Single Engine Service Bulletin SEB01-1 Revision 2
CESSNA F-152 · Service Bulletins
Overview
This document is a service bulletin for the Cessna F-152 aircraft, specifically addressing the Rudder Stop Modification. It outlines the necessary updates, compliance requirements, and installation instructions for enhancing the rudder stop to prevent potential issues during operation.
- Mandatory compliance during the next 100-hour or 12-month inspection.
- Updates include new service kit numbers and labor hour estimates.
- Revision C introduces corrosion protection measures.
- Installation requires approximately 10.0 man-hours.
- Contact a Textron Aviation Authorized Service Facility for parts.
- The bulletin applies to specific model serial numbers.
- Cessna cannot guarantee the quality of work performed.
- Service documents are available online for customers.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Reference only, not for flight. Use the current approved manual for your aircraft. See terms, section 5.
Document
Source
Copy found at cessnaowner.org. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Service Bulletins
- Year ·
- 2020
- File size ·
- 143 KB
- Copy found at ·
- cessnaowner.org
- Language ·
- en
Specifications & performance
Extracted from this document.
Weight & balance
- Change in weight and balance ·
- Negligible
What is the Single Engine Service Bulletin SEB01-1 Revision 2?
The Single Engine Service Bulletin SEB01-1 Revision 2 is a service bulletins for the CESSNA F-152, dated 2020.
What year was the Single Engine Service Bulletin SEB01-1 Revision 2 published?
The Single Engine Service Bulletin SEB01-1 Revision 2 — the CESSNA F-152 service bulletins on file — is dated 2020.
Common. More common than 99% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the CESSNA F-152.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
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In this document
Purpose
To provide an enhanced rudder stop, bumper, doubler, and attachment hardware to prevent the rudder from overriding the stop bolt.
Compliance
Mandatory compliance is required during the next scheduled inspection, not to exceed 100 hours or 12 months.
Labor-Hours
Approximately 10.0 man-hours are estimated for the installation of the modification kits.
Material
Contact a Textron Aviation Authorized Service Facility for current cost and availability of parts.
Effectivity
The bulletin applies to various model serial numbers of the Cessna 150 and 152 series.
Approval
FAA approval has been obtained on technical data affecting airplane type design.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Safety notes
- Cessna cannot be responsible for the quality of work performed.
- Compliance with SEB01-1 Revision 2 is not required if already compliant with the Original Issue or Revision 1.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Full document text
Revision Transmittal September 17, 2020 SUBJECT: Single Engine Service Bulletin SEB01-1 Revision 2, Rudder Stop Modification REASON FOR REVISION Updates the service kit numbers. Updates the estimate of labor hours. Editorial edits to Effectivity to arrange models. NOTE: Compliance with SEB01-1 Revision 2 is not required if in compliance with the Original Issue or Revision 1. NOTE: Revision C to SK152-24 and SK152-25 have extensive changes and updated process for corrosion protection with the addition of: • sealant during installation of the bumpers and rudder horn. • color chemical film treatment, corrosion resistant primer, polyurethane paint and corrosion inhibiting compound coating to the bumpers and rudder horn. REQUIRED ACTION Please replace any previous copy of SEB01-1 with a copy of SEB01-1 Revision 2. LOG OF REVISIONS Original Issue January 22, 2001 Revision 1 March 22, 2011 Revision 2 September 17, 2020 * * * * * * * Page 1 of 1 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 © 2020 Single Engine Service Bulletin September 17, 2020 SEB01-1 Revision 2 TITLE RUDDER STOP MODIFICATION EFFECTIVITY Model Serial Numbers 150 649, 15061533 thru 15079405 A150 A1500001 thru A1500734, 15064970 A–150 A-1501001 thru A-1501039 A-A150 A-A1500001 thru A-A1500009 F150 F150-0001 thru F150-0529, F15000530 thru F15001428 FA150 FA1500001 thru FA1500336 FRA150 FRA1500121 thru FRA1500336 152 15279406 thru 15286033 A152 681, A1500433, A1520735 thru A1521049 F152 F15201429 thru F15201980 FA152 FA1520337 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. Revision C of SK152-24 and SK152-25 provides added instructions to assemble the rudder stop with corrosion resistant primer, Type X sealant and corrosion inhibiting compound. Original Issue: January 22, 2001 Revision 2: September 17, 2020 Page 1 of 2 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. This service document must be accomplished at the next 100-hour or 12-month (annual-type) inspection. APPROVAL FAA approval has been obtained on technical data in this publication that affects airplane type design. LABOR-HOURS For planning purposes only: Approximately 10.0 man-hours to install SK152-24C or SK152-25C. MATERIAL Please contact a Textron Aviation Authorized Service Facility for current cost and availability of parts listed in this service document. Part Number Description Qty/Airplane SK152-24C Rudder Stop Modification Kit (Sheet metal Bulkhead) 1 SK152-25C Rudder Stop Modification Kit (Forged Bulkhead) 1 ACCOMPLISHMENT INSTRUCTIONS Change In Weight And Balance Negligible Refer to SK152-24C and SK152-25C for installation instructions. * * * * * * * SEB01-1 Revision 2 Page 2 September 17, 2020 Owner Advisory September 17, 2020 SEB01-1OAR2 Dear Cessna Model 150 and 152 Series Aircraft Owner This Owner Advisory is to inform you that SEB01-1 Revision 2, Rudder Stop Modification has been issued. SEB01-1 Revision 2 updates the Labor Hours and references Revision C for SK152-24 and SK152-25. NOTE: Revision C of SK152-24 and SK152-25 provides added instructions to assemble the rudder stop with corrosion resistant primer, Type X sealant and corrosion inhibiting compound. Please contact a Textron Aviation Authorized Service Facility for detailed information and arrange to have SEB01-1 Revision 2 accomplished on your airplane. COMPLIANCE Mandatory: Shall be accomplished during the next scheduled inspection, not to exceed the next 100 hour or annual / 12 month inspection, whichever occurs first. LABOR-HOURS For planning purposes only: Approximately 10.0 man-hours to install SK152-24C or SK152-25C. WARRANTY Not applicable 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 www.txtavsupport.com to register. Page 1 of 1 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 © 2011