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604–49–009:
(3) APU (if available)............................................ Start when at or below 15,000 feet.
On airplanes 5301 to 5630 NOT incorporating Service Bulletin 604–49–006 or
604–49–009:
CAUTION
Use of the APU generator in flight is not permitted unless
both main generators have failed or are off-line.
(4) AC POWER, APU GEN
switch............................................................Select to ON.
− END −
No
(2) AC ELECTRICAL page ......................................Monitor voltage, load and frequency
readouts on all generators.
END
ABNORMAL PROCEDURES
Electrical
Vol. 1 05−09−6
REV 71, Oct 31/07
CL−604 Operating Manual
PSP 604−6
1. ELECTRICAL (CONT'D)
O. AC Generator 2 Failure
Indication: GEN 2 OFF caution message on.
(1) AC POWER, GEN 2 switch ..................................Select to OFF/RESET then ON.
GEN 2 OFF caution message persists:
Yes
(2) AC POWER, GEN 2 switch ..........................Select to OFF.
NOTE
1. With generator 2 shutdown, HYD PUMP 1B is load
shed.
2. During single generator operations, AC utility busses
are shed, unless on ground with flaps at 0°.
(3) 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:
(3) APU (if available)............................................ Start when at or below 15,000 feet.
On airplanes 5301 to 5630 NOT incorporating Service Bulletin 604–49–006 or
604–49–009:
CAUTION
Use of the APU generator in flight is not permitted unless
both main generators have failed or are off-line.
(4) AC POWER, APU GEN
switch............................................................Select to ON.
− END −
No
(2) AC ELECTRICAL page ......................................Monitor voltage, load and frequency
readouts on all generators.
END
P. AC Generator Overload
Indication: GEN 1 (2) OVLD caution message on. AC ELECTRICAL page – generator
load readout indicates greater than 35 KVA.
(1) AC ELECTRICAL page ......................................Monitor generator loads,and load shed
as necessary.
END
ABNORMAL PROCEDURES
Electrical
Vol. 1 05−09−7
REV 71, Oct 31/07
CL−604 Operating Manual
PSP 604−6
1. ELECTRICAL (CONT'D)
Q. Main Battery Failure
Indication: MAIN BATT OFF caution message on. DC ELECTRICAL page – Main
battery indicates less than 18 volts DC and main battery direct bus outline is
amber.
(1) BATT MASTER switch .........................................Check ON.
MAIN BATT OFF caution message persists:
Yes
(2) DC ELECTRICAL page ..............................Monitor main battery voltage, and
assume loss of main battery.
(3) Affected airplane systems .......................... Review Refer to Bus Inoperative List
in this section.
− END −
No
(2) No further action required.
END
R. DC Emergency Bus Failure
Indication: DC EMER BUS caution message on. DC ELECTRICAL page – DC
emergency bus outline is amber.
(1) Affected airplane systems .................................. Review Refer to Bus Inoperative List
in this section.
(2) Land at the nearest suitable airport.
END
ABNORMAL PROCEDURES
Electrical
Vol. 1 05−09−8
REV 71, Oct 31/07
CL−604 Operating Manual
PSP 604−6
1. ELECTRICAL (CONT'D)
S. Bus Inoperative List
NOTE
The bus inoperative list covers systems that are important to the
approach and landing phases of flight. The list covers items that
are NOT available. The list does not cover all electrically
controlled and/or powered systems and is not a complete check
of all circuit breaker panels to determine affected systems.
LEGEND:
♦ − Indicates that the applicable system is powered by a second bus. The failure of the two
marked busses (♦) will render the applicable system inoperative.
* − If applicable (optional equipment).
SYSTEM SUBSYSTEM
AC BUS
1
AC BUS
2
DC BUS
1
DC BUS
2
AC ESS
BUS
DC ESS
BUS
DC
BATT
BUS
APU BATT
DIR BUS
MAIN
BATT
DIR BUS
ENGINE IGN A B
START L & R
inop
OIL PRESS R inop L inop BYPASS
INDIC inop
THRUST REV inop
　
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