Commonwealth legislation

AD/FU24/15 - Main Landing Gear Axle Socket - Inspection

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This AD requires operators of Airparts (NZ) FU 24 series aeroplanes (except those with disc brakes) to carry out recurring visual inspections of the main landing-gear axle sockets (P/N 245101) for cracks across the lower-link lugs, at intervals not exceeding 100 hours TIS. It affects owners/operators and maintenance providers by imposing ongoing inspection costs and downtime to detect potential structural cracking and preserve airworthiness.

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Direct links to the current provisions in AD/FU24/15 - Main Landing Gear Axle Socket - Inspection.

AD/FU24/15 - Main Landing Gear Axle Socket - Inspection

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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 Airparts (NZ) Ltd. FU 24 Series Aeroplanes

AD/FU24/15 Main Landing Gear Axle Socket - Inspection 6/68

Applicability: All models except those fitted with disc brakes.

Requirement: Inspect visually, the Main Landing Gear Axle Sockets, P/N 245101, for cracks across the lugs containing the lower links.

Compliance: At intervals not exceeding 100 hours time in service.

Source text

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