AD/PA-38/3 Amdt 1 - Vertical Fin/Rudder Leading Edge - Inspection and Modification
1AD/PA-38/3 Amdt 1 - Vertical Fin/Rudder 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-38/3
Amdt 1
Vertical Fin/Rudder Leading Edge - Inspection and Modification
1/79
Applicability: All models PA-38-112 with S/Nos. 38-78A0001 to 38-78A0215 and 38-78A0217 to 38-78A0226.
Document: 1. Piper SB No. 607A, Parts I and II; or
- FAA AD 78-22-01, Amdt. 39-3323.
Compliance: 1. Inspect at intervals not exceeding 25 hours time in service; and
- Modify within 50 hours time in service after 20 November 1978.