Commonwealth legislation

AD/BEECH 35/33 - Flap Bracket

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This airworthiness directive requires owners/operators of Beechcraft 35 (Bonanza) aeroplanes with ≥1,000 hours TIS to inspect the flap actuator bracket and adjacent structure for cracks or distress. The first inspection is due within 100 hours TIS after 31 August 1972, with repeat inspections at intervals not exceeding 300 hours. It aims to detect deterioration before failure, imposing recurring maintenance costs and demand for qualified inspection/repair.

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 35/33 - Flap Bracket.

AD/BEECH 35/33 - 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 35 (Bonanza) Series Aeroplanes

AD/BEECH 35/33 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.