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TITLE: Horizontal Stabilizer, Elevators and Attachments Inspection 2. EFFECTIVITY 15069309 thru 15078505, F15000390 thru F15001338, A15000001 thru A1500684, FA15000001 thru FA1500120, FRA1500121 thru FRA1500311 INSPECTION COMPLIANCE Cessna Distributors, 55-10-01 Horizontal Stabilizer Attachment The SID inspections have been incorporated into the affected Maintenance/Service Manuals. 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 Cessna SID into the AMP, careful consideration should be given to the potential airworthiness and safety consequences of this course of action. Any decision not to incorporate the applicable Cessna SID should be properly substantiated, to the satisfaction of the competent authority, or the CAMO in case of indirect approval of the AMP. 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.

Cessna sid 55-10-01

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Horizontal Stabilizer Attachment Inspection. Aug 16, 2013 Supplemental Inspection Number 55-10-01 directly related to the Cessna, that means the SID and CPCP, if available, unless you can show  Dec 7, 2017 Send completed form/attachments to Cessna Structures at csstructures@txtav. com. 23.

Now Cessna have said that CASA was optimistic and have reduced it back to 6500 hours (SID 57-10-08) so he still has 3500 hours to go. At his current rate that's another 20 years or so! There is no year life on the spar. Cessna Single Engine Airplanes 145,000 produced between 1946-1986 Average age is 42 years old Made of aluminum Certified CAR 3 2.

Cessna sid 55-10-01

2. EFFECTIVITY • 17280001 and On, 172S8001 and On.. INSPECTION COMPLIANCE. 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 SUPPLEMENTAL INSPECTION NUMBER: 55-10-01. 1.

Cessna sid 55-10-01

(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.
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The maintenance records  (a) SID 55-10-01 Horizontal Stabilizer, Elevators and Attachments;. (b) SID 53-12 -01 Fuselage Lower Doorpost and Strut Fitting. SID means a Cessna Aircraft  May 15, 2017 operators of some Cessna 150 and Cessna 152 airplanes about the the Cessna supplemental inspection document (SID) 55-10-01," and  Feb 1, 2018 During NDT inspection IAW AD/CESSNA 400/103, delamination was a new item; SIDs inspections 55-30-01 and 55-10-01 were carried out  CESSNA AIRCRAFT COMPANY MODEL 100 SERIES (1963 - 1968) SERVICE 1 ALL Inspect aircraft records to verify that all SID Inspections have been Refer to Section 2A-14-19, Supplemental Inspection Document 55-10-01, for  May 15, 2017 Cessna 150 landing - FAA issues SAIB CE-17-12 regarding C150, the Cessna supplemental inspection document (SID) 55-10-01, a copy of  Oct 31, 2018 AD/CESSNA 210/61 Amdt 2 OPS 28 SID 57-30-01 WING FRONT SPAR INSPECTION - EDDY CURRENT OPS 09 SID 55-10-01 HOR. CHANGE 34 TO THE BASIC MANUAL INCORPORATES THE 414 AND 414A SUPPLEMENTAL INSPECTION DOCUMENTS (SID'S), DATED 1 AUGUST 2002   Feb 3, 2012 The Twin Cessna owners are probably familiar with the idea of SIDs, but the single engine crowd has been spared the trouble….. until now. The  SUPPLEMENTAL INSPECTION NUMBER: 55-10-01 .

Approximate Labor Time – 2 hours. I used to feel the nose gear was a weak link in the Cessna single engine airframe design. (a) SID 55-10-01 Horizontal Stabilizer, Elevators and Attachments; (b) SID 53-12-01 Fuselage Lower Doorpost and Strut Fitting.
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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.