Commonwealth legislation

AD/B767/7 - Passenger/Crew Door Latch Overcentre Mechanism

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Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This airworthiness directive requires operators of specified Boeing 767s (line positions 2–121 and 124–127) to carry out Boeing Service Bulletin SB 767‑52‑0041 to inspect and restore or replace certain self‑locking nuts after reports they failed to meet locking‑torque specs. Compliance is mandatory by 31 March 1986, with operators bearing costs and downtime. CASA issued the AD and points to the Boeing SB (and FAA AD 86‑02‑01) as the required method of compliance.

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AD/B767/7 - Passenger/Crew Door Latch Overcentre Mechanism

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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 767 Series Aeroplanes

AD/B767/7 Passenger/Crew Door Latch Overcentre Mechanism 4/86

Applicability: All model 767 with line position 2 to 121 and 124 to 127. Requirement: Action in accordance with Boeing SB 767-52-0041.

Note: FAA AD 86-02-01 refers.

Compliance: Prior to 31 March 1986.

Background: Boeing Co have reported that a significant percentage of self locking nuts P/N BACN10JC6CM in stock do not meet specified locking torque requirements.

Source text

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