Commonwealth legislation

AD/BEECH 60/17 - Flap Bracket

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This airworthiness directive applies to Beechcraft 60 (Duke) aeroplanes with 1,000+ hours and requires inspection of the flap actuator bracket and adjacent structure on both flaps for cracks or distress.

The first inspection is due within 100 hours after 31 Aug 1972 and thereafter at intervals not exceeding 300 hours. It falls on owners/operators, creates recurring inspection costs and downtime, and leaves inspection methods and remedial actions unspecified.

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Current sections

Direct links to the current provisions in AD/BEECH 60/17 - Flap Bracket.

AD/BEECH 60/17 - Flap Bracket

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

View image in the official source Beechcraft 60 (Duke) Series Aeroplanes

AD/BEECH 60/17 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 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.

Source text

Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.