CTHRepealedLegislation
AD/DHC-6/13 - Flap Control Push Rod Assembly - Modification
1AD/DHC-6/13 - Flap Control Push Rod Assembly - 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-6/13 Flap Control Push Rod Assembly - Modification 8/68
Applicability: All models with S/Nos. 1 to 105 not modified in Mod. Bulletin No. 6/1085. Document: De Havilland Canada Mod. Bulletin No. 6/1085.
Compliance: Before 1 January 1969.