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AD/DHC-6/39 - Electric Power Cable Below Cockpit - Modification
1AD/DHC-6/39 - Electric Power Cable Below Cockpit - 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-6/39 Electric Power Cable Below Cockpit - Modification
Applicability: All models with S/Nos. 1 to 135.
Document: De Havilland of Canada SB No. 6/304 Rev. B.
Compliance: Within the next 100 hours time in service after 30 August 1974.
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