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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
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
− END −
No
(2) No further action required.
END
ABNORMAL PROCEDURES
Electrical
05−09−1
REV 71, Oct 31/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
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
− 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
− END −
No
(2) No further action required.
END
ABNORMAL PROCEDURES
Electrical
05−09−2
REV 71, Oct 31/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
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.
To re-establish normal operations:
(2) ADG manual release handle ................................Select to STOW (if ADG was
manually deployed).
(3) ADG PWR TXFR OVERRIDE
switch .................................................................Push in to override.
(4) HYDRAULIC pump switch 3B ..............................Check selected to AUTO.
END
G. APU Battery Failure
Indication: APU BATTERY OFF caution message on. DC ELECTRICAL page – APU
battery indicates less than 18 volts DC.
(1) BATT MASTER switch .........................................Check ON.
(2) DC ELECTRICAL page ......................................Monitor APU battery voltage. Assume
loss of APU battery. The APU
is not available.
(3) Affected airplane systems .................................. Review
END
ABNORMAL PROCEDURES
Electrical
05−09−3
REV 74, Nov 07/08
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1

　
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