AD/PA-22/13 Amdt 1 - Fuselage Fabric in Area of Windshield Top Attachment Channel - Inspection
1AD/PA-22/13 Amdt 1 - Fuselage Fabric in Area of Windshield Top Attachment Channel - Inspection
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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-22 (Tri-Pacer and Colt) Series Aeroplanes
AD/PA-22/13
Amdt 1
Fuselage Fabric in Area of Windshield Top Attachment Channel - Inspection
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Applicability: All models not incorporating SL 362. Document: 1. Piper SB No. 174; or
- FAA AD 61-6-6.
Compliance: At intervals not exceeding 100 hours time in service or 6 months whichever occurs first.