AD/BEECH 90/37 - Elevator and Rudder Trim Tab Actuator Systems - Inspection
1AD/BEECH 90/37 - Elevator and Rudder Trim Tab Actuator Systems - Inspection
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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 90 and 65-90 (King Air) Series Aeroplanes
AD/BEECH 90/37 Elevator and Rudder Trim Tab
Actuator Systems - Inspection
2/75
Applicability: All models 65-90, 65-A90,B90 & C90 with S/Nos. LJ-1 and subs., and model E90 with S/Nos. LW-1 and subs, which have in excess of 300 hours’ time in service.
Document: Beechcraft SI No. 0691-133-135.
Compliance: Within 25 hours’ time in service after 22 January 1975 and thereafter at intervals not exceeding 100 hours’ time in service.