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AD/PC-6/31 - Wing Strut Internal Corrosion - Inspection
1AD/PC-6/31 - Wing Strut Internal Corrosion - 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-6/31 | Wing Strut Internal Corrosion - Inspection | 7/71 |
|---|---|---|
| Applicability: | All models except Fairchild Hiller production. | |
| Document: | Pilatus SB No. 105. |
Compliance: Within 100 hours time in service after 31 August 1971 and thereafter at intervals not exceeding 100 hours time in service.