AD/STRIKEMASTER/1 - Electrical Cable Loom Chafing

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

Legislation au F2006B07133 In force Legislative Instrument

Legislation content

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


BAe (BAC 167) Strikemaster Series Aeroplanes

 

AD/STRIKEMASTER/1 Electrical Cable Loom Chafing 12/96 DM

Applicability: This Directive is applicable to all British Aerospace Corporation (BAC) 167 Strikemaster aeroplanes.

 

Requirement: Inspect, protect, restrain and if necessary repair the DC generating system electrical cables in accordance with British Aerospace Defence Limited, Military Aircraft Division, Company Special Technical Instruction (CSTI) Strikemaster 162 dated 4 April 1995.

 

Note: CAA(UK) Mandatory Permit Directive 1995-102 refers.

 

Compliance: Prior to 8 October 1996.

 

Background: The CAA(UK) has received a report of a short circuit in the DC generating system caused by heavy duty cables chafing against the thread/anchor nut of the port mainplane trailing edge fairing attachment bolt. The CSTI provides for a visual examination for cable chafing or damage, repair or replacement of the damaged cables, cable protection and encapsulation of the anchor nut assembly in sealing compound.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.