AD/PA-22/29 - 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
View image in the official source Piper PA-22 (Tri-Pacer and Colt) Series Aeroplanes
AD/PA-22/29 Fuselage Structure, Upper Cabin - Inspection 12/77
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.