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(1) FLIGHT SPOILER lever .......................................Select to RETRACT.
END
E. Flight Spoilers Lever Jam
Indication: Flight spoilers cannot be retracted.
(1) Approach speed ...................................VREF (Flaps 45°)
+ 10 KIAS minimum.
(2) Actual landing distance .................................... Increase as applicable by factor given
below:
WITHOUT THRUST REVERSERS WITH THRUST REVERSERS
1.50 (50%) 1.40 (40%)
END
F. Flight Spoilers Failure to Deploy
Indication: Flight spoilers cannot be deployed.
(1) Actual landing distance .................................... Increase as applicable by factor given
below:
WITHOUT THRUST REVERSERS WITH THRUST REVERSERS
1.30 (30%) 1.25 (25%)
END
G. Flight Spoiler Asymmetric Extension
Indication: An uncommanded roll during flight spoiler extension.
(1) FLIGHT SPOILER lever ..................................... Retract Do not reselect in flight.
(2) Runway ................................................................Select to minimize crosswind.
(3) Actual landing distance .................................... Increase as applicable by factor given
below:
WITHOUT THRUST REVERSERS WITH THRUST REVERSERS
1.30 (30%) 1.25 (25%)
END
ABNORMAL PROCEDURES
Flight Controls
Vol. 1 05−11−3
REV 74, Nov 07/08
CL−604 Operating Manual
PSP 604−6
1. FLIGHT CONTROLS (CONT'D)
H. Flight Spoiler Asymmetric Retraction
Indication: An uncommanded roll during flight spoiler retraction.
(1) Lateral control.................................................. Establish using ailerons, and if
necessary, rudder inputs.
(2) FLIGHT SPOILER lever ...........................Retract/adjust to eliminate roll asymmetry.
Make no further adjustments
to spoilers in flight.
(3) Runway ................................................................Select to minimize crosswind.
(4) Approach speed ...................................VREF (Flaps 45°)
+ 10 KIAS minimum.
(5) Actual landing distance .................................... Increase as applicable by factor given
below:
WITHOUT THRUST REVERSERS WITH THRUST REVERSERS
1.50 (50%) 1.40 (40%)
END
I. Flight Spoilers Failure
Indication: FLT SPLRS caution message on.
On ground:
(1) Do not take off.
END
ABNORMAL PROCEDURES
Flight Controls
Vol. 1 05−11−4
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
1. FLIGHT CONTROLS (CONT'D)
J. Flaps Failure
Indication: FLAPS FAIL caution message on. FLIGHT CONTROLS page displays flap
outline in amber.
Flaps failure occurred at 0 degrees:
Yes
(1) HYDRAULIC pump switches
1B, 2B and 3B ..............................................Select to ON.
No
(1) FLAPS ..................................................................Select to closest detent position less
than actual flap position. Do
not attempt to operate flaps
any further.
(2) Maximum enroute airspeed...................................... VFE for next greater flap setting
from failed position.
NOTE
If flaps are confirmed retracted (0 degrees), reduction of cruise
airspeed is not required.
CAUTION
If possible, avoid prolonged flight in icing. If icing is encountered
for an extended period of time, aerodynamic buffet may be
experienced.
AR Certified Airplanes
Flaps failure occurred at greater than 5 degrees:
Yes
(3) Land at the nearest suitable airport.
No
Flaps failure occurred at 45 degrees:
Yes
(4) No further action required.
NOTE
If aerodynamic buffet is encountered after flying in icing
conditions, reduce buffet by increasing the minimum
approach speed to VREF (Flaps 45°) + 5 KIAS.
− END −
ABNORMAL PROCEDURES
Flight Controls
Vol. 1 05−11−5
REV 77, Oct 20/09
▼
CL−604 Operating Manual
PSP 604−6
1. FLIGHT CONTROLS (CONT'D)
J. Flaps Failure (Cont’d)
No
Prior to landing:
(4) GPWS/FLAP OVRD switch
(if installed) ...........................................................Select to OVRD, to mute the flap
aural warning.
(5) Final approach speed...........................VREF (Flaps 45°)
+ ΔVREF for next smaller flap setting
from failed position.
(6) Actual landing distance .................................... Increase as applicable by factor given
below:
Flaps Setting
(Degrees)
Δ VREF
(KTS)
ALD Factor (Without
Thrust Reversers)
ALD Factor (With Thrust
　
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