AD/PA-30/22 - Landing Gear and Flap Assemblies - Inspection
1AD/PA-30/22 - Landing Gear and Flap Assemblies - 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-30 & 39 (Twin Comanche) Series Aeroplanes
AD/PA-30/22 Landing Gear and Flap Assemblies - Inspection 12/73
Applicability: Models PA-30, PA-39 with S/Nos. 30-1 to 30-2000, 39-1 to 39-156. Document: Piper SL No. 650 and Addendum 1.
Compliance: Within 100 hours time in service after 31 December 1973.