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switch/lights ..........................................................Select as required.
(9) ANTI-ICE, WING switch .......................................Select as required.
If wing anti-ice is selected ON and WING L HEAT or R HEAT light goes out or
WING A/ICE ON or WING/COWL A/ICE ON advisory message goes out:
(10) Thrust ............................................................... Increase until the following come on:
• WING A/ICE ON or
WING/COWL A/ICE ON
advisory message.
• WING L HEAT and R HEAT
lights.
If WING A/ICE ON or WING/COWL A/ICE ON advisory message remains out or
WING L HEAT or R HEAT light remains out:
(11) Leave icing conditions.
(12) ANTI-ICE, WSHLD/WIND L and R
switches................................................................Select as required.
NORMAL PROCEDURES
Climb, Cruise and Descent
Vol. 1 04−07−6
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
1. CLIMB, CRUISE AND DESCENT (CONT'D)
C. Descent Check (Cont’d)
(13) Fuel quantity and balance ....................................Check the following:
• Cross-check all the
readouts in the fuel quantity
gauging system.
• Check fuel balance.
At transition level:
(14) Altimeters ................................................................. Set standby altimeter to QNH
upon receipt of information,
and cross-check altitude
readouts.
NOTE
Pilot’s and copilot’s altimeters should be left at QNE (29.92 in. Hg or
1013.2 mb) until passing through transition altitude, or upon leaving the
cruise altitude, whichever is lower.
D. In Range Check
(1) APU (if required)..................................................... Start Ensure that operating
limitations/envelope is
considered.
CAAI Certified Airplanes
When above 10,000 feet AGL:
(1) 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) BLEED AIR, APU LCV
switch/light ....................................................Check pressed out.
NORMAL PROCEDURES
Climb, Cruise and Descent
Vol. 1 04−07−7
REV 66, Feb 01/07
▼
CL−604 Operating Manual
PSP 604−6
1. CLIMB, CRUISE AND DESCENT (CONT'D)
D. In Range Check (Cont’d)
(b) APU, PWR FUEL switch/light .................... Press in and check the following:
• PWR FUEL light on, and
• APU gauges displayed on
status page.
NOTE
During in flight starts at high altitudes, the APU EGT may
momentarily spike into the amber temperature zone and
then immediately return to normal green values. This is
normal operation and no crew action is required.
(c) 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.
On airplanes 5301 to 5360 not incorporating Service Bulletin 604–49–006 or 604–49–009:
(c) 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
APU BATTERY OFF caution message may appear momentarily during
APU start.
NORMAL PROCEDURES
Climb, Cruise and Descent
Vol. 1 04−07−8
REV 73, May 14/08
▼
CL−604 Operating Manual
PSP 604−6
1. CLIMB, CRUISE AND DESCENT (CONT'D)
D. In Range Check (Cont’d)
If transferring air-conditioning to APU bleed air:
(2) Air-conditioning................................................. Transfer to APU bleed.
NOTE
The 10th-stage engine bleeds must be closed for landing with the cowl
and/or wing anti-ice system on. Refer to Chapter 2; LIMITATIONS –
OPERATING LIMITATIONS..
(a) BLEED AIR, APU LCV
switch/light ................................................. Press in to preselect load control valve
　
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