AD/PA-32/67 - Rudder Skin - Inspection and Modification
1AD/PA-32/67 - Rudder Skin - 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-32 (Cherokee Six) Series Aeroplanes
AD/PA-32/67 Rudder Skin - Inspection and Modification 3/80
Applicability: All models PA-32RT-300 and PA-32RT-300T with S/Nos. referenced in Piper SL No. 882.
Document: 1. Piper SL No. 882; or
- FAA AD 79-26-04, Amdt. 39-3642.
Compliance: 1. Inspect at intervals not exceeding 25 hours time in service after 23 January 1980 until modified.
- Modify in accordance with Piper SL No. 882 within 100 hours time in service after 23 January 1980.
Note: Pilot may perform and certify for inspection in para. 1.
Background: The manufacturer has received reports of small cracks developing in the area of the skin bead at the trailing edge of the rudder.