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On airplanes 5301 to 5630 not incorporating Service Bulletin 604–49–006 or
604–49–009:
NOTE
Bleed air extraction from the APU is not permitted above 14,500 feet.
(a) BLEED AIR, 10TH STAGE R
switch/light ................................................. Press in to open right valve.
Check the following:
• R 10TH CLOSED light out.
• APU LCV OPEN light out.
(b) BLEED AIR, 10TH STAGE
ISOL switch/light......................................Press out to close isolation valve.
Check the following:
• 10TH ISOL OPEN light out.
• APU LCV OPEN light on.
(c) BLEED AIR, 10TH STAGE L
switch/light ................................................. Press in to open left valve and close
APU load control valve.
Check the following:
• L 10TH CLOSED light out.
• APU LCV OPEN light out.
(d) BLEED AIR, APU LCV
switch/light ...............................................Press out to match APU load control
valve closed position.
(3) Climb power .........................................................Check
NORMAL PROCEDURES
Climb, Cruise and Descent
Vol. 1 04−07−1
REV 68, Apr 16/07
▼
CL−604 Operating Manual
PSP 604−6
1. CLIMB, CRUISE AND DESCENT (CONT'D)
A. Climb Check (Cont’d)
CAAI Certified Airplanes
When above 10,000 feet AGL:
(4) APU................................................................Shutdown
(a) APU, START/STOP switch/light..............Press out to shutdown the APU.
Check AVAIL light out.
When rpm decreases to below 50% and EGT to below 350°C (662°F):
(b) APU, PWR FUEL switch/light ..................Press out Check the following:
• APU GEN OFF caution
message out.
• APU gauges disappear
from status page after
approximately 60 seconds.
On airplanes incorporating Canadair Service Bulletin 604−34−020 or 604−34−025:
(5) GPWS TERR INHB switch/light ............................Press Check GPWS TERR INHB
lights out.
(6) PASS SIGNS switches................................ As required
(7) EXTERNAL LTS switches ........................... As required
At transition level:
(8) Altimeters ................................................................. Set to 29.92 inches Hg.
NORMAL PROCEDURES
Climb, Cruise and Descent
Vol. 1 04−07−2
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
1. CLIMB, CRUISE AND DESCENT (CONT'D)
B. Cruise Check
NOTE
Icing conditions exist in flight at a TAT of 10°C (50°F) or below, and
visible moisture in any form is encountered (such as clouds, rain, snow,
sleet or ice crystals), except when the SAT is −40°C (−40°F) or below.
At or above 22,000 feet, the engine cowl and wing anti-ice systems must be on when
ice is indicated by the ice detection system.
Below 22,000 feet, the engine cowl and wing anti-ice systems must be on when in icing
conditions or when ice is indicated by the ice detection system.
(1) ANTI-ICE, COWL L and R
switch/lights ..........................................................Select as required.
(2) 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:
(3) 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:
(4) Leave icing conditions.
(5) Thrust ...................................................................Check
(6) Pressurization.......................................................Check that pressure differential and
cabin altitude are normal.
(7) Fuel ....................................................................Monitor fuel balance.
NOTE
During uncoordinated flight, fuel indications are inaccurate. Accurate
fuel indications will be obtained after 30 seconds when level and
stabilized in coordinated flight.
During gravity crossflow operations, a steady heading sideslip must be
used to ensure proper operation and to accelerate gravity crossflow.
To enhance gravity crossflow operation, fly one wing low slip (on the
side with less fuel).
CAUTION
Continued or repetitive automatic crossflow operation could be
indicative of a fuel tank leak.
　
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