AD/B767/102 - Fuel Pump Conduit Sleeving Inspection (Cth)

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

Boeing 767 Series Aeroplanes

AD/B767/102 Fuel Pump Conduit Sleeving Inspection 8/98

TX

Applicability: All Boeing Model 767 aircraft line positions 001 to 689 inclusive and 691.

Requirement: 1. Perform a one-time visual inspection to confirm installation of Teflon sleeves over the electrical wires to the boost pumps installed inside conduits in the main and center wing tanks in accordance with Boeing Message M-7200-98-01080, dated 18 March 1998.

2. If any Teflon sleeve is found to be missing during the inspection required by Requirement 1 of this AD inspect to detect damage to the wires, in accordance with Boeing Message M-7200-98-01080, dated 18 March 1998.

1. If no damage is found, install a Teflon sleeve in accordance with Boeing Message M-7200-98-01080, dated 18 March 1998.

3. If any damage is found, inspect to detect damage to the conduits in accordance with Boeing Message M-7200-98-01080, dated 18 March 1998.

1. If no damage is found, replace any damaged wire and install a Teflon sleeve in accordance with Boeing Message M-7200-98-01080, dated 18 March 1998.

b. If any damage is found, replace any damaged wire and conduit and install a Teflon sleeve, in accordance with Boeing Message M-7200-98-01080, dated 18 March 1998.

4. Operators are to report all instances of missing sleeving, sleeving that required rework, and any instances of damaged wiring to Boeing. The report should include the following:

1. the aircraft model number;

b. the aircraft line position;

c. the total number of hours time-in-service accumulated on the airplane;