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Single Engine Cessna A Textron Compan Service Bulletin March 22, 2011 SEB01-1 Revision 1 TITLE
RUDDER STOP MODIFICATION
EFFECTIVITY Model Serial Numbers 150 15061533 thru 15079405 150 649 A150 A1500001 thru A1500734 A150 15064970 152 15279406 thru 15286033 A152 A1500433 A152 A1520735 thru A1521049 A152 681 F150 F150-0001 thru F150-0529 F150 F15000530 thru F15001428 FA150 F1500001 thru F1500336 FRA150 FRA1500121 thru FRA1500336 F152 F15201429 thru F15201980 FA152 FA1520337 thru FA1520425 A-150 A-1501001 thru A-1501039 A-A150 A-A1500001 thru A-A1500009
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.
Original Issue: January 22, 2001 Page 1 of 3 To obtain satisfactory results, procedures specified in this publication must be accomplished in accordance with accepted methods and prevailing government regulations. Cessna Aircraft Company cannot be responsible for the quality of work performed in accomplishing the requirements of this publication.
Cessna Aircraft Company, Customer Service, P.O. Box 7706, Wichita, Kansas 67277, U.S.A. (316) 517-5800, Facsimile (316) 517-7271 www.cessnasupport.com COPYRIGHT © 2001
COMPLIANCE Mandatory; Shall be accomplished within the next 100 hours of operation or 12 months, whichever occurs first.
NOTE: Compliance with SEB01-1 Revision 1 is not required if in compliance with the Original Issue.
APPROVAL FAA approval has been obtained on technical data in this publication that affects airplane type design.
MAN-HOURS
• Approximately 4.0 man-hours to install SK152-24B or SK152-25B.
MATERIAL Authorized Service Facility: The following parts are available from Cessna Service Parts and Programs through an appropriate Cessna Part Number Description Qty/Airplane SK152-24B Rudder Stop Modification Kit (Sheet metal 1 Bulkhead) SK152-25B Rudder Stop Modification Kit (Forged Bulkhead) 1
ACCOMPLISHMENT INSTRUCTIONS Change In Weight And Balance Negligible
• SK152-24B and SK152-25B 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.
Page 2 SEB01-1 Revision 1 March 22, 2011
CREDIT Not applicable
OWNER NOTIFICATION A. On January 22, 2001 the following Owner Advisory message was sent to applicable owners of record in SEB01-1A.
Dear Cessna Single Engine Legacy 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.
B. On March 22, 2011 the following Owner Advisory message will be sent to applicable owners of record in SEB01-1AR1.
Dear Cessna Owner:
This Owner Advisory is to inform you that Cessna has issued Service Bulletin SEB01-1 Revision 1 Rudder Stop Modification, 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.
NOTE: Compliance with SEB01-1 Revision 1 is not required if in compliance with the Original Issue.
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.
Cessna Service Bulletin SEB01-1 Revision 1 accomplished on your airplane. Please contact a Cessna Single Engine Authorized Service Facility for detailed information and arrange to have SEB01-1 Revision 1 March 22, 2011 Page 3