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PUSH.
• APU FIRE PUSH.
• BOTTLE 1 and 2 ARMED
PUSH TO DISCH.
• (APU) BOTTLE ARMED
PUSH TO DISCH.
All indications go out when
switch released.
(b) FIRE DET switch .......................................... Select to FAIL.
Hold the switch in this position
and check that the following
caution messages come on:
• L and R FIRE FAIL.
• APU FIRE FAIL.
• L and R JETPIPE OVHT
FAIL.
Messages go out when switch
released.
(15) EXTERNAL LTS, NAV switch ..............................Select to ON.
NORMAL PROCEDURES
Airplane Preparation
Vol. 1 04−04−9
REV 75, Feb 17/09
▼
CL−604 Operating Manual
PSP 604−6
1. AIRPLANE PREPARATION (CONT'D)
C. Normal Power-Up Check (First Flight of the Day) (Cont’d)
(16) APU (if required)..................................................... Start Ensure that operating
limitations/envelope is
considered.
NOTE
The APU, PWR FUEL switch/light must be selected off between each
APU start attempt. The APU, PWR FUEL switch/light should be firmly
pressed once only. If pressed twice, an immediate shutdown may
occur.
(a) AC POWER, APU GEN switch..................... Select to OFF.
(b) BLEED AIR, APU LCV
switch/light ....................................................Check pressed out.
(c) APU, PWR FUEL switch/light .................... Press in Check APU gauges displayed
on status page.
(d) APU, START/STOP switch/light................ Press in and check the following:
• START light on.
• 60% rpm – START light out.
NOTE
Greater than 30% rpm
within 60 seconds.
• 95% rpm + 4 seconds
(approx) – AVAIL light on.
• 100% rpm + 15 seconds
(approx) – APU GEN OFF
caution message on.
NORMAL PROCEDURES
Airplane Preparation
Vol. 1 04−04−10
REV 75, Feb 17/09
▼
CL−604 Operating Manual
PSP 604−6
1. AIRPLANE PREPARATION (CONT'D)
C. Normal Power-Up Check (First Flight of the Day) (Cont’d)
On airplanes 5301 to 5360 NOT incorporating Service Bulletin 604–49–006 or 604–49–009:
(d) APU, START/STOP switch/light................ Press in and check the following:
• START light on.
• 60% rpm – START light
out.
NOTE
Maximum 60 seconds
below 60% rpm.
• 95% rpm + 4 seconds
(approx) – AVAIL light on.
• 100% rpm + 15 seconds
(approx) – APU GEN OFF
caution message on.
NOTE
1. APU BATTERY OFF caution message may appear momentarily
during APU start.
2. If time permits, allow APU rpm to stabilize at 100% for 2 minutes
before applying bleed air load.
After APU RPM and EGT have stabilized:
(e) AC POWER, APU GEN switch..................... Select to ON.
If APU and AC external power are not available:
(16) Start engine using external air........................ Complete then go to step (23).
(17) Electrics (AC and DC) ................................. Established Check the following:
• Voltage, frequency and load
indications are normal, and
all AC busses powered and
lit on AC electrical page.
• TRUs are on-line, and
voltage and load indications
are normal on DC electrical
page.
• All DC busses powered and
lit, and battery chargers
operating on DC electrical
page.
NORMAL PROCEDURES
Airplane Preparation
Vol. 1 04−04−11
REV 75, Feb 17/09
▼
CL−604 Operating Manual
PSP 604−6
1. AIRPLANE PREPARATION (CONT'D)
C. Normal Power-Up Check (First Flight of the Day) (Cont’d)
(18) Lamps......................................................................Test 1
(a) LAMP TEST switch....................................... Select to 1 and hold.
Check all switch/lights come
on.
Release switch and check all
switch/lights go out.
(b) LAMP TEST switch....................................... Select to 2 and hold.
Check all switch/lights come
on.
Release switch and check all
switch/lights go out.
(19) Bleed leak detection ................................................Test 1
(a) BLEED AIR, DUCT MON
switch.................................................................Set to TEST. Check that:
• L and R DUCT FAIL lights
(10th and 14th) are on.
• L and R 10TH DUCT warning
messages on.
• L and R 14TH DUCT warning
messages on.
• “BLEED AIR DUCT” aural
on.
　
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