AD/BEECH 76/3 - Elevator Trailing Edge Bond
1AD/BEECH 76/3 - Elevator Trailing Edge Bond
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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 76/3 Elevator Trailing Edge Bond 6/79
Applicability: All model 76 with S/Nos. ME-1 to ME-6 and ME-8 to ME-62. Requirement: Action in accordance with Beechcraft SI No. 1041.
Compliance: Unless already accomplished, within 100 hours’ time in service after 30 June 1979. Background: There is a possibility of in-service separation of the elevator trailing edge bond.
Federal Register of Legislative Instruments F2006B04178