AD/BEECH 95/23 - Control Surface Trim Tab Systems
1AD/BEECH 95/23 - Control Surface Trim Tab Systems
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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 Beechcraft 95 (Travelair) Series Aeroplanes
AD/BEECH 95/23 Control Surface Trim Tab Systems 6/80
Applicability: All models 95, B95, B95A, D95A and E95 with S/Nos. TD-2 to TD-721. Requirement: Action in accordance with Beechcraft SI No 0846-152, Rev 2.
Compliance: Within 100 hours’ time in service after 30 June 1980 and thereafter at intervals not exceeding 100 hours’ time in service.
Background: The inspection procedure defines maximum allowable control surface trim tab freeplay caused by accumulative wear in control linkages and actuators.