AD/BEECH 76/3 - Elevator Trailing Edge Bond

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B04178 Not in force Legislative Instrument

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


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

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.