1AD/DHC-6/11 - Flap Elevator Trim Cables - 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-6/11 Flap Elevator Trim Cables - Modification 2/68

Applicability: All models with S/Nos. 1 to 95.

 

Document: De Havilland of Canada Mod. Bulletin No. 6/1127. Compliance: Within 300 hours time in service after 21 March 1968.