AD/PA-38/10 - Stabiliser/Elevator Leading Edge - Inspection and Modification
1AD/PA-38/10 - Stabiliser/Elevator Leading Edge - Inspection and Modification
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text Piper PA-38 (Tomahawk) Series Aeroplanes
AD/PA-38/10 Stabiliser/Elevator Leading Edge - Inspection
and Modification Applicability: All models PA-38-112 with S/Nos. 38-78A0001 to 38-78A0400. Document: 1. Piper SB No. 607A, Part III; or
- FAA AD 78-22-01, amendment 39-3323.
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Compliance: Unless already accomplished, within 50 hours time in service after 20 November 1978.