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PSP 604−1
THIS PAGE INTENTIONALLY LEFT BLANK
1. FLIGHT CONTROLS
A. Lightning Strike
Following a lightning strike, failure of the stall protection system may occur without an
associated indication to the crew. Failure of the stall protection system must be assumed.
(1) STALL PROT, PUSHER switch
(either left or right) ................................................Select to OFF.
NOTE
Stick shakers remain operative.
Prior to landing:
(2) Approach speed ...................................VREF (Flaps 45°)
+ 10 KIAS minimum, to maintain margin
above stall.
(3) Actual landing distance .................................... Increase as applicable by factor given
below:
WITHOUT THRUST REVERSERS WITH THRUST REVERSERS
1.40 (40%) 1.30 (30%)
END
ABNORMAL PROCEDURES
Flight Controls
05−11−1
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. FLIGHT CONTROLS (CONT'D)
B. Stall Protection System Failure
Indication: STALL FAIL caution message on.
(1) STALL PROT, PUSHER switch
(either left or right) ................................................Select to OFF.
NOTE
Stick shakers remain operative.
Accompanied by a nuisance shaker operation and/or warbler aural warning:
Yes
(2) Affected STALL PROT, L CH
or R CH circuit breaker (1N5
or 4C5)........................................................... Open
No
Prior to landing:
(2) Approach speed ...................................VREF (Flaps 45°)
+ 10 KIAS minimum, to maintain margin
above stall.
(3) Actual landing distance .................................... Increase as applicable by factor given
below:
WITHOUT THRUST REVERSERS WITH THRUST REVERSERS
1.40 (40%) 1.30 (30%)
END
C. Stall Protection System Altitude Compensation Failure
Indication: ALT COMP FAIL caution message on.
NOTE
The stick pusher may be inoperative. One or both channels of the stick
shaker will remain operative.
Prior to landing:
(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
1.40 (40%) 1.30 (30%)
END
ABNORMAL PROCEDURES
Flight Controls
05−11−2
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. FLIGHT CONTROLS (CONT'D)
D. Flight Spoilers Deployed During Flight
Indication: FLT SPLRS DEPLOY caution message on.
(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
05−11−3
REV 74, Nov 07/08
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
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°)
　
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