Document ID: chunk:federal_register_of_legislation:F2006B10427:body:0
Version: federal_register_of_legislation:F2006B10427
Segment Type: other
Provision Reference: 
Character Range: 0–1094

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 125/147 Cable Loom Inspection 3/95

            Applicability: Hawker 1000, BAe 125 Series 1000A and B aircraft identified in Hawker Raytheon Corporate Jets Mandatory Service Bulletin SB 24-313 dated 19 December 1994.

            Requirement: Inspect the electrical cable loom behind the right-hand throttle box cover in accordance with Hawker Raytheon Corporate Jets Mandatory Service Bulletin SB 24- 313 dated 19 December 1994.

            Note: This Service Bulletin has been classified as Mandatory by the CAA(UK).

 Compliance: Prior to 31 July 1995.

            Background: Hawker Raytheon has received a report of damage to the cable loom behind the right- hand throttle box cover caused by the flap selector spring strut. Failure of electrical systems could result if this condition is not rectified. This Directive provides a method of early detection of damage to the cable loom.