Service Bulletins for Cessna T210 Turbo Centurion

136.00 (X) ea $ 133.00 (X) ea. $ 132.00 (X) ea. $ 154.00 (X) ea. S 108.00 (X) ea $ 113.00 (X) ea. $ 98.00 (X) ea $ 147.00 (X) ea September 4, 1992 Page 3 PART NUMBER DESCRIPTION SK195-10-2 SK206-44-1 SK206-44-2 SK206-44-3 SK206-44-4 SK206-44-5 SK206-44-6 SK207-18-1 SK207-18-2 SK207-18-3 SK207-18-4 SK207-18-5 SK207-18-6 SK207-18-7 SK210-141-1 SK210-141-2 SK210-141-3 EC1300LP RTV102 Seat Belt and Shoulder Harness Installation Kit Seat Belt and Shoulder Harness Installation Kit Seat Belt and Shoulder Harness Installation Kit Seat Belt and Shoulder Harness Installation Kit Seat Bell and Shoulder Hamness Installation Kit Seat Belt and Shoulder Harness Installation Kit Seat Bell and Shoulder Hamoss Installation Kit Seat Bell And Shoulder Harness Installation Kit Seat Belt And Shoulder Hamness Installation Kit Seat Belt And Shoulder Hamess Installation Kit Seat Belt And Shoulder Hamness Installation Kit Seat Belt And Shoulder Harness Installation Kit Seat Belt And Shoulder Hamess Installation Kit Seat Belt And Shoulder Hamess installation Kit Seat Belt And Shoulder Harness Installation Kit Seat Belt And Shoulder Harness Installation Kit Seat Belt And Shoulder Harness Installation Kit Adhesive (As Required) Sealant (As Required) PRICE $198.00 (X) ea $132.00 (X) ea. $ 122.00 (X) ea $167.00 (X) ea. $121.00 (X) ea. $111.00 (X) ea. 5 121.00 (X) ea. S 70.10 (X) ea * $ 67.90 (X) ea. 126.00 (X) ea. * $ 68.00 (X) ea. S 68.00 (X) ea. 69.00 (X) ea. $ 67.00 (X) ea. $131.00 (X) ea. S 125.00 (X) ea. $ 101.00 (X) ea. RTV157 Sealant 17.60 (X) pt. 13.00 (X) Ba. $ 19.40 (X) ea. (As Required) * 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 Page 4 SEB92-28 September 4, 1992 ACCOMPLISHMENT INSTRUCTIONS Instructions for the Seat Belt and Shoulder Harness Assembly Installation Kits are included in each Service Kit. A copy of the installation instructions for Service Kits SK170-12 and SK172-136 are attached for information purposes to show a representative sample of the seat belt and shoulder harness assembly installation. CREDIT Not Applicable OWNER NOTIFICATION On September 11, 1992 a copy of this Service Bulletin less Shoulder Harness Service Kit Applicability Table and 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 SEB92-28 September 4, 1992 Page 5 CESSNA SAFETY ENHANCEMENT PROGRAM SINGLE ENGINE SERVICE BULLETIN September 4, 1992 TITLE FUEL SYSTEM QUICK DRAIN VALVE INSTALLATION EFFECTIVITY Normally aspirated and turbocharged airplanes within the serial ranges listed below. SEB92-24 MODEL SERIES YEAR SERIAL NUMBERS 120 1946 thru 1949 8000 thru 15075 140 1946 thru 1951 8000 Thru 15724 150 1969 thru 1960 17001 thru 17999 150 1960 59001 thru 59018 150 1961 thru 1974 15059019 thru 15075781 A150 1970 thru 1974 A1500001 thru A1500523 F150 1966 thru 1969 F150-0001 thru FIED 0529 F150 1970 thru 1974 F15000530 thru F15001143 FA150 1970 thru 1971 FA1500001 thru FA1500120 FRA150 1972 thru 1974 FRA1500121 thru FRA1500261 170 1948 thru 1956 18000 thru 27169 172 1956 thru 1960 28000 thru 47746 172 1961 thru 1974 17247747 thru 17263458 F172 1963 thru 1969 F172-0001 thru F172-0654 F172 1970 thru 1974 F17200655 thru F17201234 FR172 1968 thru 1974 FR17200001 thru FR17200530 P172 1963 P17257120 thru P17257188 FP172 1963 FP172-0001 thru FP172-0003 175 1958 thru 1960 55001 thru 66777 175 1961 thru 1962 17556778 thru 17557119 177 1968 thru 1974 17700001 thru 17702123 177RG 1971 thru 1974 177RG0001 thru F177RG0592 F177AG 1971 thru 1974 F177RG0001 thru F177RG0122 180 180 182 182 1963 thru 1960 1961 thru 1974 1956 thru 1960 1961 thru 1974 30000 thru 50911 18050912 