SUPPLEMENTAL INSPECTION NUMBER: 55-10-01. 1. TITLE: • Horizontal Stabilizer, Elevators and Attachments Inspection. 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

2018-06-28

Download full  SUPPLEMENTAL INSPECTION NUMBER: 55-10-01. 1. TITLE: • Horizontal Stabilizer, Elevators and Attachments Inspection. 2. EFFECTIVITY • 17280001 and On, 172S8001 and On.. INSPECTION COMPLIANCE.

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William J. Hughes Technical Center On September 1, 2007, Cessna introduced the Supplemental Structural Inspection Program (SID) for the Model 425, after working with Model 300/400 operators and the FAA. The program consists of the current structural maintenance inspections, plus supplemental inspections, as required, for continued airworthiness of the airplane as years of service are accumulated. SID’s, of course, are the industry’s way of addressing the aging GA aircraft fleet. It’s likely SID’s will be developed for all legacy GA aircraft, not just twin Cessna’s. Currently, SID’s are not mandatory for piston powered aircraft which, of course, includes 310’s. No 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; 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.

EFFECTIVITY 18265176 thru 18268615, F18200026 thru F18200169 INSPECTION COMPLIANCE ALL USAGE: INITIAL 10,000 Hours or 20 Years (NOTE) REPEAT 3,000 Hours or 5 CESSNA AIRCRAFT COMPANY MODEL 100 SERIES (1963 - 1968) SERVICE MANUAL SUPPLEMENTAL INSPECTION NUMBER: 55-10-01 1. TITLE: Horizontal Stabilizer, Elevators and Attachments Inspection - All Models 2. EFFECTIVITY Model 150 Serial Numbers 644, 649, 15059701 thru 15069308, Model F150 Serial Numbers F150-0001 thru F150-0389, cracking discovered in 2011 (SID 55-10-01) Case Study – Cessna 210 SID 55-11-02 Cessna 150/152 Vertical Stabilizer Attach .

Cessna 100 series aircraft: all required SID inspections must be completed by 30 June 2014 (2A-13-00 page 5). Note: 2A-14-31 Engine Mount inspection by 30 June 2015 or next engine overhaul. The additional SID inspection requirements are incorporated into the specific aircraft Instructions for Continued Airworthiness (ICAs).

STABILIZERS - TAILCONE AND HORIZONTAL STABILIZER INSPECTION. Download full  SUPPLEMENTAL INSPECTION NUMBER: 55-10-01. 1. TITLE: • Horizontal Stabilizer, Elevators and Attachments Inspection.

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Coordinate this inspection with SID 55-30-01, Vertical Stabilizer, Rudder and Attachments Inspection. SID inspections. Due to the wide scope of work that needs to be carried out during the first introductory structural inspection, our offer is divided into two stages. 1 Dic 2015 aún cuando no estén alcanzadas por el SID. A raíz de la novedad informada por ANAC, CESSNA AIRCRAFT ha emitido una revisión de. May 1, 2008 The Conquest SID calls for all 441s to undergo a substantial and costly initial inspection by September 1, imposes additions to existing phase  Jun 20, 2017 listed in the SAIB, the FAA recommends performing the inspections detailed in Cessna's supplemental inspection document (SID) 55-10-01. 7. Jan. 2014 Lufttüchtigkeit, wie die Cessna SID entwickelt, kontrolliert und 206.

I bought my first aircraft last year here in Sweden with a fresh annual. It’s a beautiful C182P from 1972. This year when I left her for the annual the maintenance team told me that they have to remove the interior to look for corrosion because of the Cessna SID. We can perform the SID & CPCP inspection for all Cessna 100 Series models including Reims Rocket, Cardinal, RG, TR and other variants. We have experience with all versions of Cessna 172, all versions of Cessna 150, Cessna 152 and both Cessna 182 fixed gear and Cessna 182 retractable gear versions. Cessna Single Engine Service-Letter (SEL) SEL-05-01 vom 3. Oktober 2012, und die geltenden Cessna Service-Handbücherentsprechend Anhang 1 dieses SIB, der die SID Inspektionen beinhaltet. Anwendbarkeit: Cessna 100 und 200 Series Flugzeuge, alle Typen, Modelle und Seriennummern, bis zur Herstellung 1986 (einschließlich).
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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.

Download full  SUPPLEMENTAL INSPECTION NUMBER: 55-10-01. 1. TITLE: • Horizontal Stabilizer, Elevators and Attachments Inspection.
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Cessna 150 airplanes. The inspection that resulted in these SDRs was done following Cessna Supplemental Inspecion Document (SID) 55-11-02. FAA and Textron Aviation (Cessna) have been aware of cracking of the aft fin attachment fitting; and have previously issued a number of airworthiness publications to inform owner, operators, and

Watch and see why.The Cessna Citation Mustang is a very light jet built by Cessna.Download | https://store.x-plane. 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; 2016-06-27 2018-03-03 Cessna C152 II (11) Cessna C172N (6) Cessna C182RG (2) Cessna CT206H (13) Cessna CT210M (14) Piper PA28 Archer II (3) Piper PA28 Arrow IV (3) Piper PA31 Navajo (6) Piper Shared (2) FSX / P3D Default .

Hi everyone. I bought my first aircraft last year here in Sweden with a fresh annual. It’s a beautiful C182P from 1972. This year when I left her for the annual the maintenance team told me that they have to remove the interior to look for corrosion because of the Cessna SID.

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. 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.

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. 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.