Cessna C-152: SID: 27-20-01 Rudder Pedal Torque Tube Inspection: 27-30-01 Elevator Trim Pulley Bracket and Actuator Bracket Structure Inspection: 55-10-01 Horizontal Stabilizer, Elevators and Attachments Inspection: 55-11-02 Vertical Stabilizer Attach Bracket and Horizontal Stabilizer Rear Spar Attachment Inspection

(vi) Cessna Aircraft Company Model 100 Series (1963-1968) Service Manual, Supplemental Inspection Number: 55-10-01, D637-1-13 Temporary Revision Number 9, dated December 1, 2011. (vii) Cessna Aircraft Company Model 180/185 Series (1969-1980) Service Manual, Supplemental Inspection Number: 55-10-01, D2000-9-13 Temporary Revision Number 7, dated

Applicability: Cessna 100 and 200 Series aeroplanes, all types, models Cessna Supplemental Inspection Document (SID) 55-10-01: Remarks: Comments regarding this safety information should be referred to the Safety Information Section, Certification Directorate, EASA; E-mail: ADs [at] easa.europa [dot] eu The FAA recommends performing the inspections that are outlined in the Cessna supplemental inspection document (SID) 55-10-01, a copy of which can be found here.If either worn or incorrect hardware is found, the agency further recommends replacing it according to the instructions provided in the SID. This instrument applies to any single engine Cessna Aircraft Company (Cessna) aircraft to which any of the following Cessna documents apply: (a) Service Bulletin SEB03-1 or SB 02-55-01 “Elevator Rivet Installation” as referenced in Supplemental Inspection Document ( SID ) 55-10-01; Cessna C-152: SID: 27-20-01 Rudder Pedal Torque Tube Inspection: 27-30-01 Elevator Trim Pulley Bracket and Actuator Bracket Structure Inspection: 55-10-01 Horizontal Stabilizer, Elevators and Attachments Inspection: 55-11-02 Vertical Stabilizer Attach Bracket and Horizontal Stabilizer Rear Spar Attachment Inspection The SAIB was issued based on a service difficulty report of an elevator hinge bolt backing out on a C-150. The FAA recommends performing the inspections detailed in the Cessna supplemental inspection document (SID) 55-10-01. Both the SAIB and the SID(s) can be found here. Note The regulations require maintenance to be carried out in accordance with other Cessna documents that apply to the relevant aircraft, including the following documents, as existing from time to time: (a) SID 55-10-01 Horizontal Stabilizer, Elevators and Attachments; (b) SID 53-12-01 Fuselage Lower Doorpost and Strut Fitting. with Cessna Customer Service prior to beginning the repair.

(viii) Cessna Aircraft Company Model 180/185 Series (1981-1985) Service Manual, Supplemental Inspection Number: 55-10-01, D2067-1-13 Temporary Revision Number 7, dated December 1, 2011. (i) Alternative Methods of Compliance (AMOCs) CESSNA AIRCRAFT COMPANY MODEL 180/185 SERIES (1981 - 1985) SERVICE MANUAL SUPPLEMENTAL INSPECTION NUMBER: 55-10-01 1. TITLE: Horizontal Stabilizer, Elevators and Attachments Inspection 2. EFFECTIVITY 18053168 thru 18053203 18504139 thru 18504448 INSPECTION COMPLIANCE ALL USAGE: INITIAL 5,000 Hours or 20 Years (NOTE) REPEAT 2,000 Hours or 5 TEMPORARY REVISION NUMBER 5 DATED 1 DECEMBER 2011 MANUAL TITLE Model 152 Series 1978 Thru 1985 Service Manual MANUAL NUMBER - PAPER COPY D2064-1-13 TEMPORARY REVISION NUMBER D2064-1TR5 MANUALDATE 7 February 1985 REVISION NUMBER 1 DATE 2 October 1995 This Temporary Revision consists of the following pages, which add to existing pages in the paper copy … 2012-05-24 Cessna 100 SIDs compliance extension for private operators Cessna 100 series aircraft owners have an extra two years to complete the special structural inspection program developed by Cessna. The extension applies to the Supplemental Inspection Document - or SIDs - requirements for Cessna 100 series aircraft used in private operations. Cessna 100 series aircraft SIDs must begin at the next 2017-05-15 Cessna Supplemental Inspection Document (SID) 55-10-01: Remarks: Comments regarding this safety information should be referred to the Safety Information Section, Certification Directorate, EASA; E-mail: ADs [at] easa.europa [dot] eu 2012-11-10 2017-05-15 The FAA recommends performing the inspections detailed in the Cessna supplemental inspection document (SID) 55-10-01. If worn or incorrect hardware is found, it should be replaced according to the instructions in the SID. I am an aviation attorney representing several owners of Conquest aircraft that are deeply concerned about the SID program adopted by Cessna and your interpretation of it being mandatory in your Info Memorandum if the owner had not selected a maintenance program in their maintenance log prior to August 31, 2007.

