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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
Vol. 1 05−11−6
REV 77, Oct 20/09
▼
CL−604 Operating Manual
PSP 604−6
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
Vol. 1 05−11−7
REV 77, Oct 20/09
CL−604 Operating Manual
PSP 604−6
1. FLIGHT CONTROLS (CONT'D)
K. Flap System Reset (On Ground)
Indication: FLAPS FAIL caution message on. FLIGHT CONTROLS page displays flap
outline in amber.
WARNING
Attempting to reset the flaps system in flight is not permitted.
(1) FLAPS ..................................................................Select between flap detent positions
(e.g., between 0 and 20).
(2) FLAP CONT 1 and FLAP CONT 2
circuit breakers (1F3 and 2F3) .............................. Open
(3) FLAP CONT 1 and FLAP CONT 2
circuit breakers (1F3 and 2F3) ..............................Close Check FLAPS FAIL caution
message out.
FLAPS FAIL caution message persists:
Yes
(4) Do not take-off.
− END −
No
(4) FLAPS ..................................................................Select to 0.
(5) Flap alignment......................................................Check alignment of inboard and
outboard flaps on each wing is
within tolerance shown on
Figure 05−11−1 .
Alignment is within tolerance:
Yes
(6) No further action required.
− END −
No
(6) Do not take-off.
ABNORMAL PROCEDURES
Flight Controls
Vol. 1 05−11−8
REV 77, Oct 20/09
▼
CL−604 Operating Manual
PSP 604−6
1. FLIGHT CONTROLS (CONT'D)
K. Flap System Reset (On Ground) (Cont’d)
LF604_05_001
INBOARD FLAP
OUTBOARD FLAP
OUTBOARD FLAP WING INBOARD FLAP
FLAPS IN 0−DEGREE POSITION WHEN POP MARKS ARE IN LINE ±0.063 INCH
Flap System Reset
Figure 05−11−1
END
ABNORMAL PROCEDURES
Flight Controls
Vol. 1 05−11−9
REV 77, Oct 20/09
CL−604 Operating Manual
PSP 604−6
1. FLIGHT CONTROLS (CONT'D)
L. Ground Spoilers Failure
Indication: GND SPLRS NOT ARMED caution message on.
(1) GND SPOILERS switch .......................................Select to ARM.
GND SPLRS NOT ARMED caution message persists:
Yes
(2) Actual landing distance............................. Increase as applicable by factor given
below:
WITHOUT THRUST REVERSERS WITH THRUST REVERSERS
1.30 (30%) 1.25 (25%)
NOTE
Landing distance factors for failed ground spoilers are
based upon serviceable flight spoilers.
After touchdown:
(3) FLIGHT SPOILER lever ...............................Select to MAX.
− END −
No
(2) No further action required.
END
M. Ground Spoilers Unsafe
Indication: GND SPLRS caution message on.
On ground:
Yes
NOTE
GND SPLRS caution message may come on at taxi speeds
above 16 knots.
(1) Airplane .......................................................... Stop
(2) Ground spoilers pre-flight
check ................................................... Accomplish Refer to the Airplane Flight
　
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