AD/PA-32/66 - Window Curtain Rod Support Area - Inspection
1AD/PA-32/66 - Window Curtain Rod Support Area - 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-32 (Cherokee Six) Series Aeroplanes
AD/PA-32/66 Window Curtain Rod Support Area - Inspection 3/80
Applicability: All models PA-32-260, PA-32-300, PA-32R-300, PA-32RT-300 and PA-32RT-300T
with S/Nos. referenced in Piper SB No. 656.
Document: Piper SB No. 656.
Compliance: Within 100 hours time in service after 30 November 1979.
Background: Damage to the fuselage longerons at the lower window line may have been caused when installing the window curtain rods at manufacture.