Applicability: Cessna 100 and 200 Series aeroplanes, all types, models Cessna Supplemental Inspection Document (SID) 55-10-01: Remarks: Comments regarding this safety information should be referred to the Safety Information Section, Certification Directorate, EASA; E-mail: ADs [at] easa.europa [dot] eu The FAA recommends performing the inspections that are outlined in the Cessna supplemental inspection document (SID) 55-10-01, a copy of which can be found here.If either worn or incorrect hardware is found, the agency further recommends replacing it according to the instructions provided in the SID. This instrument applies to any single engine Cessna Aircraft Company (Cessna) aircraft to which any of the following Cessna documents apply: (a) Service Bulletin SEB03-1 or SB 02-55-01 “Elevator Rivet Installation” as referenced in Supplemental Inspection Document ( SID ) 55-10-01; Cessna C-152: SID: 27-20-01 Rudder Pedal Torque Tube Inspection: 27-30-01 Elevator Trim Pulley Bracket and Actuator Bracket Structure Inspection: 55-10-01 Horizontal Stabilizer, Elevators and Attachments Inspection: 55-11-02 Vertical Stabilizer Attach Bracket and Horizontal Stabilizer Rear Spar Attachment Inspection The SAIB was issued based on a service difficulty report of an elevator hinge bolt backing out on a C-150.

intervals that have calendar time specified. Read Note 1 in section 2A-14-00 of SIDs document for details. 7. Cessna SIDs compliance Plan - Example words for Log Book Statement: In accordance with all the requirements contained in Schedule 1 of CASA Instrument EX96/16, this aircraft is approved for SIDs extension beyond 30 June 2016.

The SID inspections have been incorporated into the affected Maintenance/Service Manuals. SID 55-10-01; o Service Bulletin SEB 05-2 “Fuselage skin & Fuel Step All remaining Cessna SID inspections must be completed prior to 30 June 2018. Thereafter comply with, as required, Cessna Corrosion Prevention and Control Program (CPCP) and Cessna SID’s Cessna SID Implementation in New Zealand – Mandatory compliance – 90 to 95% of inspected airplanes required maintenance action – 20% of those which required action needed major repair – 80% of the findings were corrosion and 20% cracking – Most (SID 55-10-01) Case Study – Cessna 210 Cessna Distributors, Single Engine Authorized Service Facilities, and affected Owners of Record 55-10-01 Horizontal Stabilizer Aft Attach Bracket X X X X The SID inspections have been incorporated into the affected Maintenance/Service Manuals.

2009-08-23 · The Cessna SID program goes back a few years as you mention below and Cessna is working on developing SID programs for most of their fleet. For the majority of operators complying with Cessna SIDs is not mandatory. The recent issue with the C-425/441 SID surrounded the fact that those aircraft fall under FAR 91.409(e) and (f) and have to be on

ALL USAGE: INITIAL 10,000 Hours or 20 Years (NOTE). REPEAT 3,000 Hours or 5 Years (NOTE) NOTE: Refer to Note 1, Section 5-14-00.. 3. PURPOSE Model 182S/182T/T182T Maintenance Manual (Rev 20) 5-14-11-0 (Rev 18) SUPPLEMENTAL INSPECTION NUMBER: 55-10-01. 1.

Coordinate this inspection with SID 55-30-01, Vertical Stabilizer, Rudder and Attachments Inspection. D2070-3-13 Temporary Revision Number 10 - Aug 1/2011 2A-14-12 Page 2 For Cessna 100 airplanes and Cessna 208/208B airplanes, we recommend adherence to the applicable Textron Aviation SIDs and maintenance manuals for corrosion inspections. Airplanes based or operated in high corrosion areas are recommended to be inspected more frequently.
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SID’s, of course, are the industry’s way of addressing the aging GA aircraft fleet.

2 Buyers should plan to deduct $150,000 to $200,000 if the airplane has not had Cessna’s “mandatory” supplemental inspection document (SID) checks done. Cessna modified its maintenance manual in 2007 to incorporate the SID, which required numerous additional maintenance phases, a large group of which must be accomplished all at once to kick off the program.
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All remaining Cessna SID inspections must be completed prior to 30 June 2018. Thereafter comply with, as required, Cessna Corrosion Prevention and Control Program (CPCP) and Cessna SID’s (for REPEAT compliance) requirements. I, _, being the registered owner responsible for VH-_ confirm

The new Supplemental Inspection Documents (SID's) have been released by Cessna for the C336/C337 Skymaster and have been incorporated in the Maintenance Manual. These SID's are not mandatory in the US for Part 91 operations but could affect other commercial operations and most jurisdictions outside of the US could enforce the procedures. 2012-11-10 · SID 32-20-01 Nose Gear Torque Link Bolt and Fork Inspection Type of Inspection – Visual and Eddy Current. Initial Compliance:3000 hours or 5 years. Recurring Compliance: 3000 hours or 5 years. Approximate Labor Time – 2 hours. I used to feel the nose gear was a weak link in the Cessna single engine airframe design.

All remaining Cessna SID inspections must be completed prior to 30 June 2018. Thereafter comply with, as required, Cessna Corrosion Prevention and Control Program (CPCP) and Cessna SID’s (for REPEAT compliance) requirements. I, _____, being the registered owner responsible for VH-_____ confirm

All remaining Cessna SID inspections must be completed prior to 30 June 2018. Thereafter comply with, as required, Cessna Corrosion Prevention and Control Program (CPCP) and Cessna SID’s (for REPEAT compliance) requirements. I, _, being the registered owner responsible for VH-_ confirm