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25 knots to 10 knots. Perform
the prescribed number of
brake applications during the
last mile/kilometer of taxi prior
to and not including the final
stop or snub before take-off.
Do not drag the brakes.
AIRPLANE WEIGHT NUMBER OF BRAKE APPLICATIONS
Greater than 42,000 lb 5
36,000 to 42,000 lb 6
Less than 36.000 lb 7
NOTE
1. Use of symmetric braking is recommended, to ensure uniform brake
heating.
2. Warming of the brakes will preclude the chance of water saturated
brakes freezing at altitude and being locked for landing touchdown.
(2) Flaps......................................................................... Set for take-off.
Check corresponding surface
displacement on flight controls
page.
NORMAL PROCEDURES
Taxiing and Take-Off
Vol. 1 04−06−1
REV 77, Oct 20/09
▼
CL−604 Operating Manual
PSP 604−6
1. TAXIING AND TAKE-OFF (CONT'D)
A. Taxi Check (Cont’d)
(3) Thrust reversers ...................................................Check 1
(a) Thrust reverse levers...................................Deploy to select engine thrust
reverse.
Check the following:
• L and R REV ARMED
advisory messages on.
• REV icons appear on N1
gauges.
(b) Thrust reverse levers......................................Stow
(4) Aileron and rudder trims .......................................Check Set at neutral for take-off.
(5) Stabilizer trim............................................................ Set for take-off.
Check the following:
• Both channels of the
stabilizer trim are engaged.
• Trim is set to the correct
take-off CG range.
NORMAL PROCEDURES
Taxiing and Take-Off
Vol. 1 04−06−2
REV 77, Oct 20/09
▼
CL−604 Operating Manual
PSP 604−6
1. TAXIING AND TAKE-OFF (CONT'D)
A. Taxi Check (Cont’d)
EICAS STABILIZER TRIM SETTING FOR TAKE-OFF
C.G. Range (%MAC) Trim Setting
16.0 − 16.2 7.2
16.3 − 17.2 7.0
17.3 − 18.3 6.8
18.4 − 19.3 6.6
19.4 − 20.3 6.4
20.4 − 21.3 6.2
21.4 − 22.4 6.0
22.5 − 23.4 5.8
23.5 − 24.4 5.6
24.5 − 25.5 5.4
25.6 − 26.5 5.2
26.6 − 27.5 5.0
27.6 − 28.5 4.8
28.6 − 29.6 4.6
29.7 − 30.6 4.4
30.7 − 31.6 4.2
31.7 − 32.6 4.0
32.7 − 33.7 3.8
33.8 − 34.7 3.6
34.8 − 36.5 3.4
36.6 − 38.0 3.2
NOTE
Trim data from the FMS should be rounded down to the
next lowest multiple of 0.2 trim units.
On airplanes NOT incorporating Canadair Service Bulletin 604–34–035:
NOTE
Usage of trim data from the FMS is prohibited.
NORMAL PROCEDURES
Taxiing and Take-Off
Vol. 1 04−06−3
REV 77, Oct 20/09
▼
CL−604 Operating Manual
PSP 604−6
1. TAXIING AND TAKE-OFF (CONT'D)
A. Taxi Check (Cont’d)
(6) Flight Instruments..................................................... Set Check the following:
• No abnormal annunciations
are displayed on the EFIS.
• EFIS slip/skid indications
are normal.
• EFIS is set for departure.
(7) Fuel balance.........................................................Check
(8) ANTI-ICE, WING switch .......................................Select as required.
(9) ANTI-ICE, COWL
L and R switch/lights ............................................Select as required.
NOTE
During taxi with the anti-ice selected ON, the L or R COWL A/ICE
caution message may be posted and will go out if thrust is increased.
NORMAL PROCEDURES
Taxiing and Take-Off
Vol. 1 04−06−4
REV 77, Oct 20/09
CL−604 Operating Manual
PSP 604−6
1. TAXIING AND TAKE-OFF (CONT'D)
B. Take-Off Check
(1) IGNITION, CONT switch/light................................Press to turn ON, if required.
(2) ANTI-ICE, WING switch .......................................Select as required.
NOTE
1. The wing anti-ice system must be selected ON, for final taxi prior to
take-off, if the OAT is 5°C (41°F) or below, unless Type II, III or IV
anti-icing fluids have been applied. Single engine taxi operations are
prohibited in these conditions.
2. L (R) WING A/ICE caution messages may be posted or L HEAT or R
HEAT lights may go out during taxi but caution messages must be
verified out and WING A/ICE ON or WING/COWL A/ICE ON advisory
message and L HEAT and R HEAT lights must be verified on, prior
　
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