AD/PC-6/4 - Aileron Balance Weight Arm - Inspection
1AD/PC-6/4 - Aileron Balance Weight Arm - 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 Pilatus Porter PC-6 Series Aeroplanes
AD/PC-6/4 Aileron Balance Weight Arm - Inspection 3/66
Applicability: All models with S/Nos. 338, 341, 344, 345, 349, 350, 516 to 518, 521, 522, 524, 525,
526, 528, 531, 532, 535 to 538, 543 to 551 and 554.
Document: Pilatus SB No. 25.
Compliance: At intervals not exceeding 100 hours time in service after 15 April 1966.