AD/B737/19 - Engine Overheat, Fire Detection and Fire Extinguishing Systems (Cth)

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

Boeing 737 Series Aeroplanes

AD/B737/19 Engine Overheat, Fire Detection and Fire Extinguishing Systems

Applicability: All 737-200, -300 and -400 aeroplanes.

Requirement: "FIRE EXTINGUISHER BOTTLE CROSS-CONNECTION"

1. The routing of the electrical wiring to the fire extinguisher bottles is to be

3/89 permanently modified in such a manner that inadvertent cross-connection of any explosive squib electrical connectors is impossible.

Note: Boeing Service Letter 737-SL-24-57 refers.

ENGINE OVERHEAT, FIRE DETECTION AND FIRE EXTINGUISHING SYSTEMS

2. 737-200 series aircraft. Carry out a functional check of each system in accordance with Boeing Telex M-7272-89-0532 dated 31 January 1989.

3. 737-300 and -400 series aircraft. Carry out a functional check of each system in accordance with Boeing Telex M-7272-89-0530 dated 31 January 1989.

Note 1: Operators of models 737-300 and -400 series aircraft that have completed a functional check of one engine's overheat and fire detection system, and a continuity check of the second engine's overheat and fire protection system to comply with FAA AD 89-01-51 dated 11 January 1989, are only required to complete the functional check on the second engine, and the "Fire Extinguishing Wire" portion of the functional test procedure detailed in Boeing Telex M-7272-89-0530 (Requirement 3 above).

Note 2: Boeing have superseded Telex 0156 with 0530.

Note 3: FAA Telegraphic AD T89-03-51 refers to Requirements 2 and 3.

Compliance: Requirement 1: Within 25 days from 7 February 1989.