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INOP status messages out.
STAB TRIM caution message persists:
Yes
(3) STAB TRIM, CH2 switch/light....................Press in to engage.
Check STAB CH1 INOP
status message on.
STAB TRIM caution message still persists:
Yes
NOTE
1. Minimize changes to airspeed and configuration to
minimize control forces or autopilot servo loads.
2. Disregard MACH TRIM caution message.
No
(3) MACH TRIM switch/light ...................................Press in to engage. Check the
following:
• MACH TRIM INOP light out.
• MACH TRIM caution
message out.
− END −
ABNORMAL PROCEDURES
Flight Controls
05−11−11
REV 77, Oct 20/09
▼
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. FLIGHT CONTROLS (CONT'D)
O. Stabilizer Trim Failure (Cont’d)
Autopilot is engaged:
Yes
(4) Autopilot....................................... Consider leaving
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
05−11−12
REV 77, Oct 20/09
▼
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. FLIGHT CONTROLS (CONT'D)
O. 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
05−11−13
REV 77, Oct 20/09
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. FLIGHT CONTROLS (CONT'D)
P. 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
05−11−14
REV 77, Oct 20/09
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. FLIGHT CONTROLS (CONT'D)
Q. Aileron PCU Malfunction
Indication: AILERON PCU caution message on.
　
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