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 2012-05-24 · Cessna presented and described it well. Cessna, in partnership with the University of Kansas had initiated inspections of long use Cessna 400 series twins. They bought two back from operators, and took them all apart, documenting every defect they found. It would be this experience which is the basis for their SID's.
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1800lbs useful load, IO360 engines, low time factory re-manufactured engines, SL30 Digital Nav/Comm, Apollo GX65 Digital GPS/Comm, SL70 Transponder/altitude encoder, KR87 Digital ADF, PS Engineering PMA7000-S audio panel/intercom, Robertson STOL kit 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 … 2012-10-10 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 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). I give this aircraft a 3.3/5 Star Rating.
Download full SUPPLEMENTAL INSPECTION NUMBER: 55-10-01. 1. TITLE: • Horizontal Stabilizer, Elevators and Attachments Inspection.
These supplemental inspections were developed to utilize May 31, 2017 The FAA recommends performing the inspections detailed in the Cessna supplemental inspection document (SID) 55-10-01. Both the SAIB and Getting the books cessna 180 185 service manual now is not type of challenging COMMENTS Coordinate this inspection with SID. 55-30-01 55-10-01 1. 10RS.23, DC-10 SID REFERENCE STANDARD DETAIL -1 SHEET 1 PAGE 1.
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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PRICE REDUCED!!! Owner needs gone! 1800lbs useful load, IO360 engines, low time factory re-manufactured engines, SL30 Digital Nav/Comm, Apollo GX65 Digital GPS/Comm, SL70 Transponder/altitude encoder, KR87 Digital ADF, PS Engineering PMA7000-S audio panel/intercom, Robertson STOL kit 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).
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. D2070-3-13 Temporary Revision Number 10 - Aug 1/2011 2A-14-12 Page 2 For Cessna 100 airplanes and Cessna 208/208B airplanes, we recommend adherence to the applicable Textron Aviation SIDs and maintenance manuals for corrosion inspections. Airplanes based or operated in high corrosion areas are recommended to be inspected more frequently.