AD/BEECH 76/2 - Cowl Flap Hinge Assemblies
1AD/BEECH 76/2 - Cowl Flap Hinge Assemblies
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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 Beechcraft 76 (Duchess) Series Aeroplanes
AD/BEECH 76/2 Cowl Flap Hinge Assemblies 6/79
Applicability: All model 76 with S/Nos. ME-1 to ME-6 and ME-8 to ME-79. Requirement: Action in accordance with Beechcraft SI No. 1044.
Compliance: Unless already accomplished, within 100 hours’ time in service after 30 June 1979. Background: The existing aluminium hinge is subject to cracking and failure in service.