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+ 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
05−11−4
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
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
05−11−5
REV 77, Oct 20/09
▼
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
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
Reversers)
0 30 1.80 (80%) 1.75 (75%)
20 14 1.55 (55%) 1.50 (50%)
30 7 1.40 (40%) 1.35 (35%)
NOTE
1. Accomplish a normal descent typically with a vertical speed
of not more than 400 fpm at touchdown.
2. Improper landing technique during a flaps failure can
generate nose gear loads sufficient to cause structural
damage.
3. To prevent damage:
• After main gear touchdown, gently lower the nose to the
runway.
• Apply brakes only after nose wheel touchdown.
4. When using thrust reversers, the maximum nose-up pitching
moment, due to reverse thrust, occurs at 0 degrees flaps,
light weight and aft CG. This moment is controllable with
elevator. Before selecting reverse thrust, ensure that
nosewheel touch down is achieved, with nose-down elevator
applied and flight and ground spoilers deployed.
ABNORMAL PROCEDURES
Flight Controls
05−11−6
REV 77, Oct 20/09
▼
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. FLIGHT CONTROLS (CONT'D)
J. Flaps Failure (Cont’d)
Example: If failure occurs at Flaps – 28 degrees:
Maximum Enroute
Airspeed = VFE for Flaps 30 degrees
Approach & Landing
Speed = VREF (Flaps 45°) + 14 KIAS
Factor Applied to Actual
Landing Distance (without
Thrust Reversers) = 1.55 (55%)
Factor Applied to Actual
Landing Distance (with
Thrust Reversers) = 1.50% (50%)
NOTE
If the failure occurs with the flaps at a detented flap position,
use the VFE, VREF and landing distance factor relative to the flap
position.
END
ABNORMAL PROCEDURES
Flight Controls
05−11−7
REV 77, Oct 20/09
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. FLIGHT CONTROLS (CONT'D)
K. Ground Spoilers Failure
Indication: GND SPLRS NOT ARMED caution message on.
(1) GND SPOILERS switch .......................................Select to ARM.
　
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