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(5) Jammed side ......................................... Determine If left side, do not re-engage
autopilot.
Right side jammed:
Yes
(6) STALL PROT, PUSHER
switch (either left or right) .....................Select to OFF.
NOTE
Stick shaker on operative control column, operates at
a lower intensity.
No
(3) Land at the nearest suitable airport.
NOTE
Controllability is reduced. Select the longest runway available
with minimum turbulence and crosswind.
Prior to landing:
(4) GPWS/FLAP OVRD switch
(if installed) ...........................................................Select to OVRD, to mute the flap
aural warning.
(5) FLAPS ..................................................................Select to 20° for landing.
EMERGENCY PROCEDURES
Flight Controls
Vol. 1 03−12−2
REV 74, Nov 07/08
▼
CL−604 Operating Manual
PSP 604−6
1. FLIGHT CONTROLS (CONT'D)
B. Elevator System Jammed (Cont’d)
(6) Approach speed ...................................VREF (Flaps 45°)
+ 14 KIAS minimum.
(7) Actual landing distance .................................... Increase as applicable by factor given
below:
WITHOUT THRUST REVERSERS WITH THRUST REVERSERS
1.55 (55%) 1.50 (50%)
END
EMERGENCY PROCEDURES
Flight Controls
Vol. 1 03−12−3
REV 74, Nov 07/08
CL−604 Operating Manual
PSP 604−6
1. FLIGHT CONTROLS (CONT'D)
C. Rudder System Jammed
Indication: Higher than normal flight control forces.
NOTE
With a jammed primary flight control, it may be necessary to
reduce airspeed to improve airplane handling.
(1) Autopilot ....................................................... Disconnect if coupled.
(2) YD DISC pushbutton .............................................Press to disengage yaw damper.
Check YAW DAMPER caution
message on.
(3) Rudder pedals .............................................. Overpower Attempt to overpower jammed
condition.
Jam persists:
Yes
(4) Straight flight............................................. Maintain using aileron and differential
thrust, until touchdown.
NOTE
Approximately 20% N1 differential thrust may be required
to maintain wings-level flight using thrust alone. If
available, rudder trim can be used to maintain directional
control.
No
(4) Land at the nearest suitable airport.
NOTE
Select the longest runway available with minimum turbulence
and crosswind.
Prior to landing:
(5) GPWS/FLAP OVRD switch
(if installed) ...........................................................Select to OVRD, to mute the flap
aural warning.
(6) FLAPS ..................................................................Select to 20° for landing.
(7) Approach speed ...................................VREF (Flaps 45°)
+ 14 KIAS minimum.
(8) Actual landing distance .................................... Increase as applicable by factor given
below:
WITHOUT THRUST REVERSERS WITH THRUST REVERSERS
1.55 (55%) 1.50 (50%)
EMERGENCY PROCEDURES
Flight Controls
Vol. 1 03−12−4
REV 74, Nov 07/08
▼
CL−604 Operating Manual
PSP 604−6
1. FLIGHT CONTROLS (CONT'D)
C. Rudder System Jammed (Cont’d)
NOTE
After touchdown, use nose wheel steering and, if necessary, differential
braking to maintain directional control, as the airplane will turn in the
direction of the jammed rudder.
END
EMERGENCY PROCEDURES
Flight Controls
Vol. 1 03−12−5
REV 74, Nov 07/08
CL−604 Operating Manual
PSP 604−6
1. FLIGHT CONTROLS (CONT'D)
D. Stabilizer Trim Runaway
Indication: Abnormal/uncommanded change in pitch attitude.
Stabilizer trim changes without pilot input.
Higher or lower than normal and increasing or decreasing pitch control
forces.
(1) Control column ..................................................Assume manual control and override
runaway.
(2) Both STAB TRIM DISC switches ..........................Press hold and release.
(3) Control .............................................................. Transfer to pilot (left) side.
(4) STAB CH1 and CH2 HSTCU
circuit breakers (2F8 and 4B8) .............................. Open
(5) Airspeed ...............................................................Adjust to minimize out of trim
condition.
NOTE
1. If a pull force is required, increase airspeed. If a push force
is required, decrease airspeed.
2. Do not exceed VMO /MMO or minimum maneuvering speed
　
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