Document ID: chunk:federal_register_of_legislation:F2006B03093:body:0
Version: federal_register_of_legislation:F2006B03093
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Boeing 747 Series Aeroplanes

AD/B747/191 Engine Fire Detection 12/98
 Applicability: Model 747 series aeroplanes fitted with Rolls-Royce RB211-524G/H engines. Requirement:              Modify the engine fire detection system in accordance with Boeing Alert Service
            Bulletin 747-26A2250 dated 26 June 1997.

            Note: FAA AD 98-17-13 Amdt 39-10715 and Rolls-Royce PLC Service Bulletin RB.211-26-C101 refer.

 Compliance: At the next engine shop visit of the engine but no later than 5 November 2003.

            This Airworthiness Directive becomes effective on 5 November 1998.

            Background: The FAA has received a report advising of a combuster burn-through event that damaged the engine fire detection system such that no fire warning was annunciated on the flight deck. This directive implements a modification which is intended to prevent failure of the engine fire detector system to annunciate a fire warning message to flight crew following a severe engine failure. Failure to annunciate a fire warning could lead to delayed or improper flight crew response to the engine failure.