Document ID: chunk:federal_register_of_legislation:F2006B02853:body:0:p2
Version: federal_register_of_legislation:F2006B02853
Segment Type: other
Provision Reference: 
Character Range: 2691–5578

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

4.    If any chafing of the FQIS wiring harness is found, replace the wire harness with a new wire harness or accomplish the applicable action(s) specified below, in accordance with the ASB.

                1. For jacket damage only that is less than 25.4mm (1 inch) in length with no sign of abrasion to the wire insulation - Install a Teflon sleeve over the wiring.

               b.    For jacket damage or a harness with an exposed shield or conductor and the insulation of the other wire is not damaged (there can be no broken shield strands if the shield wire is damaged or no broken wire strands if the unshielded wire is damaged) - Install a Teflon sleeve over the wiring terminal and along the wire to the damaged area.

5.    For wiring that was repaired in accordance with Requirement 4.a., repair the wire harness or replace the wire harness with a new wire harness.

6.    For aeroplanes on which the modification per FAA AD 99-03-04, Amdt 39-11018 has been accomplished prior to the effective date of this Directive - Perform the actions specified in Requirement 1, and in Requirements 2 or 3 of this Directive.

           Note 2: Repairs accomplished by splicing the wires in accordance with the procedure included in Boeing ASB 737-28A1168, dated 26 September 2000, prior to the effective date of this Directive, are considered acceptable for compliance with Requirements 1, 2 and 3 of this Directive.

7.    Submit a report of inspection findings to Service Bulletin Engineering, Boeing Commercial Airplane Group, PO Box 3707, Mail Stop 2H-37, Seattle, Washington 98124-2207, USA, as follows:

                1. For aeroplanes on which the Requirement 1 inspection is accomplished after the effective date of this Directive.

               b.    For aeroplanes on which the Requirement 1 inspection has been accomplished prior to the effective date of this Directive.

           Note 3: FAA AD 2001-01-13 requires submission to the FAA of a compliance plan for this work. CASA does not require submission of such a plan. However, operator planning should note: the amount of work involved. the relatively short compliance period, and the difficulty to satisfy the requirements of an exclusion under CAR (1998) 39.4.

           Note 4: FAA AD 2001-01-13 Amdt 39-12084 refers.

    Compliance:   For Requirement 1 - Within 6 months after the effective date of this Directive.

               For Requirement 2 - Before further flight. For Requirement 3 - Before further flight. For Requirement 4 - Before further flight.
               For Requirement 5 - At the next scheduled "C" Check, but no later than 15 months after the effective of this Directive.

               For Requirement 6 - Within 18 months after