AD/B767/38 Amdt 2 - Engine Fire and Overheat Detection System

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

Legislation au F2006B03393 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

 


Boeing 767 Series Aeroplanes

 

AD/B767/38

Amdt 2


Engine Fire and Overheat Detection System 11/93

 

Applicability: All model 767 series aeroplanes fitted with Kidde engine fire and overheat detection systems as listed in Boeing SB 767-26-0037 Revision 3 dated 8 July 1993.

 

Requirement: Modify the engine fire and overheat detection system in accordance with Boeing SB 767-26-0037 Revision 3 dated 8 July 1993.

 

Note: FAA AD 90-05-05 Amendment 39-6516 refers.

 

Compliance: Unless previously accomplished, prior to 31 March 1994.

 

Background: This Directive is prompted by numerous instances of false fire and overheat warnings that have resulted in engine in-flight shutdowns and aircraft diversions. This condition, if not corrected, could result in unnecessary engine in-flight shutdowns and aircraft diversions that unduly jeopardise continued safe operation of the aircraft.

 

Amendment 1 to this Directive was issued to reflect additional work required by Revision 2 of the Service Bulletin.

 

Amendment 2 is issued following release of Revision 3 of the Service Bulletin, which requires additional work for some aircraft.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.