Commonwealth legislation

AD/BEECH 50/21 - Flap Bracket

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This AD requires owners/operators of Beechcraft 50 (Twin Bonanza) aeroplanes with 1,000+ hours TIS to perform scheduled inspections of the flap actuator bracket and adjacent structure on both left and right flaps to detect cracks or distress. The first inspection is due within 100 hours TIS after 31 August 1972 and must be repeated at intervals not exceeding 300 hours TIS.

JSON API

Deep dive

Want the full deep dive?

Zoe can write the in-depth analysis on top of the summary above: how it works, who it affects and what each part actually does.

Current sections

Direct links to the current provisions in AD/BEECH 50/21 - Flap Bracket.

AD/BEECH 50/21 - Flap Bracket

meta-content-style-type: text/css meta-content-type: application/xhtml+xml; charset=utf-8 meta-generator: Aspose.Words for .NET 22.10.0

?xml version="1.0" encoding="utf-8" standalone="no"?>

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 50 (Twin Bonanza) Series Aeroplanes

AD/BEECH 50/21 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.