Document ID: chunk:federal_register_of_legislation:F2006B03227:body:0
Version: federal_register_of_legislation:F2006B03227
Segment Type: other
Provision Reference: 
Character Range: 0–682

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

 Boeing 747 Series Aeroplanes

 AD/B747/47 Upper Deck Type A Door - Power and Slide
                     Deployment Mechanism Fasteners

 Applicability: All aircraft listed in the Requirement Document. Requirement: Action in accordance with Boeing SB 747-52A2198.
            Note: FAA AD 86-02-03 refers.

 Compliance: Prior to 31 March 1986.

 4/86
 DM

            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.