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POWER PLANT FIRE
DETECTION/EXTINGUISHING
AFT CLOSET
OPTIONAL
LAVATORY SMOKE
DETECTION
(OPTIONAL)
FORWARD LEFT AND RIGHT
CLOSET (OPTIONAL SMOKE
DETECTION)
AFT
LAVATORY
(OPTIONAL)
AVIONICS BAY
SMOKE DETECTION
GF0910_001
The FIDEEX system includes fire detector assemblies, sensing elements, smoke detectors, fire
extinguishing containers and a FIDEEX control unit.
FIRE PROTECTION
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 2
09−10−1
FLIGHT COMPARTMENT FIRE WARNING
The fire protection system provides the means to detect and extinguish a fire in the engine nacelles
and in the Auxiliary Power Unit (APU) compartment. Engine/APU fire warning is provided by:
· MASTER warning lights (2).
· Aural warning.
· EICAS messages.
· Three red warning lights (one for each engine nacelle and one for the APU compartment),
installed in the flight compartment fire handles.
Both the detection systems and extinguishing systems permit testing and/or monitoring for system
faults from the flight compartment. A fire warning and extinguisher preflight
test of the system is
provided in the flight compartment.
FIRE DETECTING SYSTEM
An overheat detection system, installed in the pylon area for each engine, permits the flight crew to
monitor any overheat condition in this area. A similar overheat detection system is installed in each
main landing gear wheel well.
WHEEL WELL OVERHEAT WARNING
An element in the wheel well area warns of an overheat condition in either of the main wheel wells.
Indication and test function is provided in the flight compartment.
FIRE AGENT DISCHARGE INDICATION
The fire extinguisher bottle is fitted with a low pressure switch. The switch provides an annunciation
in the flight compartment when pressure drops below a predetermined pressure setting.
SMOKE DETECTION
The FIDEEX system can provide smoke detection capability for the baggage compartment, forward
and aft lavatories, up to four cabin closets and avionics bay.
PORTABLE FIRE EXTINGUISHERS
Portable fire extinguishers are located throughout the airplane. One halon type fire extinguisher is
installed in the flight crew compartment. Refer to the EMERGENCY EQUIPMENT Chapter for
additional information on the portable fire extinguishers.
FIRE PROTECTION
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 2
09−10−2
SYSTEM OVERVIEW SCHEMATIC
IAC
Master WARNING/CAUTION
LIGHTS.
PRIMARY EICAS Page Displays,
Warnings, Cautions, Advisory
and Status Messages.
Fire Extinguisher
Bottle No.1.
Fire Extinguisher
Bottle No. 2.
Fire Control Handles.
Left Main Wheel Well
Overheat Detection.
Right Main Wheel Well
Overheat Detection.
APU Compartment
Discharge Lines.
Left Engine
Compartment
Discharge Lines.
Right Engine
Compartment
Discharge Lines.
Avionics Bay (2).
GF0910_002
MASTER
WARNING/CAUTION
WARNING
CAUTION
ROLL SPLRS
PLT CONT
ROLL
SEL
PLT
ROLL
MASTER
WARNING/CAUTION
WARNING
CAUTION
ROLL SPLRS
CPLT CONT
ROLL
SEL
CPLT
ROLL
RAD BARO
MINIMUMS NAV SCR BARO SET
PUSH STD
IN HPa RAD BARO
MINIMUMS NAV SCR BARO SET
PUSH STD
IN HPa
SPD
PUSH CHG
CRS 1 FMS MAN
PUSH DCT
HDG
PUSH SYNC
DN
UP
ALT CRS 2
PUSH DCT
DISCH
PULL
1 2
DISCH
PULL
1 2
DISCH
PULL
1 2
7 8
APU Compartment
DAU
FIDEEX
Control Unit
LH MLG Bay RH MLG Bay
6
11
9 10
TOTAL FUEL (LBS) 41550
1.54 1.54
73.3 73.3
789 789
14600 10000 14600
2350 ND
STAB
NU
NL RUDDER
LWD RWD
NR
TRIMS
7.2
N2
FF (PPH)
OIL TEMP
OIL PRESS
93.4
5750
115
81
93.4
5750
115
81
EPR
N1
ITT
AIL
1.65 1.65
CRZ
SYNC
APU FIRE
R ENG FIRE
L ENG FIRE
5 4
2
1
3
1
2
3
4
5
6
7
8
9
10
11
LH Engine RH Engine
FIRE PROTECTION
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 2
09−10−3
FIRE CONTROL HANDLES
The three fire control handles are provided for the engine and APU fire protection system. They are
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