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engaged as long as needed to reduce
workload.
AP TRIM IS ND (NU) caution message is displayed:
Yes
(5) Airspeed................................................Adjust as required to keep autopilot
engaged as long as possible.
NOTE
1. If AP TRIM IS ND is displayed, decrease
airspeed. If AP TRIM IS NU is displayed, increase
airspeed.
2. AP TRIM IS ND (NU) caution message will go out if
the airspeed is adjusted.
AP TRIM IS ND (NU) caution message persists:
Yes
NOTE
Anticipate an out-of-trim condition with autopilot
disengagement.
(6) Autopilot................................ Disconnect
No
Prior to landing:
Failure occurred with flaps at 45°:
Yes
(7) FLAPS .......................................................... Leave at 45°.
CAUTION
Do not jettison fuel if trim runaway is in nose down
direction.
Fuel jettison will cause the CG to move forward requiring a
larger pull force to counter and causing any push force to
be reduced.
Consider use of fuel jettison in the event of a nose-up trim
runaway condition.
A landing may be made with fuel in the tail tank.
− END −
ABNORMAL PROCEDURES
Flight Controls
Vol. 1 05−11−14
REV 77, Oct 20/09
▼
CL−604 Operating Manual
PSP 604−6
1. FLIGHT CONTROLS (CONT'D)
P. Stabilizer Trim Failure (Cont’d)
No
(7) GPWS/FLAP OVRD switch
(if installed) ...........................................................Select to OVRD, to mute the flap
aural warning.
(8) FLAPS ..................................................................Select to 20° for landing.
(9) Approach speed ...................................VREF (Flaps 45°)
+ 14 KIAS minimum.
(10) Actual landing distance .................................... Increase as applicable by factor given
below:
WITHOUT THRUST REVERSERS WITH THRUST REVERSERS
1.55 (55%) 1.50 (50%)
CAUTION
Do not jettison fuel if trim runaway is in nose down
direction.
Fuel jettison will cause the CG to move forward requiring a
larger pull force to counter and causing any push force to
be reduced.
Consider use of fuel jettison in the event of a nose-up trim
runaway condition.
A landing may be made with fuel in the tail tank.
END
ABNORMAL PROCEDURES
Flight Controls
Vol. 1 05−11−15
REV 77, Oct 20/09
CL−604 Operating Manual
PSP 604−6
1. FLIGHT CONTROLS (CONT'D)
Q. Stabilizer Trim Malfunction
Indication: Stabilizer cannot be trimmed to the desired position. STAB CH 1 INOP status
message is not displayed.
(1) Pilot’s or copilot’s STAB TRIM
DISC switch...........................................................Press hold and release.
Check the following:
• STAB TRIM caution
message on.
• MACH TRIM caution
message on.
(2) STAB TRIM, CH2 switch/light ...........................Press in to engage.
Check STAB CH1 INOP status
message on.
NOTE
Do not engage STAB TRIM CH 1.
(3) MACH TRIM switch/light ...................................Press in to engage.
Check the following:
• MACH TRIM INOP light out,
and
• MACH TRIM caution
message out.
END
ABNORMAL PROCEDURES
Flight Controls
Vol. 1 05−11−16
REV 77, Oct 20/09
CL−604 Operating Manual
PSP 604−6
1. FLIGHT CONTROLS (CONT'D)
R. Aileron PCU Malfunction
Indication: AILERON PCU caution message on.
If control response is such that intended flight path cannot be maintained:
At a safe altitude:
(1) ROLL DISC handle..............................PULL and TURN 90 degrees to lock.
NOTE
1. The pilot with the operative aileron will be required to maintain a roll
control input to offset the effects of the aileron PCU malfunction.
2. If the right aileron control circuit is inoperative, the autopilot system
is inoperative.
(2) Land at the nearest suitable airport.
NOTE
Controllability is reduced. Select longest runway available with
minimum turbulence and crosswind.
Prior to landing:
(3) GPWS/FLAP OVRD switch
(if installed) ...........................................................Select to OVRD, to mute the flap
aural warning.
(4) FLAPS ..................................................................Select to 20° for landing.
(5) Approach speed ...................................VREF (Flaps 45°)
+ 14 KIAS minimum.
(6) Actual landing distance .................................... Increase as applicable by factor given
　
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