (1) C156003-0101 CAP ASSEMBLY (2 REQUIRED) (CAP SHOWN IN CLOSED POSITION) (7) 2009015-4 FILLER DOOR ASSEMBLY - LH (2 REQUIRED) (2) C156001-0104 CHAIN ASSEMBLY (2 REQUIRED) (3) EXISTING SCREWS (REFERENCE) (6) FAYING SURFACE (REFERENCE) October 5, 1984 Revised September 4, 1992 FWD OUTBO DETAIL A LH SHOWN - RH OPPOSITE Figure 1. Fuel Cap & Adapter Modification (4) WING LEADING EDGE UPPER SKIN (REFERENCE) (5) DOUBLER ASSEMBLY (REFERENCE) SK177-39 Page 4 Single-Engine SERVICE KIT TITLE REDUCED DIAMETER FUEL CAP MODIFICATION (LONG RANGE TANKS) Cessna SK177-40D EFFECTIVITY MODEL(S) 177 177RG F177RG SERIAL NUMBERS 17701774 thru 17702752 177RG0283 thru 177RG1366 F177RG0063 thru F177RG0177 DESCRIPTION The following procedures provide instructions to replace existing flush type fuel cap with a protruding reduced diameter fuel cap and a new adapter filler door. APPROVAL FAA approval has been obtained on technical data in this publication that affects airplane type design. For Reims Aviation airplanes: DGAC approval has been obtained on technical data in this publication that affects airplane type design. REFERENCE SEB92-27 CHANGE IN WEIGHT AND BALANCE WEIGHT INCREASE I ARM RESULTANT MOMENT MOMENT/1000 0.6 pounds 40.6 inches 24.3 inch/pounds 0.024 October 5, 1984 Revised September 4, 1992 SK177-40 Page 1 of 4 To obtain satisfactory results, procedures specified in this publication must be accomplished in accordance with accepted methods and prevailing government regulations. The Cessna Aircraft Company cannot be responsible for the quality of work performed in accomplishing the requirements of this publication. The Cessna Aircraft Company, Product Support, P.O. Box 7706, Wichita, Kansas 67277, U.S.A. (316) 941-7550, Telex 4319022, Facsimile (316) 942-9006 COPYRIGHT © 1992 MATERIAL INFORMATION PART NUMBER SK177-40D SERVICE KIT QUANTITY 1 C156001-0104 C156003-0101 S2608-1 2009015-5 2009015-6 22211 2 1 1 DESCRIPTION SK177-40D Kit, consisting of the following parts: Chain Assembly Cap Assembly Placard GAMA Avgas, 100/100LL - Filler Door Assembly - LH Filler Door Assembly - RH Instructions NOTE: In addition to the parts provided in this Service Kit, the following additional parts must be available for installation of this service kit. PART NUMBER CMNP022CLASSB1/2 QUANTITY 1 Various As Required DESCRIPTION - Sealant Low Adhesion - (6 oz. Semkit) Alternate is PR1403G-B1/2 or equivalent Placards (to replace those removed during installation of this kit). (Refer to appropriate Parts Catalog.) ACCOMPLISHMENT INSTRUCTIONS 1. Description of Installation. A. Draining fuel from tanks. B. Removing existing fuel filler door assemblies with cap and adapter assemblies. 2. C. Installing and sealing new filler door assemblies furnished in kit. D. Installing placards removed for this installation. Installation Instructions. A. (Refer to Figure 1.) Fuel Cap and Adapter Modification. (1) Drain fuel from both RH and LH wing tanks. (2) Remove existing filler door assembly, which includes cap, adapter and chain assembly, discard filler door assembly, retain screws (3). (3) Clean off all old sealer remaining on the filler door assembly cavity, on leading edge upper skin (4). NOTE: Be sure and check fuel cell for dirt, old sealer, etc. that may have fallen into fuel cell. Clean or vacuum as required. (4) Apply CMNP022CLASSB1/2 sealer per instructions on container and appropriate Service Manual sealing procedures, to the faying surface (6) on door assembly (7). Cure time for sealer is 24 hours at approximately 77° F (25° C) and 50% relative humidity. October 5, 1984 Revised September 4, 1992 SK177-40 Page 2 SERVICE KIT SK177-40D (5) Install new filler door assembly (7) and secure with retained screws (3). NOTE: Be sure and position the filler door assembly with the slotted opening of the indicator guard forward and slightly outboard for both the RH & LH filler door assemblies, 2009015-5 for the LH wing and 2009015-6 for the RH wing.. (6) Attach chain assembly (2) to filler door assembly (7) and cap assembly (1). NOTE: Replace all placards removed during this modification. Refer to the appropriate Parts Catalog for part numbers. Install S2608-1 GAMA fuel placard near fuel filler. (7) Repeat these same procedures for the opposite wing. (8) After completion of this modification, refuel airplane. 