AD/HS 125/145 - Electrical Wiring Chafing

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B10425 In force Legislative Instrument

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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 125/145 Electrical Wiring Chafing 11/94

Applicability: Hawker 1000 and BAe 125 Series 1000A and B aircraft identified in Hawker Raytheon Corporate Jets Mandatory Service Bulletin SB A29-92 Revision 1 dated 1 August 1994.

 

Requirement: If not previously accomplished, action in accordance with Hawker Raytheon Corporate Jets Mandatory Service Bulletin SB A29-92 Revision 1 dated 1 August 1994.

 

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

 

Compliance: Prior to 30 October 1994.

 

Background: The aircraft manufacturer has received reports of chafing of an electrical cable/loom on a hydraulic pipe, this caused an insulation breakdown and electrical short circuit which produced a pin-hole failure of the hydraulic pipe. Action required by this Directive is designed to decrease the likelihood of a loss of hydraulic pressure, electrical malfunction or an in-flight fire.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.