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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). REPEAT 3,000 Hours or 5 Years (NOTE).NOTE: Refer to Note 1, Section 5-14-00.. 3. PURPOSE

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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.

Effectivity. Initial. Repeat. 55-10-01. 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.

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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.

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.

SID Instructional Powerpoint . View YouTube Video . Cessna Supplemental Inspection Task Specific Non Destructive Inspection Technique Training For MRO’s And Cessna Service Facilities SIDS NDT Training Brochure (Model 100 Series and 200 Series) SIDS NDT Training Schedule (Model 100 Series and 200 Series)

Initial Compliance:3000 hours or 5 years. Recurring Compliance: 3000 hours or 5 years. Approximate Labor Time – 2 hours.

Cessna sid 55-10-01

CHANGE 34 TO THE BASIC MANUAL INCORPORATES THE 414 AND 414A SUPPLEMENTAL INSPECTION DOCUMENTS (SID'S), DATED 1 AUGUST 2002  

Cessna sid 55-10-01

TITLE: Horizontal Stabilizer, Elevators and Attachments Inspection 2. 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 . Company Private SID Number Manual Revision SID Rev. Date 100 (1953-62) 55-10-01 8 May 18, 2015 100 (1963-68) For Cessna 100 airplanes and Cessna 208/208B airplanes, SID Information : 100 Series/200 Series HPSE : SID Instructional Powerpoint .

TITLE: • Horizontal Stabilizer, Elevators and Attachments Inspection. 2. EFFECTIVITY • 18280001 and On, T18208001 and On.. INSPECTION COMPLIANCE.
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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). Beschreibung: De föreskrifter som Transportstyrelsen ger ut finns samlade i Transportstyrelsens författningssamling (TSFS).
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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;

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). REPEAT 3,000 Hours or 5 Years (NOTE).NOTE: Refer to Note 1, Section 5-14-00.. 3.

Cessna Distributors, Single Engine Authorized Service Facilities, and affected Owners of Record 55-10-01 Horizontal Stabilizer Attachment The SID inspections

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). REPEAT 3,000 Hours or 5 Years (NOTE).NOTE: Refer to Note 1, Section 5-14-00.. 3.

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 . AirCreation 582SL (5) BeechCraft B58 (12) Boeing B737 (7) Cessna C172SP (13) Cessna C172SP-I (8) Cessna Shared (2) deHavilland DHC-2 (13) What is interesting is to compare the letter from the CAA to the letter from the LBA section Hamburg (so not from the HQ)..