Document ID: chunk:federal_register_of_legislation:F2006B03424:body:0
Version: federal_register_of_legislation:F2006B03424
Segment Type: other
Provision Reference: 
Character Range: 0–642

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.