Commonwealth legislation

AD/B727/129 - Fuselage Circumferential Joint Doubler BS259, 360, 441, 481 and 681

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Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

4/10 complexity

The Civil Aviation Safety Authority requires operators of certain Boeing 727‑100 (line positions 1–547) and 727‑200 (line positions 433–549) to carry out the inspections and repairs specified in FAA AD 90‑26‑09 (and consult Boeing Service Bulletin 727‑53‑0084 Rev.4).

This adopts the FAA safety concern about delamination, corrosion or cracking of fuselage circumferential joint doublers that could cause loss of cabin pressurisation; affected owners/operators must obtain the referenced documents, pay for and ensure compliance.

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Current sections

Direct links to the current provisions in AD/B727/129 - Fuselage Circumferential Joint Doubler BS259, 360, 441, 481 and 681.

AD/B727/129 - Fuselage Circumferential Joint Doubler BS259, 360, 441, 481 and 681

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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/B727/129 Fuselage Circumferential Joint Doubler

BS259, 360, 441, 481 and 681

Applicability: 727-100 line position 1 through 547.

727-200 line position 433 through 549.

3/91

Requirement: Action in accordance with the technical requirements of FAA AD 90-26-09 Amdt 39- 6835.

Note: Boeing SB 727-53-0084 Rev. 4 refers.

Compliance: As specified in the Requirement Document.

Background: Country of origin AD. Delamination, corrosion and/or cracking if not corrected, could result in loss of cabin pressurisation.

Source text

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