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

The following defects have been found in compliance with the SIDs for Cessna 100 Series aircraft. Click on the pictures below to view a larger version.

Click on the pictures below to view a larger version. For your convenience, I've provided two different packages: msfs2020-G3000-enhanced-std and msfs2020-G3000-enhanced-tbm. At this point, I recommend downloading the -tbm version for several reasons. First, the -std version will break the Cessna Citation Longitude (if you don't have the Longitude installed you can safely ignore this point). IAE for Quality and Reliability – the one stop shop Our Cranfield facility has been successfully maintaining aircraft for over Fifteen years, and its aircraft maintenance, avionic and electrical component overhaul and repair section has grown into one of Britain’s leading suppliers for most types of aircraft with numerous third party customers. 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.

The additional SID inspection requirements are incorporated into the specific aircraft Instructions for Continued Airworthiness (ICAs). The following defects have been found in compliance with the SIDs for Cessna 100 Series aircraft. Click on the pictures below to view a larger version. For your convenience, I've provided two different packages: msfs2020-G3000-enhanced-std and msfs2020-G3000-enhanced-tbm. At this point, I recommend downloading the -tbm version for several reasons.

2014-03-07

23. Make an entry in the airplane logbook that states Oct 5, 2013 Nathan Whetzel of Airframe Components shows how to inspect a Cessna 172 horizontal stabilizer spar to look for cracks that could cause Jul 31, 2012 I am amazed that there has no mention or reaction to cessna's new inspection requirements for the ageing cessna.I have just read through the In case you missed it, Cessna has quietly added a huge SID (Supplementary Inspection Document) to its Maintenance/Service Manual for the 400 Series piston Oct 31, 2019 On 3 June 2002, the Cessna Aircraft Company issued SID Number 32-30-05 titled “Main/Nose Gear Retraction Systems Teardown and Cessna 100 Series 1962 & Prior Maintenance Manual (part# PC-300) SERVICE MANUAL SUPPLEMENTAL INSPECTION NUMBER: 55-10-01 1. Inspection Document - or SIDs - requirements for Cessna 100 Series 1956-62 service. Mar 3, 2018 numbers of the 400-series twin Cessna's including the 425 Conquest the overlapping Supplemental Inspection Document (SID) released Single Engine Alert: SERVICE LETTER MANDATORY SEL-55-01.

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.

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. TITLE: • Horizontal Stabilizer, Elevators and Attachments Inspection. 2.

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.
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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 CESSNA AIRCRAFT COMPANY MODEL 180/185 SERIES (1969 - 1980) SERVICE MANUAL SUPPLEMENTAL INSPECTION NUMBER: 55-10-01 1. TITLE: Horizontal Stabilizer, Elevators and Attachments Inspection 2. EFFECTIVITY 18051994 thru 18053167 185-1448 thru 18504138 INSPECTION COMPLIANCE ALL USAGE: INITIAL 5,000 Hours or 20 Years (NOTE) REPEAT 2,000 Hours or 5 CESSNA AIRCRAFT COMPANY MODEL 150 SERIES (1969 - 1976) SERVICE MANUAL SUPPLEMENTAL INSPECTION NUMBER: 55-10-01 1. TITLE: Horizontal Stabilizer, Elevators and Attachments Inspection 2.

[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.
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Cessna SID Vad har hänt sedan förra året? Presentatör . Johan Brunnberg, Flygteknisk Inspektör & Del-M Koordinator . Sjö- och luftfartsavdelningen . Enheten för operatörer, fartyg och luftfartyg . Sektionen för teknisk operation . 2014-10-16/20 1

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.