Document ID: chunk:federal_register_of_legislation:F2006B03393:body:0
Version: federal_register_of_legislation:F2006B03393
Segment Type: other
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Character Range: 0–1352

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.