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MAIN LANDING GEAR OVERHEAT DETECTION
Figure 10-
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EICASIndications 10-
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Figure 10-
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System Test 10-
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FIRE PROTECTION Vol. 1 10-
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1. INTRODUCTION
The aircraftfire protection systemconsistsofthefollowing separate subsystems:
W Fire andoverheatdetection
W Fire extinguishing.
The fire protection systemprovidesdetection andextinguishing of afire in the engine nacelles,the auxiliarypower unit(APU) compartment andthe cargo compartment. An independentsystemis providedforfire detection andextinguishingin thelavatory. A detection system is also providedforthe main landinggear wheel wells.
The fire protection systemprovidesdetection andextinguishing of afire in the engine nacelles andthe auxiliarypower unit(APU) compartment. The mainlandinggear wheel wells are provided withfire detection only. Anindependentsystemis providedforfire detection andextinguishingin the lavatory. <0057>
Indications toalertthe crew tofire, smoke andoverheat conditions aswell asfire protection systemhealth are providedbytheEICASdisplaysand panellights.
Flight Crew Operating Manual MASTER
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FIRE PROTECTION Introduction Vol. 1 10-
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LHMLG
WHEELWELL
SENSING
ELEMENT
<PRE0057>
CARGO
COMPARTMENT
LAVATORY
Detection System Block Diagram <MST>
Figure 10---10---1
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LAVATORY
TRASHBIN
LAVATORY
FIRE
EXTINGUISHER
PORTABLEFIRE
EXTINGUISHER
CABIN
PORTABLEFIRE
EXTINGUISHER
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Fire Detection and Extinguishing (FIDEEX) REV 56, Jan 31/03
1. FIRE DETECTION AND EXTINGUISHING
A. Engine
Eachengine detection systemis dividedintotwo zones (Aand B):
W Zone Acovers the core section oftheengine andis provided withfire detection and extinguishing
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