# Cessna Service Bulletin SEB01-1: Revision 1 - Rights: © Textron Aviation Inc. Filed by the FAA in regulations.gov docket FAA-2007-27747; AD 2009-10-09, 2009-10-09 R1, 2009-10-09 R2 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication. - Document: [Cessna Service Bulletin SEB01-1](https://openairdocs.org/service-documents/cessna/seb01-1.md) - Title as filed: U.S. DOT/FAA - Service Information - SEB01-1 - Pages: 4 - PDF: https://openairdocs.org/files/sha256/2b/b5/2bb50159ab4afcb903ebf9046ab0c5531294a29831a7483626a9906787ef9e02 - Page: https://openairdocs.org/service-documents/cessna/seb01-1/file/2bb50159ab4a ## Text This text is OCR from a scan. OCR can misread letters and numbers. Each page's text from the PDF; open the PDF at a page with #page=N. ### Page 1 (OCR) ATTACH Single Engine Cessna A Textron Company Service Bulletin January 22, 2001 SEB01-1 TITLE RUDDER STOP MODIFICATION EFFECTIVITY: Model Series Year Serial Numbers 150F 1966 15061533 thru 15064532 150G 1967 15064533 thru 15064969 150G 1967 15064971 thru 15067198 150H 1968 15067199 thru 15069308 150H 649 150J 1969 15069309 thru 15071128 150K 1970 15071129 thru 15072003 150L 1971 15072004 thru 15072628 150L 1972 15072629 thru 15073658 150L 1973 15073659 thru 15074850 150L 1974 15074851 thru 15075781 150M 1975 15075782 thru 15077005 150M 1976 15077006 thru 15078505 150M 1977 15078506 thru 15079405 A150K 1970 A1500001 thru A1500226 A150L 1971 A1500227 thru A1500276 A150L 1972 A1500277 thru A1500342 A150L 1973 A1500343 thru A1500429 A150L 1974 A1500430 thru A1500432 A150L 1974 A1500434 thru A1500523 A150M 1975 A1500524 thru A1500609 A150M 15064970 A150M 1976 A1500610 thru A1500684 A150M 1977 A1500685 thru A1500734 152 1978 15279406 thru 15282031 152 1979 15282032 thru 15283591 152 1980 15283592 thru 15284541 152 1981 15284542 thru 15285161 152 1982 15285162 thru 15285594 152 1983 15285595 thru 15285833 152 1984 15285834 thru 15285939 152 1985 15285940 thru 15286033 Page 1 of 4 To obtain satisfactory results, procedures specified in this publication must be accomplished in accordance with accepted methods and prevailing goverment regulations. Cessna Aircraft Company cannot be responsible for the quality of work performed in accomplishing the requirements of this publication. Cessna Aircraft Company, Product Support, P.O. Box 7706, Wichita, Kansas B7277, U.S.A. (316) 517-5800 Facsimile (316) 942-9006 COPYRIGHT®2001 ### Page 2 (OCR) Model Series Year Serial Numbers A152 1978 A1520735 thru A1520808 A152 A1500433 A152 1979 A1520809 thru A1520878 A 152 681 A 152 1980 A1520879 thru A1520943 A 152 1981 A1520944 thru A1520983 A152 1982 A1520984 thru A1521014 A 152 1983 A1521015 thru A1521025 A152 1984 A1521026 thru A1521027 A152 1985 A1521028 thru A1521049 A-150L 1972 thru 1973 A-1501001 thru A-1501039 A-A150L 1972 thru 1973 A-A1500001 thru A-A1500009 F150F 1966 F150-0001 thru F150-0067 F150G 1967 F150-0068 thru F150-0219 F150H 1968 F150-0220 thru F150-0389 F150J 1969 F150-0390 thru F150-0529 F150K 1970 F15000530 thru F15000658 F150L 1971 F15000659 thru F15000738 F150L 1972 F15000739 thru F15000863 F150L 1973 F15000864 thru F15001013 F150L 1974 F15001014 thru F15001143 F 150M 1975 F15001144 thru F15001248 F150M 1976 F15001249 thru F15001338 F150M 1977 F15001339 thru F15001428 FA150K 1970 FA1500001 thru FA1500081 FA150L 1971 FA1500082 thru FA1500120 FA150L 1972 FA1500121 thru FA1500166 FA150L 1973 