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to take-off. If wing anti-ice is not required for take-off it should be
selected OFF just prior to take-off.
3. To prevent wing contamination from reverse jet blast, operating the
thrust reversers during taxi operations on wet and contaminated
surfaces should be avoided.
4. The wing anti-ice system must be selected and confirmed ON for
take-off, when the OAT is 5°C (41°F) or below and:
(a) visible moisture in any form (such as clouds, fog or mist) is
present below 400 feet AGL, or
(b) the runway is wet or contaminated, or
(c) in the presence of any precipitation (such as rain, snow, sleet
or ice crystals).
5. If wing anti-ice is selected ON for take-off, the cowl anti-ice must
also be selected ON.
6. When Type II, III or IV anti-icing fluids have been applied, the wing
anti-ice system must only be selected and confirmed ON just prior to
thrust increase for take-off.
7. The wing anti-ice system may be selected OFF only if it can be
positively verified that all of the following conditions are met:
(a) the runway to be used is not wet or contaminated,
(b) there is no precipitation, and
(c) there is no visible moisture in any form (such as clouds, fog,
mist, rain, snow, sleet or ice crystals) below 400 feet AGL.
8. Refer to Chapter 6; SUPPLEMENTARY PROCEDURES – COLD
WEATHER OPERATION – PHASE OF FLIGHT PROCEDURES.
NORMAL PROCEDURES
Taxiing and Take-Off
Vol. 1 04−06−5
REV 77, Oct 20/09
▼
CL−604 Operating Manual
PSP 604−6
1. TAXIING AND TAKE-OFF (CONT'D)
B. Take-Off Check (Cont’d)
AR Certified Airplanes
WARNING
When the OAT is 5°C (41°F) or below use deicing/anti-icing
treatment before take-off.
When the OAT is 5°C (41°F) or below the wing anti-ice system must
be selected ON for take-off, just prior to thrust increase for take-off.
NOTE
When Type II, III or IV anti-icing fluids have been applied, the wing
anti-ice system must only be selected on, if required, just prior to
thrust increase for take-off.
(3) ANTI-ICE, COWL
L and R switch/lights ............................................Select as required.
NOTE
1. The engine cowl anti-ice system must be on when the OAT is 10°C
(50°F) or below and visible moisture in any form is present (such as
fog with visibility of one mile or less, rain, snow, sleet and ice
crystals).
2. The engine cowl anti-ice system must also be on when the OAT is
10°C (50°F) or below when operating on runways, ramps, or
taxiways where surface snow, ice, standing water or slush is
present.
(4) ANTI-ICE, WSHLD/WIND
L and R switches ..................................................Select to HI or LOW, as required.
(5) ANTI-ICE, PROBES switches ..............................Select to ON.
NOTE
If departure is not imminent, delay selecting the PROBES to ON
until just prior to take-off. A lack of cooling airflow with the
PROBES selected ON may cause a loss off SAT indication on
the MFD, resulting in a potential nuisance WINDSHEAR FAIL
status message.
(6) Cabin ................................................................... Advise not less than one minute prior
to take-off.
(7) Lighting..................................................................... Set as required. Check EMER
LTS switch selected to ARM.
NORMAL PROCEDURES
Taxiing and Take-Off
Vol. 1 04−06−6
REV 77, Oct 20/09
▼
CL−604 Operating Manual
PSP 604−6
1. TAXIING AND TAKE-OFF (CONT'D)
B. Take-Off Check (Cont’d)
(8) Crew Alerting System (CAS) ................................Check the following:
• TO CONFIG OK advisory
(green) message is on.
• No warning, caution or
status messages are
present.
(9) Weather radar selectors ........................................... Set as required.
(10) ATC SEL selector..................................................... Set
NORMAL PROCEDURES
Taxiing and Take-Off
Vol. 1 04−06−7
REV 77, Oct 20/09
CL−604 Operating Manual
PSP 604−6
1. TAXIING AND TAKE-OFF (CONT'D)
C. Normal Take-Off Procedure
AR Certified Airplanes
Take-Off Speeds
Add 5 knots to the take-off speeds (V1, VR and V2) derived from the Airplane Flight
Manual, Chapter 6; PERFORMANCE – TAKE-OFF PERFORMANCE.
Take-Off Distance
The take-off distances, derived from the Airplane Flight Manual, Chapter 6;
PERFORMANCE – TAKE-OFF PERFORMANCE, must be increased by 10%.
Maximum Allowable Take-Off Weight
The take-off weight limited by brake energy, derived from the Airplane Flight Manual,
　
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