3. Make an entry in the airplane logbook stating this service kit has been installed. October 5, 1984 Revised September 4, 1992 SK177-40 Page 3 SERVICE KIT KIT SK177-40D A (1) C156003-0101 CAP ASSEMBLY (2 REQUIRED) (CAP SHOWN IN CLOSED POSITION) (7) 2009015-5 FILLER DOOR ASSEMBLY - LH 2009015-6 FILLER DOOR ASSEMBLY - RH (1 REQUIRED) (2) C156001-0104 CHAIN ASSEMBLY (2 REQUIRED) (3) EXISTING SCREWS (REFERENCE) (6) FAYING SURFACE (REFERENCE___ October 5, 1984 Revised September 4, 1992 FWD OUTBD DETAIL A LH SHOWN -RH OPPOSITE Figure 1. Fuel Cap & Adapter Modification (4) WING LEADING EDGE UPPER SKIN (REFERENCE) (5) DOUBLER ASSEMBLY (REFERENCE) SK177-40 Page 4 Single-Engine SERVICE KIT TITLE REDUCED DIAMETER FUEL CAP MODIFICATION (BLADDER FUEL CELLS) Cessna SK182-85B EFFECTIVITY MODEL(S) 180 182 R182 F182 FR182 A182 185 188 188 205 206 P206, TP206 U206, TU206 207, T207 210 T210 SERIAL NUMBERS 50449 thru 50911 18050912 thru 18053000 18053001 thru 18053203 (With Opt. Bladder Tank) 51826 thru 53007 18253008 thru 18266590 R18200001 thru R18200583 F18200001 thru F18200094 FR18200001 thru FR18200020 A182-0001 thru A182-0146 185-0001 thru 18503683 18503684 thru 18504424 (With Opt. Bladder Tank) 188-0446 thru 18803296 (Wing Tanks Only) 18800967T thru 18803296T (Wing Tanks Only) 205-0001 thru 205-0577 206-0001 thru 206-0275 P206-0001 thru P20600647 U206-0276 thru U20604649 20700001 thru 20700788 57001 thru 57575 21057576 thru 21058818 T210-0001 thru T210-0197 DESCRIPTION The following procedures provide instructions to replace existing flush type fuel cap with a protruding The following procedures provide instruct APPROVAL FAA approval has been obtained on technical data in this publication that affects airplane type design. For Reims Aviation airplanes: DGAC approval has been obtained on technical data in this publication that that affects airplane type design. REFERENCE SEB92-27 CHANGE IN WEIGHT AND BALANCE Negligible _September 21, 1984 Revised September 4, 1992 SK182-85 Page 1 of 4 To obtain satisfactory results, procedures specified in this publication must be accomplished in accordance with accepted industry maintenance practices and prevailing government regulations. The Cessna Aircraft Company is not responsible for the quality of work performed in complying with the requirements herein. The Cessna Aircraft Company, Customer Services, P.O. Box 7706, Wichita, Kansas 67277, U.S.A. (316) 941-7550, Telex 4319022, Telefax (316) 942-9006 COPYRIGHT © 1992 SERVICE KIT SK182-85B MATERIAL INFORMATION NOTE: Models 180, 185, 206 and 207 airplanes equipped with optional auxiliary refueling will require two each SK182-85B Kits (4 caps & adapter assemblies). NOTE: PART NUMBER SK182-85B C156001-0104 C156003-0101 S2608-1 000001 0726002-1 1621412-1 QUANTITY DESCRIPTION 1 Kit, consisting of the following 2 2 2 2 2 2 22 1 parts: Chain Assembly Cap Assembly Placard GAMA Avgas, - 100/100LL Placard GAMA Avgas, 80/100LL/100 Gasket Adapter Assembly Instructions In addition to the parts provided in this Service Kit, the following additional parts must be available for installation of this service kit. PART NUMBER Various QUANTITY As Required DESCRIPTION Installation of this kit consists of: 1. A. Draining fuel from tanks. B. Removing existing fuel cap and adapter assembly. C. D. Installing new gasket, adapter, and cap assembly. 2. DESCRIPTION Placards (to replace those removed during installation of this kit). (Refer to appropriate Parts Catalog.) Installing new placards removed for this modification. Installation Instructions. A. Drain fuel from both RH and LH wing tanks. B. C. Remove existing fuel cap adapter in location (1), with existing cap assembly (4) and gasket. Retain hardware, discard fuel cap, chain, and adapter assembly. NOTE: Be sure and check fuel bladder for dirt or foreign matter that may have fallen into bladder. Clean or vacuum out bladder as required. Install new adapter assembly (1) with 0726002-1 gasket furnished in kit, using retained hardware (2) removed in step (2). NOTE: Install adapter assembly with the long side of internal filler neck extension forward. September 21, 1984 Revised September 4, 1992 SK182-85B Page SERVICE KIT SK182-85B 3. 4. 5. D. E. Attach chain assembly to cap assembly (4), and adapter assembly (1). NOTE: Replace all placards removed during this modification. Refer to appropriate Parts Catalog for part numbers. Delete 1205253-1 Fuel Cap Alignment Placard with incorporation of this kit. Install appropriate GAMA fuel placard near fuel filler. Repeat these same procedures for the opposite side. "Turbo" placards removal (if installed): A. B. Remove adhesive backed external “Turbo" placards by heating with a heat gun until the adhesive softens, then remove the placard. Clean excess adhesive off the airplane with naptha or methyl ethyl ketone (MEK). NOTE: If airplane paint is lacquer (or if paint type is unknown) use naptha initially. MEK will soften lacquer paint and may cause it to wrinkle. Remove mechanically fastened external "Turbo" placards (attached with screws or rivets) by removing the attaching fasteners. Plug the screw or rivet holes with suitable sized cherry rivets and paint to match the airplane. After completion of both fuel cap replacements, refuel airplane. Make an entry in the airplane logbook stating this service kit has been installed. September 21, 1984 Revised September 4, 1992 SK182-85B Page 3