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ABNORMAL PROCEDURES
Instruments System
Vol. 1 05−15−6
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
THIS PAGE INTENTIONALLY LEFT BLANK
1. LANDING GEAR, WHEEL AND BRAKE SYSTEM
A. Inboard Anti-Skid Failure
Indication: A/SKID INBD caution message on.
NOTE
A/SKID INBD caution message indicates anti-skid braking is lost on 1 or
2 inboard wheels, or parking brake shut-off valve has failed (PARK
BRAKE SOV caution message on).
CAUTION
Extreme caution is required during braking to avoid tire damage or
blowout. Maximize use of reverse thrust.
(1) Actual landing distance .................................... Increase as applicable by factor given
below:
WITHOUT THRUST REVERSERS WITH THRUST REVERSERS
2.05 (105%) 1.65 (65%)
If excessive asymmetry or loss of braking is observed:
(2) Wheel brakes ....................................................Release momentarily.
(3) ANTI-SKID switch.................................................Select to OFF.
(4) Wheel brakes .................................................. Re-apply as required.
END
ABNORMAL PROCEDURES
Landing Gear, Wheel and Brake System
Vol. 1 05−16−1
REV 74, Nov 07/08
CL−604 Operating Manual
PSP 604−6
1. LANDING GEAR, WHEEL AND BRAKE SYSTEM (CONT'D)
B. Outboard Anti-Skid Failure
Indication: A/SKID OUTBD caution message on.
NOTE
A/SKID OUTBD caution message indicates anti-skid braking is lost on 1
or 2 outboard wheels.
CAUTION
Extreme caution is required during braking to avoid tire damage or
blowout. Maximize use of reverse thrust.
(1) Actual landing distance .................................... Increase as applicable by factor given
below:
WITHOUT THRUST REVERSERS WITH THRUST REVERSERS
2.05 (105%) 1.65 (65%)
If excessive asymmetry or loss of braking is observed:
(2) Wheel brakes ....................................................Release momentarily.
(3) ANTI-SKID switch.................................................Select to OFF.
(4) Wheel brakes .................................................. Re-apply as required.
END
C. Anti-Skid (Inboard and Outboard) Failure
Indication: A/SKID INBD caution message and A/SKID OUTBD caution message on.
NOTE
A/SKID INBD and A/SKID OUTBD caution messages indicate anti-skid
braking is lost on 2 or more wheels.
(1) ANTI-SKID switch.................................................Select to OFF.
CAUTION
Extreme caution is required during braking to avoid tire damage or
blowout. Maximize use of reverse thrust.
(2) Actual landing distance .................................... Increase as applicable by factor given
below:
WITHOUT THRUST REVERSERS WITH THRUST REVERSERS
2.05 (105%) 1.65 (65%)
END
ABNORMAL PROCEDURES
Landing Gear, Wheel and Brake System
Vol. 1 05−16−2
REV 74, Nov 07/08
CL−604 Operating Manual
PSP 604−6
1. LANDING GEAR, WHEEL AND BRAKE SYSTEM (CONT'D)
D. Inboard/Outboard Brake Pressure Low
Indication: INBD (OUTBD) BRAKE PRESS caution message on.
(1) Hydraulic pressure and fluid
quantity...............................................................Monitor for the affected system.
(2) Actual landing distance .................................... Increase as applicable by factor given
below:
WITHOUT THRUST REVERSERS WITH THRUST REVERSERS
1.70 (70%) 1.50 (50%)
NOTE
Maximize the use of reverse thrust.
END
E. Parking Brake Shut-Off Valve Failure
Indication: PARK BRAKE SOV caution message on.
NOTE
PARK BRAKE SOV caution message indicates that the parking brake
SOV is failed or is closed with the parking brake not set, possibly
affecting inboard anti-skid system performance.
CAUTION
Extreme caution is required during braking to avoid tire damage or
blowout. Maximize use of reverse thrust.
(1) Actual landing distance .................................... Increase as applicable by factor given
below:
WITHOUT THRUST REVERSERS WITH THRUST REVERSERS
2.05 (105%) 1.65 (65%)
END
ABNORMAL PROCEDURES
Landing Gear, Wheel and Brake System
Vol. 1 05−16−3
REV 74, Nov 07/08
CL−604 Operating Manual
PSP 604−6
1. LANDING GEAR, WHEEL AND BRAKE SYSTEM (CONT'D)
F. Main Landing Gear Overheat Detector Failure
Indication: MLG OVHT FAIL caution message on.
Failure occurs within 30 minutes after take-off:
Yes
(1) Airspeed .................................................... Reduce to 197 KIAS.
(2) Altitude....................................................... Reduce to below 20,000 feet, but not
　
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