1AD/PC-6/8 - Rear Fuselage - Modification

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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-6/8 Rear Fuselage - Modification 3/66

Applicability: All models with max. take-off weight of 4850 lbs. Document:  Pilatus SB No. 41.

Compliance: Before 1 July 1966.