Commonwealth legislation

AD/BEECH 90/28 - Flap Bracket - Inspection

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This AD from the Civil Aviation Safety Authority requires operators of Beechcraft 90 and 65‑90 (King Air) aeroplanes with 1,000+ hours TIS to start and repeat inspections of the flap actuator bracket and adjacent structure for cracks or distress. It mandates the first check within 100 hours after 31 Aug 1972 and then every 300 hours, creating a recurring maintenance obligation to manage structural safety risk.

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 90/28 - Flap Bracket - Inspection.

AD/BEECH 90/28 - Flap Bracket - Inspection

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 90 and 65-90 (King Air) Series Aeroplanes

AD/BEECH 90/28 Flap Bracket - Inspection 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.