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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. SID means a Cessna Aircraft Company Supplemental Inspection Document. 4 Exemption — certificate of registration holder CASA AD/Cessna/400/40, that has been around for more than 10 years, gave the spar an 8200 hour life. 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.

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. 8. COMMENTS This inspection supersedes and replaces CAP 55-10-01, Horizontal Stabilizer Aft Attach Fitting. Coordinate this inspection with SID 55-30-01, Vertical Stabilizer, Rudder and Attachments Inspection.

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.

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. 2003-10-03 2018-06-28 2014-03-07 Cessna 150 airplanes. The inspection that resulted in these SDRs was done following Cessna Supplemental Inspecion Document (SID) 55-11-02.

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. 2003-10-03 2018-06-28 2014-03-07 Cessna 150 airplanes.

(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 Company Supplemental Inspection Document. 4 Exemption — certificate of registration holder CASA AD/Cessna/400/40, that has been around for more than 10 years, gave the spar an 8200 hour life.
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7. Jan. 2014 Lufttüchtigkeit, wie die Cessna SID entwickelt, kontrolliert und 206. Vorderer Holm. Höhenleitwerk.

PURPOSE SUPPLEMENTAL INSPECTION NUMBER: 55-10-01. 1. TITLE: • Horizontal Stabilizer, Elevators and Attachments Inspection. 2. EFFECTIVITY • 18280001 and On, T18208001 and On.. INSPECTION COMPLIANCE. ALL USAGE: INITIAL 10,000 Hours or 20 Years (NOTE).
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Subject: Cessna – Supplemental (Structural) Inspection Programmes Ref. Publications: Cessna Single Engine Service Letter (SEL) SEL-05-01 dated 3 October 2012; and the applicable Cessna Service Manuals, as listed in Appendix 1 of this SIB, which incorporate the SID inspections. 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.

7. Jan. 2014 Lufttüchtigkeit, wie die Cessna SID entwickelt, kontrolliert und 206. Vorderer Holm. Höhenleitwerk. 55-10-01. CASA AD/CESSNA 206/54. Cessna Aircraft Company developed the Supplemental.
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2014-04-13 Engine Model: IO360 engines (non-Turbo) Multiple Engines and Props : Front Engine : Factory Remanufactured 2009, 642.9 SMOH Rear Engine : Factory Remanufactured 2009, 642.9 SMOH Front Prop : 64.8 April 28/2010 Rear Prop : 18.8 April 11/2011 The Cessna 210N aircraft, registered VH -JHF, was manufactured in 1980 and first registered in Australia in 1990. The airframe had accumulated 11,299 hours total time in service. The aircraft had been modified with the approved installation of a magnetometer system for conducting low-level geophysical surveys. [IMGCAP(1)]Despite an extremely rocky start in the late 70s, Cessnas top-of-the-line turboprop has recovered nicely and now commands a premium in the marketplace. The 441 Conquest/Conquest II stacks up very well against the competition in an area of great interest to turboprop buyers: Performance. HistoryIn the aviation heyday of the 1970s, Cessna made a bold move by completely ignoring the SUPPLEMENTAL INSPECTION NUMBER: 55-10-01. 1.