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(6) CABIN PRESSURIZATION, MAN
RATE switch................................................ As required commensurate with crew and
passenger comfort.
When reaching target cabin altitude:
(7) CABIN PRESSURIZATION, MAN
ALT selector ............................................................. Set to mid position/centre.
(8) Descent ............................................................... Initiate to 10,000 feet or lowest safe
altitude, whichever is higher.
(9) Land at the nearest suitable airport.
At 10,000 feet or lowest safe altitude:
(10) CABIN PRESSURIZATION, MAN
ALT switch.................................................................DN to decrease cabin altitude to
landing field elevation.
(11) CABIN PRESSURIZATION, MAN
RATE switch................................................ As required commensurate with crew and
passenger comfort.
ABNORMAL PROCEDURES
Doors
Vol. 1 05−08−7
REV 68, Apr 16/07
▼
CL−604 Operating Manual
PSP 604−6
1. DOORS (CONT'D)
D. Baggage Door − Not Closed/Locked (Cont’d)
When reaching target cabin altitude:
(12) CABIN PRESSURIZATION, MAN
ALT selector ............................................................. Set to mid position/centre.
END
ABNORMAL PROCEDURES
Doors
Vol. 1 05−08−8
REV 68, Apr 16/07
CL−604 Operating Manual
PSP 604−6
1. ELECTRICAL
A. AC Bus 1 Transfer Failure
Indication: AC 1 AUTOXFER caution message and associated AUTO XFER FAIL light
on.
AC Bus 1 is powered:
Yes
(1) No further action required.
− END −
No
(1) Affected airplane systems .................................. Review Refer to Bus Inoperative List
in this section.
END
B. AC Bus 2 Transfer Failure
Indication: AC 2 AUTO XFER caution message and associated AUTO XFER FAIL light
on.
AC Bus 2 is powered:
Yes
(1) No further action required.
− END −
No
(1) Affected airplane systems .................................. Review Refer to Bus Inoperative List
in this section.
END
C. AC Bus 1 Failure
Indication: AC BUS 1 caution message on.
(1) AC POWER, GEN 1 switch ..................................Select to OFF/RESET then ON.
AC BUS 1 caution message persists:
Yes
(2) Affected airplane systems .......................... Review Refer to Bus Inoperative List
in this section.
− END −
No
(2) No further action required.
END
ABNORMAL PROCEDURES
Electrical
Vol. 1 05−09−1
REV 71, Oct 31/07
CL−604 Operating Manual
PSP 604−6
1. ELECTRICAL (CONT'D)
D. AC Bus 2 Failure
Indication: AC BUS 2 caution message on.
(1) AC POWER, GEN 2 switch ..................................Select to OFF/RESET then ON.
AC BUS 2 caution message persists:
Yes
(2) HYDRAULIC pump switch
3B .................................................................Select from AUTO to ON.
Check HYD PUMP 3B caution
message out.
(3) Affected airplane systems .......................... Review Refer to Bus Inoperative List
in this section.
− END −
No
(2) No further action required.
END
E. AC Essential Bus Failure
Indication: AC ESS BUS caution message on.
Manually transfer AC essential to alternate source:
(1) AC POWER, AC ESS XFER
switch/light .........................................................Press in to manually transfer the
essential bus to AC Bus 2.
Check the following:
• ALTN light on, and
• AC ESS ALTN status
message on.
AC ESS BUS caution message persists:
Yes
(2) Affected airplane systems .......................... Review Refer to Bus Inoperative List
in this section.
− END −
No
(2) No further action required.
END
ABNORMAL PROCEDURES
Electrical
Vol. 1 05−09−2
REV 71, Oct 31/07
CL−604 Operating Manual
PSP 604−6
1. ELECTRICAL (CONT'D)
F. ADG Inadvertent Deployment
Indication: ADG operating.
On airplanes 5301 to 5407:
(1) Airspeed ...........................................Do not exceed 250
KIAS with the ADG deployed.
Refer to Chapter 2;
LIMITATIONS − OPERATING
SPEEDS.
NOTE
The AC essential bus and hydraulic pump 3B can be transferred back
to either main generator, or to the APU generator, if operating, by
pressing the PWR TXFR OVERRIDE switch on the ADG control panel
after the ADG manual deploy handle is re-stowed.
　
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