thru 18052500 33000 thru 53007 18253008 thru 18263475 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. Cessna The Cessna Aircraft Company Customer Services PO Box 7706 Wichita, Kamas 67277 USA 316-941-7550 TELEX 4319022 FAX 316-942-9006 Comp MODEL SERIES A182 185 185 190 195 205 206 YEAR 1966 thru 1976 1961 thru 1969 1970 thru 1974 SERIAL NUMBERS A182-0001 thru A182-0148 185-0001 thru 185-1599 18501600 thru 18502565 1948 thru 1953 7001 thru 16183 1948 thru 1953 7001 thru 16183 1963 thru 1964 205-0001 thru 205-0577 1964 206-0001 thru 206-0275 P206/TP206 1965 thru 1969 P206-0001 thru P206-0603 P206/TP206 U206/TU206 1970 P20600604 thru P20600647 1965 thru 1969 U206-0276 thru U206-1444 U206/TU206 1970 thru 1974 U20601445 thru U20602579 207/T207 1969 thru 1974 20700001 thru 20700267 210 210 1960 1961 thru 1966 57001 thru 57575 21057576 thru 21058818 210/T210 1969 thru 1974 21059062 thru 21060539 T210 T210 1966 1969 T210-0001 thru T210-0197 T210-0393 thru T210-0454 PURPOSE To provide a modification for installing fuel tank quick drain valves in place of the existing drain plugs. These drains will assist in the detection and removal of water and/or other fuel contaminants in the wing fuel tanks. With the airplane on a level surface, fuel samples from each fuel drain shall be taken during each preflight inspection to verify that the airplane has been serviced with the correct aviation fuel and that no water or other contaminants are present. Water, contaminants and/or unidentifiable fuel shall be removed from the fuel system before flight. Failure to verify that the airplane has been serviced with the proper type grade of aviation fuel and to remove all fuel contaminants before flight may result in loss of engine power or engine stoppage in flight. COMPLIANCE Mandatory; shall be accomplished within the next 400 hours of operation or 12 months, whichever occurs first. NOTE: This Service Bulletin supersedes Cessna Single Engine Service Information Letter SE79- 45; Fuel Quick Drains for single engine airplanes. If SE79-45 or FAA AD86-19-11 has pre- viously been accomplished by installing AK150-82, AK177-23, AK177-37, AK180-77, AK206-61 or AK210-89 (or later revision), compliance with this Service Bulletin is not re- quired. 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. MAN-HOURS Estimated 0.3 man-hour per valve. Page 2 SEB92-24 September 4, 1992 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 SK150-60 SK177-50 DESCRIPTION QTY AIRPLANE Fuel Sampler Cup and Drain Valve Installation PRICE $ 29.40 (X) ea. Kit (See Note 1) Fuel Sampler Cup and Drain Valve Installation Kit (See Note 1) $ 28.90 (X) oa. SK177-51 Fuel Sampler Cup and * $ 31.30 (X) ea. Drain Valve Installation Kit (See Note 1) SK185-51 Fuel Sampler Cup and Drain Valve Installation Kit (See Note 1) 1 * $ 26.60 (X) Ba. SK206-43 Fuel Sampler Cup and Drain Valve Installation Kit (See Note 1) 1 * $ 44.90 (X) ea. SK210-140 Fuel Sampler Cup and Drain Valve Installation Kit (See Note 1) * $ 47.10 (X) ea. NOTE 1: Refer to the attached Fuel Sampler Cup and Drain Valve Installation instructions for appli- cable airplane model and serials. 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 Service Kits, SK150-60, SK177-50, SK177-51, SK185-51, SK206-43 and SK210-140 Fuel Sampler Cup and Drain Valve Installation instructions are attached. SEB92-24 September 4, 1992 Page 3 = CREDIT Not Applicable OWNER NOTIFICATION On September 11, 1992 a copy of this Service Bulletin less the 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. 