AD/BEA 121/23 - Engine Mounting Structure

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

Legislation au F2006B03588 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

 


Beagle B121 (Pup) Series Aeroplanes

 

AD/BEA 121/23 Engine Mounting Structure 10/79

Applicability: All Beagle B121 series 1 and 2, which have achieved 1000 hours time in service. Requirement:              Action in accordance with British Aerospace (Scottish Division) SB No. B121/81.

Compliance: Inspect within 50 hours time in service after 27 August 1979 and thereafter at intervals not exceeding 50 hours time in service.

 

Background: The manufacturer reports that cases of engine mount cracking have been discovered in service.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.