FA1500167 thru FA1500211 FA150L 1974 FA1500212 thru FA1500261 FA150M 1975 FA1500262 thru FA1500281 FA150M 1976 FA1500282 thru FA1500311 FA150M 1977 FA1500312 thru FA1500336 F152 1978 F15201429 thru F15001528 F152 1979 F15201529 thru F15201673 F152 1980 F15201674 thru F15201808 F152 1981 F15201809 thru F15201893 F152 1982 F15201894 thru F15201928 F152 1983 F15201929 thru F15201943 F152 1984 F15201944 thru F15201952 F152 1985 F15201953 thru F15201965 F152 1986 F15201966 thru F15201980 FA152 1978 FA1520337 thru FA1520347 FA152 1979 FA1520348 thru FA1520357 FA152 1980 FA1520358 thru FA1520372 FA152 1981 FA1520373 thru FA1520377 FA152 1982 FA1520378 thru FA1520382 Page 2 SEB01-1 January 22, 2001 ### Page 3 (OCR) Model Series Year Serial Numbers FA152 1983 FA1520383 thru FA1520387 FA152 1985 FA1520388 thru FA1520415 FA152 1986 FA1520416 thru FA1520425 PURPOSE To provide an enhanced rudder stop, bumper, doubler and attachment hardware designed to assist in preventing the possibility of the rudder overriding the stop bolt during full left and/or right operation of the rudder. COMPLIANCE Mandatory; within the next 100 hours of operation or 12 months, whichever occurs first. 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 4.0 man-hours to install SK152-24 or SK152-25. MATERIAL The following parts are available from Cessna Parts Distribution through an appropriate Cessna Service Station for the suggested list price shown. Part Number Description Qty/Airplane Price SK152-24 Rudder Stop $ 67.60 (A) ea. Modification Kit (Sheet metal Bulkhead) SK152-25 Rudder Stop $ 54.20 (A) ea. Modification Kit (Forged Bulkhead) ALL PRICES SUBJECT TO CHANGE WITHOUT NOTICE Page 3 SEB01-1 January 22, 2001 ### Page 4 (OCR) ACCOMPLISHMENT INSTRUCTIONS Change In Weight And Balance Negligible SK152-24 and SK152-25 instructions are attached. NOTE: This information shall be considered an amendment to the Cessna Manufacturer's Service/Maintenance Manual or Instructions for continued airworthiness, and must be accomplished for ongoing airworthiness compliance as required per FAR43.13. CREDIT Not applicable OWNER NOTIFICATION On January 22, 2001 the following Owner Advisory message will be sent to applicable owners of record in SEB01-1A. Dear Cessna Owner: This Owner Advisory is to inform you that Cessna has issued Service Bulletin SEB01-1 which provides a modification for the rudder stop on your airplane. This modification provides an enhanced rudder stop, bumper, doubler and attachment hardware designed to assist in preventing the possibility of the rudder overriding the stop bolt during full left and/or right operation of the rudder. Compliance is mandatory: shall be accomplished within the next 100 hours of operation or 12 months, whichever occurs first. The information contained in the referenced Cessna Service Bulletin shall be considered an amendment to the Cessna Manufacturer's Service/Maintenance Manual or Instructions for continued airworthiness, and must be accomplished for ongoing airworthiness compliance as required per FAR43.13. Please contact a Cessna Single Engine Service Station for detailed information and arrange to have Cessna Service Bulletin SEB01-1 accomplished on your airplane. * * Page 4 SEB01-1 January 22, 2001 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain, except the copies of manufacturers’ service documents, which belong to their rights holders.