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• APU SOV CLSD advisory
message on.
(8) BATT MASTER switch ............................................OFF to prevent CVR erasure.
Copilot: On evacuation command
(9) ATC .......................................................................Notify of emergency conditions and
of intention to evacuate.
(10) AIR-CONDITIONING, L and R
PACK switch/lights ..........................................Press out to ensure minimum
differential pressure within
airplane.
(11) CABIN PRESSURIZATION,
EMER DEPRESS switch/light ...........................Press in to drive outflow valves open.
Check EMER DEPRESS
caution message on.
(12) Exits....................................................................... Open
(13) Passenger evacuation...................... Render assistance and direct passengers away
from the airplane.
EMERGENCY PROCEDURES
Emergency Evacuation
03−10−1
REV 74, Nov 07/08
▼
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. EMERGENCY EVACUATION (CONT'D)
A. Passenger Evacuation (Cont’d)
(14) Airplane ........................................................... Abandon by any suitable exit.
END
EMERGENCY PROCEDURES
Emergency Evacuation
03−10−2
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. ELECTRICAL
A. Loss of All Normal Electrical Power
Indication: ADG automatically deployed and EMER PWR ONLY warning message.
(1) ADG manual deploy handle .....................................Pull for at least 1 second, then
stow.
(2) ADG......................................................................Check AC ESS BUS powered.
When ADG power is established:
(3) STAB TRIM, CH 2 switch ..................................Press in to engage CH 2.
Check STAB CH 2 INOP
status message out.
(4) Engine instruments................................................Verify and check N1, N2 and ITT
indications.
Both engines confirmed failed:
Yes
(5) Double Engine Failure
procedure ............................................ Accomplish Refer to POWER PLANT –
Double Engine Failure
procedure in this chapter.
− END −
No
(5) AIR-CONDITIONING, R PACK
switch/light .......................................................Press out to deselect.
(6) Cabin altitude .....................................................Monitor
(7) Descent ....................................................... As required If an immediate descent is
required, refer to
AIR-CONDITIONING AND
PRESSURIZATION –
Emergency Descent
procedure in this chapter.
On airplanes 5301 to 5407:
CAUTION
Do not exceed 250 KIAS with the ADG deployed.
(8) AC POWER, GEN 1 and GEN 2
switches................................................................Select to OFF/RESET then ON.
Check GEN 1 and 2 OFF
caution messages out.
EMERGENCY PROCEDURES
Electrical
03−11−1
REV 71, Oct 31/07
▼
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. ELECTRICAL (CONT'D)
A. Loss of All Normal Electrical Power (Cont’d)
Any generator comes on-line:
Yes
Re-establish normal power:
No
(9) APU........................................................................ Start when at or below 20,000 feet.
On airplanes 5301 to 5630 NOT incorporating Service Bulletin 604–49–006 or
604–49–009:
(9) APU........................................................................ Start when at or below 15,000 feet.
(10) AC POWER, APU GEN switch.............................Select to ON.
Check APU GEN OFF caution
message out.
Any generator comes on-line:
Yes
Re-establish normal power:
(11) ADG PWR TXFR,
OVERRIDE switch.........................................Press to override.
Check EMER PWR ONLY
warning message out.
(12) HYDRAULIC pump
switch 3B ......................................................Select to AUTO/ON, as applicable.
Check HYD PUMP caution
messages are not displayed.
(13) CAS messages........................................... Review
(14) Affected systems ....................................... Restore
− END −
No
(11) Descent ........................................................... Continue to 10,000 feet or lowest safe
altitude (if required).
Wing anti-ice is required:
Yes
(12) ANTI-ICE, WING switch ...............................Select to STBY.
Check both N2 gauges change
　
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