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REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
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
Vol. 1 03−11−1
REV 71, Oct 31/07
▼
CL−604 Operating Manual
PSP 604−6
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
colour to indicate wing anti-ice
on.
(13) Leave icing conditions.
EMERGENCY PROCEDURES
Electrical
Vol. 1 03−11−2
REV 71, Oct 31/07
▼
CL−604 Operating Manual
PSP 604−6
1. ELECTRICAL (CONT'D)
A. Loss of All Normal Electrical Power (Cont’d)
No
(12) CAS messages................................................... Review affected systems.
The following significant systems are not available when on emergency power
only:
• Yaw damper 2 and AFCS 2
• Flaps, ground spoilers
• Stabilizer trim channel 1
• Mach trim, aileron and rudder trim
• Hydraulic pumps 1B, 2B & 3A
• DME, FMS 2, GPS
On airplanes 5301 to 5386 not incorporating SB 604−24−002:
• FMS 1
• Copilot’s PFD, MFD, navigation & communication systems
• R Pack
• Right probe heaters, AOA vane heater and ice detector
• Nose wheel steering system, anti-skid system
• Both windshield heaters, right window heater
• Copilot’s instrument lights, NAV lights, and L & R landing lights
• SPS altitude compensation
NOTE
1. With Mach trim not available, do not exceed 250 KIAS
(0.7 M), unless the autopilot is engaged and functioning
normally.
2. Without probe and AOA vane heaters, do not rely on stall
　
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