100 DE Page 4 SOTTOM TA-BUNE MOITOURT THE THOMIKELHIMODDA h SEB92-24 September 4, 1992 CESSNA SAFETY ENHANCEMENT PROGRAM SINGLE ENGINE SERVICE BULLETIN September 4, 1992 TITLE REDUCED DIAMETER VENTED FUEL CAP INSTALLATION AND TURBO PLACARD REMOVAL EFFECTIVITY Normally aspirated and turbocharged airplanes within the serial ranges listed below. MODEL SERIES YEAR SERIAL NUMBERS 140 1949 thru 1951 15200 thru 15724 150 1959 thru 1960 17001 thru 17999 150 1960 59001 thru 59018 150 1961 thru 1975 15059019 thru 15077005 A150 1970 thru 1975 A1500001 thru A1500609 F150 1966 thru 1969 F1ED 0001 thru F150-0529 F150 1970 thru 1975 FA150 1970 thru 1971 FRA150 1972 thru 1975 170 1949 thru 1956 172 1956 thru 1960 28000 172 1961 thru 1975 F172 1963 thru 1969 F172 1970 thru 1975 FR172 1968 thru 1975 P172 1963 FP172 1963 175 1958 thru 1960 175 1961 thru 1962 177 1968 thru 1978 177RG 1971 thru 1978 F177RG 1971 thru 1977 180 1953 thru 1960 180 1961 thru 1981 182 1956 thru 1960 33000 182 1961 thru 1984 A182 1966 thru 1974 F182 1976 thru 1980 A182 1978 thru 1984 FR182 1978 thru 1980 185 1961 thru 1969 185 1970 thru 1984 188 1968 thru 1969 188 1970 thru 1978 F15000530 FA1500001 thru FA1500120 FRA1500121 thru FRA1500281 18730 thru 27169 thru 47746 17247747 thru 17265684 F172-0001 thru F172-0654 F17200655 thru F17201384 FR17200001 thru FR17200569 P17257120 thru P17257188 FP172-0001 thru FP172-0003 55001 thru 56777 17556778 thru 17557119 17700001 thru 17702752 177RG0001 thru 177RG1366 F177AG0001 thru F177RG0177 30000 thru 50911 18050912 thru 18053203 thru 53007 18253008 thru 18268434 A182-0001 thru A182-0146 F18200001 thru F18200169 R18200001 thru R18201999 FR18200001 thru FR18200070 185-0001 thru 185-1599 18501600 thru 18504424 188-0446 thru 188-0572 18800573 thru 18803296 thru F15001248 SEB92-27 Page 1 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. Cessna The Casino Aircraft Compony Customer Services PO Box 7706 Wichita, Kansas 67277 USA. 316-941-7550 TELEX 4319022 FAX 316-942-9006 186 MODEL SERIES YEAR 1972 thru 1978 205 206 1963 thru 1964 1964 P206/TP206 P206/TP206 U206/TU206 1965 thru 1969 1970 1965 thru 1969 U206/TU206 1970 thru 1984 207/T207 210 1969 thru 1984 1960 210 T210 1961 thru 1966 1966 SERIAL NUMBERS 18800967 thru 18803296T 205-0001 thru 205-0577 206-0001 Ihru 206-0275 P206-0001 thru P206-0603 P20600604 thru P20600647 U206-0276 thru U206-1444 U20601445 thru U20606846 20700001 thru 20700788 thru 57575 thru 21058818 thru T210-0197 57001 21057576 T210-0001 PURPOSE To provide a modification for replacing flush and/or non-vented type fuel caps with new raised reduced diameter vented style fuel caps. The new cap is designed to assist in preventing water from entering into the fuel tank through the fuel filler ports and to provide secondary venting capabilities for each tank. The new cap and fuel filler port adapters are of the reduced diameter type to assist in preventing the airplane from being misfueled with turbine jet fuel. Airplanes that are equipped with a turbocharger and have external placards that identify the airplane as turbocharger equipped ("Turbo System" or "Turbo Centurion", etc.) shall have these placards removed to assist in preventing these airplanes from being misfueled with turbine jet fuel. Careful preflight inspection of the primary fuel vent(s) is required to assure a properly functioning vent system. Any indication of fuel vent system blockage shall be investigated and the cause corrected before next flight. Some symptoms of vent system blockage are: inability of air to pass through the vent line, fuel lank "oil-canning" in flight or immediately after flight, sudden in-rush of air when the fuel cap is removed or loss of fuel tank capacity. With the