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message is provided.
MESSAGE MEANING
AURAL WARNING
(IF ANY)
APU FIRE Fire detected in the APU enclosure. FIRE BELL
L ENGINE FIRE
Fire detected in the respective engine nacelle. FIRE BELL
R ENGINE FIRE
L JETPIPE OVHT
Fire detected in the respective jetpipe and/or pylon
area.
“JETPIPE
OVERHEAT”
R JETPIPE OVHT
GALLEY OVHT Galley overheat detected (if galley overheat detector
is installed).
WARNING
Triple Chime
SMOKE BAGGAGE BAY Smoke detected in the baggage compartment. “SMOKE”
SMOKE TOILET Smoke detected in the lavatory area. “SMOKE”
APU BOTTLE LO APU firex bottle pressure is low.
APU FIRE FAIL APU fire detection loop is failed (shorted out).
APU NEG G SOV
APU negative-G shutoff valve is open after actuation of the APU FIRE PUSH
switch/light, or the negative-G shutoff valve position does not match the APU
PWR FUEL switch/light position within 5 seconds.
APU SOV
APU fuel shutoff valve is open after actuation of the APU FIRE PUSH
switch/light, or the fuel shutoff valve position does not match the APU PWR
FUEL switch/light position within 5 seconds.
ENG BOTTLE 1 LO
Respective engine firex bottle pressure is low.
ENG BOTTLE 2 LO
FIRE PROTECTION
Description
Vol. 2 09−10−15
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
EICAS MESSAGES (CONT'D)
MESSAGE MEANING
AURAL WARNING
(IF ANY)
L ENG SOV Respective fuel shutoff valve is not closed after actuation of the ENG FIRE
R ENG SOV PUSH switch/light.
L FIRE FAIL
Respective fire detection loop is failed (shorted out).
R FIRE FAIL
HYD SOV 1 Hydraulic shutoff valve is not closed after actuation of the respective ENG
HYD SOV 2 FIRE PUSH switch/light.
L JETPIPE OVHT FAIL
The respective jetpipe/pylon overheat detection loop is failed (shorted out).
R JETPIPE OVHT FAIL
APU SOV CLSD APU fuel shutoff and negative-G shutoff valves have closed after actuation of
the APU FIRE PUSH switch/light.
APU SQUIB 1 OK
Respective squib has passed its self-test.
APU SQUIB 2 OK
L ENG SOV CLSD Respective engine fuel shutoff valve has closed after actuation of respective
R ENG SOV CLSD ENG FIRE PUSH switch/light.
L ENG SQUIB 1 OK
Respective squib has passed its self-test.
L ENG SQUIB 2 OK
R ENG SQUIB 1 OK
R ENG SQUIB 2 OK
HYD SOV 1 CLSD Respective hydraulic shutoff valve has closed after actuation of the respective
HYD SOV 2 CLSD ENG FIRE PUSH switch/light.
FIRE PROTECTION
Description
Vol. 2 09−10−16
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
POWER SUPPLY AND CIRCUIT BREAKER SUMMARY
SYSTEM SUB-SYSTEM CB NAME BUS BAR
CB
PANEL
CB LOCATION NOTES
Fire Protection Detection ENG JETPIPE
OVHT R
DC BATT 1 N7
ENG JETPIPE
OVHT L
DC BATT 1 N8
FIRE DETECTORS
R ENG
DC BATT 1 N9
FIRE DETECTORS
L ENG
DC BATT 1 N10
FIRE DETECTORS
APU
DC BATT 1 N11
FIRE DETECTORS
TEST
DC BATT 1 N12
MLG BAY OVHT
DET
DC BATT 2 N4
SMOKE DETECT DC BUS 2 2 K4
Extinguishing FIRE EXT 1 R ENG DC
EMERGENCY
1 R1
FIRE EXT 1 L ENG DC
EMERGENCY
1 R2
FIRE EXT 2 R ENG DC
EMERGENCY
1 R3
FIRE EXT 2 L ENG DC
EMERGENCY
1 R4
APU FIRE EXT DC
EMERGENCY
1 R5
FIRE PROTECTION
Summary
Vol. 2 09−20−1
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
FIRE PROTECTION
Summary
Vol. 2 09−20−2
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
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庞巴迪挑战者605机组操作手册 CL605-FIRE_PROTECTION(6)
