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below:
WITHOUT THRUST REVERSERS WITH THRUST REVERSERS
1.55 (55%) 1.50 (50%)
END
ABNORMAL PROCEDURES
Flight Controls
Vol. 1 05−11−17
REV 77, Oct 20/09
CL−604 Operating Manual
PSP 604−6
1. FLIGHT CONTROLS (CONT'D)
S. Elevator System Malfunction
Indication: ELEVATOR SPLIT caution message on.
(1) Elevator controls......................................... Move slowly and monitor position on
EICAS to identify
malfunctioning elevator
surface.
If control response is such that intended flight path cannot be maintained:
At a safe altitude:
(2) Elevator controls................................................Release Release pilot/copilot
differential pressure on the
controls.
(3) PITCH DISC handle ............................PULL and TURN 90 degrees to lock.
(4) Jammed side ................................................. Determine If left side, do not re-engage
autopilot.
Right side jammed:
Yes
(5) STALL PROT, PUSHER
switch (either left or right) .............................Select to OFF.
NOTE
Stick shaker on operative control column, operates at a
lower intensity.
No
(5) Land at the nearest suitable airport.
NOTE
Controllability is reduced. Select the longest runway available
with minimum turbulence and crosswind.
Prior to landing:
(6) GPWS/FLAP OVRD switch
(if installed) ...........................................................Select to OVRD, to mute the flap
aural warning.
(7) FLAPS ..................................................................Select to 20° for landing.
(8) Approach speed ...................................VREF (Flaps 45°)
+ 14 KIAS minimum.
(9) Actual landing distance .................................... Increase as applicable by factor given
below:
WITHOUT THRUST REVERSERS WITH THRUST REVERSERS
1.55 (55%) 1.50 (50%)
END
ABNORMAL PROCEDURES
Flight Controls
Vol. 1 05−11−18
REV 77, Oct 20/09
CL−604 Operating Manual
PSP 604−6
1. FUEL
A. Fuel Imbalance
Indication: FUEL IMBALANCE caution message on. Left and right fuel quantity readouts
indicate amber.
CAUTION
If a fuel imbalance caution message is displayed:
• Do not taxi until imbalance is rectified.
• Do not land until imbalance is rectified, unless a greater
emergency exists.
NOTE
1. The maximum permissible fuel imbalance is 182 kg (400 lb) for
take-off, taxi, and landing.
2. The maximum permissible fuel imbalance is 363 kg (800 lb) in flight.
(1) Fuel distribution ..................................................Monitor to identify appropriate action
required.
Affected high tank:
(2) FUEL, L (R) TO AUX XFLOW
switch/light .........................................................Press in to open crossflow valve.
Check L (R) TO AUX XFLOW
ON light on.
(3) Fuel tank quantity readouts ................................Monitor
When tank quantities have equalized:
(4) FUEL, affected L (R) TO AUX
XFLOW switch/light .........................................Press out to close crossflow valve.
Check L (R) TO AUX XFLOW
ON light out.
ABNORMAL PROCEDURES
Fuel
Vol. 1 05−12−1
REV 74, Nov 07/08
▼
CL−604 Operating Manual
PSP 604−6
1. FUEL (CONT'D)
A. Fuel Imbalance (Cont’d)
Fuel imbalance persists:
Yes
(5) FUEL, GRAVITY/XFLOW
switch/light .................................................Press in to open gravity crossflow
valve.
Check GRAVITY XFLOW
OPEN light on.
NOTE
1. A steady heading sideslip will accelerate gravity
crossflow operation. Fly one wing low slip (on the side
with less fuel) to ensure proper operation and to
accelerate gravity crossflow.
2. During uncoordinated flight, fuel indications are
inaccurate. Accurate fuel indications will be obtained
after 30 seconds when level and stabilized in
coordinated flight.
On the low quantity side:
(6) Affected engine.......................................... Reduce thrust.
(7) Fuel tank quantity readouts ........................Monitor
When main tank quantities have equalized:
(8) FUEL, GRAVITY/XFLOW
switch/light ...............................................Press out to close gravity crossflow
valve.
Check GRAVITY XFLOW
OPEN light out.
(9) Fuel tank quantity readouts ........................Monitor
Imbalance persists (fuel leak from wing tank is suspected):
Yes
(10) Fuel Leak Procedure ....................Accomplish Refer to Fuel Leak Procedure
　
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