曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
(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
05−16−2
REV 74, Nov 07/08
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
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
05−16−3
REV 74, Nov 07/08
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
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
below minimum safe altitude.
(3) LDG GEAR lever ..........................................Select to DN or leave extended for
5 minutes, then retract gear
and resume climb.
− END −
No
(1) No further action required.
END
G. Nose Wheel Steering System Failure
Indication: STEERING INOP caution message on.
During taxi:
Yes
(1) Nose wheel.................................................. Centre using differential braking/
reverse thrust as required.
(2) Nose wheel steering tiller ........................... Ensure centered.
(3) Rudder pedals ............................................ Ensure centered.
NOTE
The NOSE STEER switch must be selected to ARMED to
enable the nosewheel steering circuit, and centering of the
nosewheel.
(4) NOSE STEER switch ....................................Cycle OFF and ARMED.
(5) Nose wheel steering .....................................Check responsiveness and ensure
normal operation.
Caution message persists:
Yes
(6) NOSE STEER switch............................Select to OFF.
Check STEERING INOP
caution message out.
− END −
No
(6) No further action required.
− END −
ABNORMAL PROCEDURES
Landing Gear, Wheel and Brake System
05−16−4
REV 74, Nov 07/08
▼
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. LANDING GEAR, WHEEL AND BRAKE SYSTEM (CONT'D)
G. Nose Wheel Steering System Failure (Cont’d)
No
In flight:
NOTE
Centering of the nosewheel steering tiller, rudder pedals, and/or
cycling the switch from OFF to ARMED will not enable centering
of the nosewheel.
(1) NOSE STEER switch ...........................................Select to OFF.
Check STEERING INOP
caution message out.
NOTE
1. When landing with the nosewheel steering inoperative,
select the longest runway available with minimum turbulence
and crosswind.
2. Use differential braking, rudder and engine thrust as required
to assist directional control.
END
H. Weight-on-Wheels Input Fault
Indication: WOW INPUT caution message on.
(1) NOSE STEER switch ......................................... Ensure selected to ARMED.
(2) No further action required.
END
ABNORMAL PROCEDURES
Landing Gear, Wheel and Brake System
05−16−5
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. LANDING GEAR, WHEEL AND BRAKE SYSTEM (CONT'D)
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
庞巴迪挑战者604飞机飞行手册CL604 Airplane Flight Manual 2(26)
