AD/BEA 121/5 Amdt 1 - Rudder Control Lever Assembly P/N BE 45.10193

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

Legislation au F2006B03599 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 121/5

Amdt 1

Applicability: All models.


Rudder Control Lever Assembly P/N BE 45.10193


5/71

 

Requirement: Action in accordance with Beagle SB B121/25.

 

Compliance: 1. For aircraft not already inspected in accordance with AD/BEA 121/5, and, for those having more than 40 hours time in service since last inspected in accordance with AD/BEA 121/5 - within 10 hours time in service after 13 May 1971; and;

 

2.    For aircraft having less than 40 hours time in service since last inspected in accordance with AD/BEA 121/5 - within 50 hours time in service from last inspection, and

 

3.    Thereafter at intervals not exceeding 50 hours time 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.