Document ID: chunk:federal_register_of_legislation:F2006B10440:body:0:p1
Version: federal_register_of_legislation:F2006B10440
Segment Type: other
Provision Reference: 
Character Range: 4–3234

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

    British Aerospace BAe 125 Series Aeroplanes

AD/HS 125/159 Wiring Inspections  1/2000 DM

    Applicability: Model Hawker 1000 series aeroplanes serial numbers 258151, 258159 and 259003
               through 259052 inclusive.

                 Requirement: 1. Perform a detailed visual inspection of the PS wire bundle coming from the bung 'DF' for chafing against the front ventral tank transfer/crossfeed actuator, in accordance with Raytheon Aircraft Service Bulletin SB 24-3201 dated October 1998.

               Note 1: For the purposes of this Airworthiness Directive, a detailed visual inspection is defined as: "An intensive visual examination of a specific structural area, system, installation, or assembly to detect damage, failure, or irregularity. Available lighting is normally supplemented with a direct source of good lighting at intensity deemed appropriate by the inspector. Inspection aids such as mirror, magnifying lenses, etc., may be used. Surface cleaning and elaborate access procedures may be required."

                 2.    Perform the applicable action when the following conditions are found during the Requirement 1 inspection:

                   1. No chafing - Ensure a minimum 0.25-inch clearance exists between the PS wire bundle and valve actuator; and install spiral wrap, as necessary, in accordance with the service bulletin.

                  b.    Chafing on a 22, 20, 16, or 14 gauge (non-shielded) wire - Repair chafed wire by splicing the damaged section using MIL-S-81824/1 splices. Ensure a minimum 0.25-inch clearance exists between the wire bundle and valve actuator; and install spiral wrap, as necessary, in accordance with the service bulletin.

                  c.    Chafing on a 10 gauge wire - Replace the entire wire with a new 10 gauge wire. Ensure a minimum 0.25-inch clearance exists between the wire bundle and valve actuator; and install spiral wrap, as necessary, in accordance with the service bulletin.

                 3.    Perform a detailed visual inspection of the shielded wires going to the fuel probe 'G' for chafing against the wing transfer valve actuator and mounting screws, in accordance with Raytheon Aircraft Service Bulletin SB 24-3201 dated October 1998.

                 4.    Perform the applicable action when the following conditions are found during the Requirement 3 inspection:

                   1. No chafing - Ensure a minimum 0.25-inch clearance exists between the wire bundle and valve actuator; and install spiral wrap, as necessary, in accordance with the service bulletin.
 COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

               b.    Chafing - Replace the entire shielded wire with a new shielded wire. Ensure a minimum 0.25-inch clearance exists between the wire bundle and valve actuator; and install spiral wrap, as necessary, in accordance with the service bulletin.

5.    Perform a borescope inspection of the entire forward wing spar/forward ventral tank