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I. Weight-on-Wheels Output Fault
Indication: WOW OUTPUT caution message on.
The following may occur:
• PFD, speed trend vector inoperative.
• PFD, low speed cue comes on; HSI portion indicates TA ONLY,
• RTU indicates TCAS STANDBY and ATC 1(2) STANDBY,
• Inadvertent take-off configuration warnings, and
• Fuel quantity fluctuates during pitch and bank maneuvers.
On ground:
Yes
(1) Do not take off.
(2) ADG DEPLOY CONT, AUTO
circuit breaker (2N6) ...................................... Open to prevent inadvertent
deployment during
APU/engine shutdown.
(3) CRT Display temperatures .........................Monitor for possible overheat.
− END −
No
In flight:
(1) Manual Cabin Pressurization
Control Procedure ....................................... Accomplish Refer to AIR-CONDITIONING
AND PRESSURIZATION –
Manual Cabin Pressurization
Control Procedure in this
chapter.
(2) GND SPOILERS switch .......................................... Set to DISARM.
(3) NOSE STEER switch ...........................................Select to OFF.
STALL FAIL caution message is on:
Yes
(4) Stall Protection System
Failure Procedure ................................ Accomplish Refer to FLIGHT CONTROLS
– Stall Protection System
Failure procedure in this
chapter.
No
After touchdown:
(4) GND SPOILERS switch .......................................Select to ARM.
ABNORMAL PROCEDURES
Landing Gear, Wheel and Brake System
05−16−6
REV 74, Nov 07/08
▼
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. LANDING GEAR, WHEEL AND BRAKE SYSTEM (CONT'D)
I. Weight-on-Wheels Output Fault (Cont’d)
If loss of braking occurs below 35 knots:
(5) ANTI-SKID switch.................................................Select to OFF.
CAUTION
Extreme caution is required during braking to avoid tire damage
or blowout. Maximize use of reverse thrust.
If nose wheel steering is required:
(6) NOSE STEER switch ...........................................Select to ARMED.
After landing:
(7) ADG DEPLOY CONT, AUTO
circuit breaker (2N6).............................................. Open to prevent inadvertent ADG
deployment during shutdown.
END
ABNORMAL PROCEDURES
Landing Gear, Wheel and Brake System
05−16−7
REV 74, Nov 07/08
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. LANDING GEAR, WHEEL AND BRAKE SYSTEM (CONT'D)
J. Proximity Sensing System Failure (Total System Shutdown)
Indication: PROX SYS caution message on, GND SPLRS caution message on, and
landing gear symbols (nose, left and right main gear) display amber dash
marks (position unknown) with landing gear lever UP or DN.
NOTE
1. EICAS landing gear position indications are inoperative.
2. Normal landing gear extension/retraction is not available.
3. Anti-skid, ground spoilers and nose wheel steering systems are
inoperative.
4. Nose door open warning system is not available.
(1) Airspeed ............................................................ Reduce to not more than:
• Flaps 0° – 181 KIAS.
• Flaps 20° – 197 KIAS.
• Flaps 30° – 197 KIAS.
• Flaps 45° – 189 KIAS.
(2) HYDRAULIC pump switches 2B
and 3B ..................................................................Select to ON.
(3) LDG GEAR lever ..................................................Select to DN.
(4) LANDING GEAR MANUAL
RELEASE handle .....................................................Pull to release landing gear.
Confirm gear position with
control tower.
(5) GND SPOILERS switch ........................................... Set to DISARM.
(6) ANTI-SKID switch..................................................... Set to OFF.
CAUTION
Extreme caution is required during braking to avoid tire damage
or blow out. Maximize use of reverse thrust.
(7) NOSE STEER switch ...........................................Select to OFF.
NOTE
If landing with nosewheel steering inoperative, select the longest
runway available with minimum turbulence and crosswind. Use
differential braking, rudder, and engine thrust as required during taxi.
ABNORMAL PROCEDURES
Landing Gear, Wheel and Brake System
05−16−8
REV 74, Nov 07/08
▼
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. LANDING GEAR, WHEEL AND BRAKE SYSTEM (CONT'D)
J. Proximity Sensing System Failure (Total System Shutdown) (Cont’d)
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庞巴迪挑战者604飞机飞行手册CL604 Airplane Flight Manual 2(27)
