Federal Register of Legislation
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES
Beechcraft 56TC (Turbo Baron) Series Aeroplanes
AD/BEECH 56/12 Flap Bracket 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 and 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.
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