Commonwealth legislation

AD/BEECH 55/23 Amdt 1 - Flap Bracket

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This Civil Aviation Safety Authority AD requires owners/operators of Beechcraft 55, 58 and 95‑55 (Baron) aeroplanes with ≥1,000 hours TIS to inspect both left and right flap actuator brackets and adjacent structure for cracks or distress.

First inspection within 100 hours after 31 Aug 1972, then repeat at intervals not exceeding 300 hours; owners fund compliance and maintenance organisations perform the work.

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Current sections

Direct links to the current provisions in AD/BEECH 55/23 Amdt 1 - Flap Bracket.

AD/BEECH 55/23 Amdt 1 - 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 55, 58 and 95-55 (Baron) Series Aeroplanes

AD/BEECH 55/23

Amdt 1

Flap Bracket 8/72

Applicability: All 95-55, 55 & 58 series aeroplanes 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.