AD/B737/20 Amdt 2 - Engine Fire/Overheat Detection Module

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

Legislation au F2006B02900 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 737 Series Aeroplanes

 

AD/B737/20

Amdt 2


Engine Fire/Overheat Detection Module 4/90

 

Applicability: All model 737-200, -300 and -400 series aircraft.

 

Requirement: 1. Inspect the engine fire/overheat detection module to determine the module part number.

 

2. If part number 10-61096-41, -71, -81, -91, -92 or 1062061-1, 2, -3, -11 or -12 is

installed, modify the control module in accordance with Walter Kidde Aerospace Service Bulletin 899315-26-326 (for -200 series aeroplanes), or 899315-26-324 (for -300 and -400 series aeroplanes) as applicable.

 

Note: FAA AD 89-08-12 R1 refers.

 

Compliance: Prior to 22 August 1990.

 

Background: Boeing have advised that certain Walter Kidde engine fire/overheat warning systems may become inoperative after an electrical power transfer, with no indication of failure given to flight crew. This could jeopardize continued safe flight and landing.

 

Amendment 2 to this Directive is issued to delete reference to the Australian CAA Flight Manual amendment which will be issued separately and to mandate incorporation of the referenced Walter Kidde Service Bulletins.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.