airplane on a level surface, fuel samples from each fuel drain shall be taken during each preflight inspection to verify that the airplane has been serviced with the correct aviation fuel and that no water or other contaminants are present. Water, contaminants and or unidentifiable fuel shall be removed from the fuel systern before flight. Failure to verify that the airplane has been serviced with the proper type/grade of aviation fuel, and that fuel tank vent(s) are not obstructed, and failure to remove all fuel contaminants before flight may result in loss of engine power or engine stoppage in flight. COMPLIANCE Mandatory; shall be accomplished within the next 400 hours of operation or 12 months, whichever occurs first. This Service Bulletin supersedes: Single Engine Service Letter SE77-6 and SE77-6 Revision 1: Vented Fuel Caps. Single Engine Service Information Letter SE84-16 and SE84-16 Revision 1: Fuel Filler Diameter Modifica- tion And External Turbo Placard Removal. 1. It SE77-6, SE77-6 Revision 1 or FAA AD79-10-14R1 has previously been accomplished by installing C156003-0101 vented fuel caps, compliance with this Service Bulletin is not required for the following airplanes. All serial numbers listed in the Effectivity section of this Service Bulletin for models 140, 150, A150, F150, FA150, FRA150, 170, 172, F172, P172, FP172, FR172, 175 and 180 serials 30000 thru 50448 and 182 serials 33000 thru 51825. Page 2 SEB92-27 September 4, 1992 2. If SE84-16 or SE84-16 Revision 1 has previously been accomplished by installing the appropriate Service Kit, SK177-39, SK177-40, SK182-85, SK182-86 (or later revision) and all external placards identifying the airplane as turbocharged have been removed, compliance with this Service Bulletin is not required for the following airplanes: All serial numbers listed in the Effectivity section of this Service Bulletin for models A182, F182, FR182, 185, 188, 205, 206, P206, U206, 207, 210, T210 and 180 serials 50449 thru 18053203, 182 serials 51826 thru 18268434. 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. 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) SK182-858 (See Note 1&2) SK182-86C (See Note 1) C156003-0101 (See Note 3&5) 0709115-2 (See Note 4) 000001 (See Note 3) $2608-1 (See Note 5) CMNP022CLASSB1/2 (Alternate PR1403G-B1/2) (See Note 1) CMNP021CLASSB1/2 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 Fuel Cap Cover Door " Avgas Placard GAMA (80, 100LL, 100) Avgas Placard - GAMA (100LL, 100) Sealant (6 Oz. Semkit) Sealant (Alternate MILS88021B1/2) (2.5 Oz. Semkit) (See Note 3&5) QTY./ AIRPLANE PRICE $ 115.00 (X) ea. S 112.00 (X) ea S 144.00 (X) ea. * $ 95.80 (X) ea. * $ 25.90 (X) ea. $ 25.50 (X) ea N 2.30 (PS) ea. 1,50 (PS) ea. $ 27.30 (X) ea. $ 20.90 (X) ea. NOTE 1: Refer to the attached Fuel Cap Modification Service Kits installation instructions for appli- cable airplane model and serials. 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 448 and 182 serials 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, serials 30000 thru 50448 and 182 serials 33000 thru 51825: P172, F FP172, FR172, 175, 180 A. B. 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. 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. C. 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. CREDIT Service Kits SK177-39D, SK177-40D, SK182-85B and SK182-86C Fuel Cap Modification installation instructions are attached. 