AD/DHC-6/40 - Wing Struts - Inspection and Modification
1AD/DHC-6/40 - Wing Struts - Inspection and 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 DHC-6 (Twin Otter) Series Aeroplanes
AD/DHC-6/40 Wing Struts - Inspection and Modification 4/76 Applicability: All models with S/Nos. 1 to 462, 464, 465, 468, 469, 472, 473, 474, 478 and 481. Document: De Havilland of Canada SB No. 6/342.
Compliance: 1. Inspect within 120 hours time in service after 31 May 1976.
- Modify within 360 hours time in service after 31 May 1976.