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