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

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Legislation au F2006B03424 In force Legislative Instrument

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Boeing 767 Series Aeroplanes

 

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

DM

 

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.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.