AD/B767/7 - Passenger/Crew Door Latch Overcentre Mechanism
1AD/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
Image unavailable in extracted text Boeing 767 Series Aeroplanes
AD/B767/7 Passenger/Crew Door Latch Overcentre Mechanism 4/86
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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.