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pitch target of 10 degrees in
one continuous motion at a
pitch rate not exceeding
3 degrees per second.
(10) Pitch attitude.........................................................Adjust to achieve a minimum
airspeed of V2 + 10 KIAS.
NORMAL PROCEDURES
Taxiing and Take-Off
Vol. 1 04−06−16
REV 77, Oct 20/09
▼
CL−604 Operating Manual
PSP 604−6
1. TAXIING AND TAKE-OFF (CONT'D)
E. Rolling Take-Off Procedure (Cont’d)
When positive rate of climb is indicated:
(11) LDG GEAR lever ...................................................... Set to UP.
Check three amber hash
marks are displayed on the
EICAS primary page,
indicating that the landing gear
is in transit, followed by three
white UP indications,
indicating that the landing gear
is up and locked.
NOTE
If taxi and/or take-off were on snow or slush covered surfaces, unless
weather conditions or performance requirements prohibit, delay
retraction of the landing gear until excess water, snow or slush is
thrown off by wheel rotation and/or slip stream force.
F. After Take-Off Procedure
(1) Airspeed ...........................................V2 + 10 to 15 KIAS
(2) Flight and engine instruments ............................Monitor Check that engine indications
remain within limits, and flight
instruments indicate the
desired climb profile.
At a safe altitude, not below 320 ft AGL:
(3) AP switch/light ...................................................Press in to engage, if required.
Check the following:
• Heading mode engaged.
• Speed bug set to 200 KIAS.
NOTE
The use of excessive pitch mode (VS) on the FCP could cause
autopilot uncommanded disengagement.
Autopilot can be re-engaged after disengagement.
(4) Climb thrust .............................................................. Set the computed climb thrust
setting.
(5) IGNITION, CONT switch/light...................... As required
NORMAL PROCEDURES
Taxiing and Take-Off
Vol. 1 04−06−17
REV 77, Oct 20/09
CL−604 Operating Manual
PSP 604−6
1. TAXIING AND TAKE-OFF (CONT'D)
G. After Take-Off Check
(1) Landing gear ........................................................Check retracted.
NOTE
During normal operations, landing gear and flap indications are
normally occulted (removed from EICAS) when the landing gear are
stowed and the flaps are up.
At not less than VFTO + 5 KIAS:
(2) Flaps......................................................................... Set to 0°.
(3) THRUST REVERSER,
L and R switches ..................................................Select to OFF.
Check L and R REV ARMED
advisory messages out.
(4) CAS.............................................................Check/clear Verify and analyze any
messages, and clear (if any).
Monitor during flight.
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.
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.
(5) ANTI-ICE, COWL
L and R switch/lights ............................................Select as required.
(6) 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:
(7) 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:
(8) Leave icing conditions.
NORMAL PROCEDURES
Taxiing and Take-Off
Vol. 1 04−06−18
REV 77, Oct 20/09
CL−604 Operating Manual
PSP 604−6
1. CLIMB, CRUISE AND DESCENT
A. Climb Check
NOTE
When the auxiliary tank fuel quantity is low, the fuel quantity will
fluctuate during the climb due to fuel migration.
(1) Pressurization.......................................................Check
If the APU is supplying bleed air:
(2) Air-conditioning................................................. Transfer to engine bleeds.
NOTE
Bleed air extraction from the APU is not permitted above 15,000 feet.
　
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