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D. High Crosswind Take-Off Procedure (Cont’d)
When positive rate of climb is indicated:
(12) 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.
NORMAL PROCEDURES
Taxiing and Take-Off
Vol. 1 04−06−14
REV 77, Oct 20/09
CL−604 Operating Manual
PSP 604−6
1. TAXIING AND TAKE-OFF (CONT'D)
E. Rolling Take-Off Procedure
Rolling take-off procedures are described below. If used, the corresponding take-off distance
penalties must be applied (refer to the Airplane Flight Manual, Chapter 6; PERFORMANCE –
TAKE-OFF PERFORMANCE – ROLLING 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,
Chapter 6; PERFORMANCE – TAKE-OFF PERFORMANCE, must be reduced by
500 kg (1,100 lb).
The take-off weight limited by tire speed, derived from the Airplane Flight Manual,
Chapter 6; PERFORMANCE – TAKE-OFF PERFORMANCE, must be reduced by
1,200 kg (2,650 lb).
On airplanes NOT incorporating Service Bulletin 604−22−006:
Prior to entering the runway or when aligned on the runway centre line:
(1) Take-Off/Go-Around switch...................................Press
(2) VS pitch wheel................................................... Reduce the flight director command
cue to 10 degrees.
When cleared for take-off and aligned on the runway centre line:
(3) Brakes ...............................................................Release
(4) Thrust levers.....................................................Advance promptly to achieve
appropriate take-off N1 setting,
and press
Take-Off/Go-Around (TOGA)
switches.
On airplanes NOT incorporating Service Bulletin 604−22−006:
(4) Thrust levers.....................................................Advance promptly to achieve
appropriate take-off N1 setting.
(5) Thrust levers............................................................. Set to pre-determined take-off N1
by the time 60 KIAS is
reached.
Check APR ARM advisory
message comes on at above
79% N1.
NORMAL PROCEDURES
Taxiing and Take-Off
Vol. 1 04−06−15
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)
(6) Flight and engine instruments ............................Monitor Check that engine indications
do not exceed limits.
(7) N1 setting..................................................... Crosscheck
(8) Airspeed .............................................................Monitor
WARNING
Excessive rotation rates (exceeding 3 degrees per second) or
over-rotations may lead to high pitch attitudes and angles of attack
being attained while the aircraft is near the ground. This can reduce
stall margins significantly resulting in stick shaker/pusher activation and
potentially loss of control. Pilots must rotate smoothly towards the
target pitch attitude then transition to speed control.
NOTE
1. The flight director guidance represents an initial target for rotation
only and does not guarantee that the recommended climb speed will
be achieved/maintained under all conditions. Pilots must transition
to speed control immediately after initial rotation.
2. Stall margins may be improved by reducing initial pitch attitude.
At VR:
(9) Airplane ............................................................... Rotate smoothly towards an initial
pitch target of 12 degrees in
one continuous motion at a
pitch rate not exceeding
3 degrees per second.
On airplanes NOT incorporating Service Bulletin 604−22−006:
(9) Airplane ............................................................... Rotate smoothly towards an initial
　
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