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
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.
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.
The SID inspections have been incorporated into the affected Maintenance/Service Manuals. SID 55-10-01; o Service Bulletin SEB 05-2 “Fuselage skin & Fuel Step All remaining Cessna SID inspections must be completed prior to 30 June 2018. Thereafter comply with, as required, Cessna Corrosion Prevention and Control Program (CPCP) and Cessna SID’s Cessna SID Implementation in New Zealand – Mandatory compliance – 90 to 95% of inspected airplanes required maintenance action – 20% of those which required action needed major repair – 80% of the findings were corrosion and 20% cracking – Most (SID 55-10-01) Case Study – Cessna 210 Cessna Distributors, Single Engine Authorized Service Facilities, and affected Owners of Record 55-10-01 Horizontal Stabilizer Aft Attach Bracket X X X X The SID inspections have been incorporated into the affected Maintenance/Service Manuals. Cessna Single Engine Airplanes 145,000 produced between 1946-1986 Average age is 42 years old Made of aluminum Certified CAR 3 • Why is a new safety initiative required for Cessna single engine airplanes? The reasons for this new initiative can best be\ഠunderstood by first reviewing the history of … SID Information : 100 Series/200 Series HPSE : 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) Cessna SID into the AMP, careful consideration should be given to the potential airworthiness and safety consequences of this course of action.
CESSNA AIRCRAFT COMPANY MODEL 180/185 SERIES (1981 - 1985) SERVICE MANUAL SUPPLEMENTAL INSPECTION NUMBER: 55-10-01 1. 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
The reasons for this new initiative can best be\ഠunderstood by first reviewing the history of these airplanes. CESSNA AIRCRAFT COMPANY MODEL 152 SERIES SERVICE MANUAL B. Section 2A-10-01, Inspection Time Limits.
Cessna Single Engine Airplanes 145,000 produced between 1946-1986 Average age is 42 years old Made of aluminum Certified CAR 3 2. 2
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1. TITLE: • Horizontal Stabilizer, Elevators and Attachments Inspection.
(i) Alternative Methods of Compliance (AMOCs)
CESSNA AIRCRAFT COMPANY MODEL 180/185 SERIES (1981 - 1985) SERVICE MANUAL SUPPLEMENTAL INSPECTION NUMBER: 55-10-01 1. TITLE: Horizontal Stabilizer, Elevators and Attachments Inspection 2.
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[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
EQUIV. EQUIV. NDT1046-3-5: BOEING COMPOSITE STANDARD, ALL PT9 51-00-01 PG. 6 FIGURE 1.
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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
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. 5290020-4, Cessna Model 401/402 Calibration Standard Figure 4 part 2 & 3 Inspection. Plate A 603, BOEING REFERENCE STANDARD 767 PT 4 55-10- 01 . Airworthiness Program Inspection Number. Inspection Compliance Title. Model.