AD/PA-20/12 - Fuselage Structure, Upper Cabin - Inspection
1AD/PA-20/12 - Fuselage Structure, Upper Cabin - 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-20 (Pacer) Series Aeroplanes
AD/PA-20/12 Fuselage Structure, Upper Cabin - Inspection 11/77
Applicability: All models.
Requirement: 1. Remove interior trim to expose fuselage lateral members at top of windshield, front and rear spar carry through structure and upper longerons in cabin area.
- Visually inspect the exposed structural members for corrosion and condition of protective coatings.
Compliance: Initially inspect before 1 January 1979 unless inspected since 1 July 1977 and thereafter at intervals not exceeding 3 years.