Commonwealth legislation

AD/B727/32 - Nose Landing Gear Actuating Bracket - Inspection

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

The Civil Aviation Safety Authority requires removal and non‑destructive inspection (fluorescent dye penetrant or eddy current) of nose landing‑gear actuating bracket P/N 65‑16370‑1 on affected Boeing 727s once that bracket reaches 1,000 hours TIS, and repeating inspections at intervals not exceeding 600 hours. Operators bear removal/inspection and any repair/replacement costs, and must schedule recurring downtime and track bracket hours to comply.

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AD/B727/32 - Nose Landing Gear Actuating Bracket - 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 Boeing 727 Series Aeroplanes

AD/B727/32 Nose Landing Gear Actuating Bracket - Inspection 6/66

Applicability: All models with nose landing gear actuator brackets, P/N 65-16370-1, which have accumulated 1000 hours total time in service.

Requirement: Remove Bracket P/N 65-16370-1 and inspect for cracks initiating at all bolt holes using a fluorescent dye penetrant or eddy current technique.

Compliance: At intervals not exceeding 600 hours time in service.

Source text

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