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caution message on.
If warning persists (after 10 sec):
(5) BOTTLE ARMED PUSH TO
DISCH switch/light.............................................Press in and hold until light goes out,
to discharge firex bottle.
Check ENG BOTTLE 1 (2) LO
caution message on.
If warning persists (after an additional 30 sec):
(6) Other BOTTLE ARMED PUSH TO
DISCH switch/light.............................................Press in and hold until light goes out,
to discharge other firex
bottle.
Check ENG BOTTLE 1 (2) LO
caution message on.
EMERGENCY PROCEDURES
Power Plant
Vol. 1 03−03−1
REV 66, Feb 01/07
▼
CL−604 Operating Manual
PSP 604−6
1. POWER PLANT (CONT'D)
A. Engine Fire/Severe Engine Damage (In Flight) (Cont’d)
(7) In-Flight Engine Failure/Shutdown .............. Accomplish Refer to Chapter 5;
ABNORMAL PROCEDURES
– POWER PLANT – In-Flight
Engine Failure/Shutdown.
END
EMERGENCY PROCEDURES
Power Plant
Vol. 1 03−03−2
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
1. POWER PLANT (CONT'D)
B. Engine Fire/Severe Engine Damage (On Ground)
Indication: L (R) ENG FIRE PUSH light on, L (R) ENGINE FIRE warning message and
fire bell on.
(1) Parking brake ........................................................... Set
Affected engine:
(2) Thrust lever ..................................................SHUT OFF
(3) ENG FIRE PUSH switch/light............................Press in Check the following:
• BOTTLE ARMED PUSH
TO DISCH lights on,
• L (R) ENG SOV CLSD
advisory message on and
• HYD SOV 1 (2) CLSD
advisory message on.
(4) FUEL, L and R BOOST PUMP
switch/lights .....................................................Press out to disarm both boost pumps.
Check L and R FUEL PUMP
caution messages on.
If warning persists (after 10 sec):
(5) BOTTLE 1 and 2 ARMED PUSH
TO DISCH switch/lights.....................................Press in and hold until lights go out, to
discharge firex bottles.
Check ENG BOTTLE 1 and 2
LO caution messages on.
(6) Passenger Evacuation procedure ............... As required Refer to EMERGENCY
EVACUATION – Passenger
Evacuation procedure in this
chapter.
END
EMERGENCY PROCEDURES
Power Plant
Vol. 1 03−03−3
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
1. POWER PLANT (CONT'D)
C. Double Engine Failure
Indication: Engine failure indicated on EICAS; N1, N2, ITT and fuel indications
(1) IGNITION, CONT switch/light............................Press in Check IGNITION A/B advisory
message on.
(2) Airspeed .......................................... 240 KIAS minimum
(3) Engine instruments............................. Verify N1, N2, ITT
If engines continue to run-down:
(4) Thrust levers (both) ......................................SHUT OFF
(5) ADG manual deploy handle .....................................Pull for at least 1 second, then
stow.
Check EMER PWR ONLY
warning message on.
When ADG power is established:
(6) STAB TRIM, CH 2 switch ..................................Press in to engage STAB TRIM CH 2.
(7) Oxygen masks (if required) ..................................... Don Set to 100%.
(8) Crew communication....................................... Establish Set MASK/BOOM switch to
MASK.
(9) PASS SIGNS, NO SMKG and
SEAT BLTS switches ...........................................Select both to ON.
(10) APU (if available).................................................... Start when at or below 20,000 feet.
On airplanes 5301 to 5630 NOT incorporating Service Bulletin 604–49–006 or
604–49–009:
(10) APU (if available).................................................... Start when at or below 15,000 feet.
(11) AC POWER, APU GEN switch.............................Select to ON.
(12) AIR-CONDITIONING, L and R
PACK switch/lights ..........................................Press out to select both packs off.
Check L and R PACK OFF
lights on.
(13) ANTI-ICE, WING switch .......................................Select to OFF.
(14) ANTI-ICE, L and R COWL
switch/lights .....................................................Press out to select cowl anti-ice off.
EMERGENCY PROCEDURES
Power Plant
Vol. 1 03−03−4
REV 76, Jul 17/09
▼
CL−604 Operating Manual
PSP 604−6
1. POWER PLANT (CONT'D)
C. Double Engine Failure (Cont’d)
WARNING
To avoid thermal seizure, increase airspeed as required to maintain at
　
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