AD/PA-34/33 - 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
View image in the official source Piper PA-34 (Seneca) Series Aeroplanes
AD/PA-34/33 Window Curtain Rod Support Area - Inspection 10/79
Applicability: All model PA-34-200T 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.