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 SEB92-27 September 4, 1992 CEMENT Cessna Revision Transmittal September 4, 1992 TO: CESSNA DISTRIBUTORS AND SINGLE E ENGINE SERVICE STATIONS SUBJECT: Service Bulletin SEBB9-2 Revision 2, Pilot ilot Seat Secondary Stop Installation REASON FOR REVISION To revise the Credit section to extend the credit ending date. To revise the Compliance section to change the compliance from Recommended to Mandatory. To revise other sections as required to accommodate the additional information and changes. REQUIRED ACTION Please replace your copy of SEB89-2 Revision 1 with the attached copy of SEB89-2 Revision 2 which is printed in its entirety. NOTE: A. B. For airplanes that have been modified per the original issue, or revisions A or B to the following Service Kits; SK180-37, SK185-30, SK185-32, SK185-36, SK185-38, SK185- 40, SK185-42 or SK185-44. Compliance with Revision 2 is required by accomplishing an inspection to determine the maximum amount of seat travel. For all other airplanes on which SEB89-2 or SEB89-2 Revision 1 has previously been accomplished, compliance with SEB89-2 Revision 2 is not required. LOG OF EFFECTIVE PAGES Page No. Date 1 2 September 4, 1992 September 4, 1992 September 4, 1992 September 4, 1992 September 4, 1992 Page 1 of 1 To obtain satisfactory results; procedures specified in this publication must be accomplished in accordance with accepted methods and prevailing government requations. The Cessna Aircraft Company cannot be responsible for the quality of work performed in accomplishing the requirements of the publication The Cessna Aircraft Company Product Support PO Box 7706 Wichita, Kansas 67277, USA (316) 941-7550, Telek 4319022, Facsimile (216) 942-9000 COPYRIGHT © 1992 2.1316/941 CESSNA SAFETY ENHANCEMENT PROGRAM SINGLE ENGINE SERVICE BULLETIN September 4, 1992 TITLE PILOT SEAT SECONDARY STOP INSTALLATION SEB89-2 Revision 2 EFFECTIVITY All Model 170 thru 185 and 205 thru P210 Series Single Engine Piston Airplanes, Normally Aspirated and Turbocharged Models. Refer to the Compliance section for affected airplanes and serial numbers. PURPOSE To provide a modification for installing a secondary seat stop on the pilot seat. The secondary seat stop is designed to assist in providing an additional margin of safety by limiting the aft travel of the seat in the event the primary latch pin is not properly engaged in the seat rail track. Seat slippage could result in the pilot not being able to reach all the controls and subsequently losing control of the airplane. COMPLIANCE Mandatory: shall be accomplished within the next 400 hours of operation or 12 months, whichever occurs first. NOTE: A B. For airplanes that have been modified per the original issue, or revisions A or B to the following Service Kits: SK180-37, SK185-30, SK185-32, SK185-36, SK185-38, SK185-40, SK185-42 or SK185-44. Compliance with Revision 2 is required by accomplishing an inspection to determine the maximum amount of seat travel. For all other airplanes on which SEB89-2 or SEB89-2 Revision 1 has previously been accomplished, compliance with SEB89-2 Revision 2 is not required. Affected Airplanes and Serial Numbers SERIAL NUMBERS MODEL YEAR 170-18000 thru 1708-27169 1948 thru 1956 172-28000 thru 17276673 F172-0001 thru F17202254 FP172-0001 thru FP172-0003 FR17200001 thru P17257120 thru P17257188 R172-0001 thru R1723454 FR17200675 1956 thru 1986 1963 thru 1986 1963 Only 1968 thru 1981 1963 Only 1967 thru 1981 172AG0001 thru 172RG1191 175-55001 thru 17557119 1980 thru 1985 1958 thru 1962 Revision 1 Issue: October 26, 1990 Original Issue: April 14, 1989 Page 1 of 5 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. Cessna The Cessna Aircraft Company Customer Services PO Box 7705 Wichita, Kansas 67277 USA 316-941-7550 TELEX 4319022 & FAX 316-942-9006