AD/BEA 121/15 - Flap Actuating Lever Assemblies
1AD/BEA 121/15 - Flap Actuating Lever Assemblies
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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 121/15 Flap Actuating Lever Assemblies 4/75
Applicability: All series 1, 2 and 3 aeroplanes.
Requirement: Action in accordance with Scottish Aviation SB No. B121/61.
Compliance: Within 25 hours time in service after 19 May 1975 and thereafter at intervals not exceeding 100 hours time in service.