AD/PC-6/28 Amdt 1 - Wing Strut Attachment - Inspection
1AD/PC-6/28 Amdt 1 - Wing Strut Attachment - 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-6/28
Amdt 1
Wing Strut Attachment - Inspection 12/80
Applicability: All models with S/Nos. 338 to 701. Document: Pilatus SB No. 93.
Compliance: At intervals not exceeding 100 hours time in service.
Background: Service experience indicates that the inspection for corrosion in the wing strut attachment can be extended to 100 hourly intervals.