Document ID: chunk:federal_register_of_legislation:F2006B03599:body:0
Version: federal_register_of_legislation:F2006B03599
Segment Type: other
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Character Range: 0–880

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.