Document ID: chunk:federal_register_of_legislation:F2006B03413:body:0
Version: federal_register_of_legislation:F2006B03413
Segment Type: other
Provision Reference: 
Character Range: 0–1029

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

 Boeing 767 Series Aeroplanes

 AD/B767/6 Flying Controls Self Locking Nuts 12/85

TX

 Applicability: All Model 767 with line position 2 to 121, and 124 to 126. Requirement:  Action in accordance with:
              1. Boeing Alert Service Bulletin 767-27A0064.

2.    (FAA ADT85-21-51 Paras. A and B refer). Compliance: As detailed in Requirement Document No. 2.
            Background: The manufacturer has advised that two incidents of defective self-locking nuts found in the primary flight control system (horizontal stabilizer) have been reported. The same type of nut is also used in the secondary flight control system - trailing edge flap and spoiler.

            These reports indicate that the self-locking nuts have backed off which could cause the disconnection of actuators from control surfaces and result in complete or partial loss of control of the aircraft.