Commonwealth legislation

AD/B737/38 - Fuselage Lap Joints BS259 to BS1016

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Commonwealth

Collection

legislative instrument

Plain English Summary

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This Directive, issued by CASA for Boeing 737s line numbers 001–291, requires operators to carry out the repairs/modifications specified in FAA AD 89‑09‑03 (paras A–D) in accordance with the referenced Requirement Document.

Completing those works partially terminates some obligations of an earlier AD, shifts inspection obligations to a repair/modification outcome, and imposes direct compliance costs on operators who must obtain and follow the FAA and Requirement Document technical guidance.

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AD/B737/38 - Fuselage Lap Joints BS259 to BS1016

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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 737 Series Aeroplanes

AD/B737/38 Fuselage Lap Joints BS259 to BS1016 5/90

Applicability: Line number 001 to 291 inclusive.

Requirement: Action in accordance with the technical requirements of FAA AD 89-09-03, paras A to D.

Note: Incorporation of the repairs/modifications in this Directive partially terminate the requirements of AD/B373/37.

Compliance: In accordance with the Requirement Document.

Background: This Directive requires terminating action for parts of AD/B737/37. This is in recognition that inspection procedures alone may not ensure an adequate level of structural integrity at the skin splices.

Source text

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