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AD/PA-28/35 Amdt 2 - Main Landing Gear Torque Links
Piper PA-28 Series AeroplanesPiper PA-28 Series Aeroplanes
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Piper PA-28 Series Aeroplanes
| AD/PA-28/35 Amdt 2 | Main Landing Gear Torque Links | 9/2011 |
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| Applicability: | All models with fixed landing gear except those with torque link P/N 78032-00V or 78033-000. |
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| Requirement: | Action in accordance with Piper Mandatory Service Bulletin No. 1199 or FAA AD 72-08-06.Note: FAA Special Airworthiness Information Bulletin CE-10-17 refers. FAA SAIBs may be accessed via the internet at the following URL:http://rgl.faa.gov |
| Compliance: | At intervals specified in Piper Mandatory Service Bulletin No. 1199 or FAA AD72-08-06.Previous compliance with Piper Service Letter No. 600 constitutes compliance with this Amendment. |
| This Amendment becomes effective on 13 May 2011. | |
| Background: | Original issue of this AD specified compliance with Piper SL No. 600.Amendment 1 exempted aircraft with improved design of torque link assembly.Amendment 2 specifies Piper MSB No. 1199 which was published in February 2009 and supersedes Piper SL No. 600 in its entirety. A Note about SAIB CE-10-17 was added. The word “Inspection” was deleted from the title. |
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Charles Lenarcic
Delegate of the Civil Aviation Safety Authority
29 April 2011