AD/BEECH 90/28 - Flap Bracket - Inspection
1AD/BEECH 90/28 - Flap Bracket - 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 90/28 Flap Bracket - Inspection 8/72
Applicability: All models which have achieved 1000 or more hours’ time in service.
Requirement: Inspect flap actuator bracket and adjacent structure on RH and LH flaps for cracks or signs of distress.
Compliance: Within 100 hours’ time in service after 31 August 1972 and thereafter at intervals not exceeding 300 hours’ time in service.