Commonwealth legislation

AD/B747/2 - Fuselage - Structural Modification

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This Australian airworthiness directive requires a fuselage structural modification for all Boeing 747 models, to be completed by 31 December 1977, following the technical instructions in FAA AD 75‑15‑05.

Issued by CASA, the mandate obliges aircraft owners/operators to carry out and fund the work, creating scheduling, cost and compliance pressure for operators and maintenance providers.

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Current sections

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AD/B747/2 - Fuselage - Structural Modification

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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 747 Series Aeroplanes

AD/B747/2 Fuselage - Structural Modification NK

Applicability: All models.

Document: FAA AD 75-15-05 (39-2262).

Compliance: Before 31 December 1977.

Source text

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