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AD/DHC-6/38 - Horizontal Stabiliser Rear Spar - Inspection
1AD/DHC-6/38 - Horizontal Stabiliser Rear Spar - 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 DHC-6 (Twin Otter) Series Aeroplanes
AD/DHC-6/38 Horizontal Stabiliser Rear Spar - Inspection 7/74
Applicability: All models with S/Nos. 1 to 393 excluding 107, 168, 182, 184, 209, 383, 385, 386,
390 and 391.
Document: De Havilland of Canada SB No. 6/310.
Compliance: Within 100 hours time in service after 31 August 1974.