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(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
05−09−7
REV 71, Oct 31/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
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 Note the following:
• Backup power to DCU 2
and 3 (if installed) is not
available.
• Engine APR system is
inoperative.
• L and R ENG MISCOMP
caution messages are
displayed.
− 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 Engine and APU fire
extinguishing systems are
inoperative:
• Firex bottles are
inoperative,
• APU fuel feed shut-off
valves will not close, and
• Engine hydraulic shut-off
valves will not close.
(2) Land at the nearest suitable airport.
END
ABNORMAL PROCEDURES
Electrical
05−09−8
REV 71, Oct 31/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. FIRE PROTECTION
A. APU Fire Detector Loop Failure
Indication: APU FIRE FAIL caution message on.
(1) APU (if not essential)......................................Shutdown
END
B. Engine Fire Detector Loop Failure
Indication: L (R) FIRE FAIL caution message on.
(1) Affected engine ..................................................Monitor
END
C. Jetpipe Overheat Detector Failure
Indication: L (R) JETPIPE OVHT FAIL caution message on.
(1) Affected engine ..................................................Monitor
END
D. APU Firex Bottle Discharged
Indication: APU BOTTLE LO caution message on (without previous APU fire).
(1) FIRE DETECTION, TEST switch .........................Select to WARN.
(2) Glareshield, APU BOTTLE
switch/light ............................................................Check on (confirming that bottle is
charged).
APU BOTTLE light is out:
Yes
(3) APU ........................................................Shutdown
− END −
No
(3) No further action required.
END
E. Engine Firex Bottle Discharged
Indication: ENG BOTTLE 1 (2) LO caution message on (without engine fire condition).
(1) FIRE DETECTION, TEST switch .........................Select to WARN.
(2) Glareshield, Engine BOTTLE 1
and 2 switch/lights ................................................Check on, confirming that engine
bottles are charged.
(3) No further action required.
If any one engine bottle light fails to come on, assume that the affected bottle is
discharged.
END
ABNORMAL PROCEDURES
Fire Protection
05−10−1
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
ABNORMAL PROCEDURES
Fire Protection
05−10−2
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
　
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