曝光臺 注意防騙 網(wǎng)曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費(fèi)者

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
Vol. 1 05−16−7
REV 74, Nov 07/08
CL−604 Operating Manual
PSP 604−6
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
Vol. 1 05−16−8
REV 74, Nov 07/08
▼
CL−604 Operating Manual
PSP 604−6
1. LANDING GEAR, WHEEL AND BRAKE SYSTEM (CONT'D)
J. Proximity Sensing System Failure (Total System Shutdown) (Cont’d)
(8) Actual landing distance .................................... Increase as applicable by factor given
below:
WITHOUT THRUST REVERSERS WITH THRUST REVERSERS
2.20 (120%) 1.75 (75%)
END
ABNORMAL PROCEDURES
Landing Gear, Wheel and Brake System
Vol. 1 05−16−9
REV 74, Nov 07/08
CL−604 Operating Manual
PSP 604−6
1. LANDING GEAR, WHEEL AND BRAKE SYSTEM (CONT'D)
K. Landing Gear Manual Extension
(1) Airspeed ............................................................ Reduce to not more than:
• Flaps 0° – 181 KIAS.
• Flaps 20° – 197 KIAS.
• Flaps 30° – 197 KIAS.
• Flaps 45° – 189 KIAS.
CAUTION
Leave hydraulic pump 3B OFF if pump was selected OFF due to a low
or decreasing pressure, or a low quantity in system No. 3.
(2) HYDRAULIC pump switches 2B
and 3B ..................................................................Select to ON.
(3) LDG GEAR lever ..................................................Select to DN.
NOTE
The landing gear lever can be cycled UP and DN. The load required to
operate the LANDING GEAR MANUAL RELEASE handle is greater
than 40 pounds. The flight crew may choose to reposition the seat prior
to handle deployment.
(4) LANDING GEAR MANUAL
RELEASE handle ..................................................PULL to full extension.
NOTE
The NOSE DOOR OPEN warning message may be displayed when
manual gear extension is accomplished.
If the nose landing gear is in transition this message will be inhibited.
(5) Landing gear indication ........................................Check for three DN indications.
Three landing gear symbols indicate DN:
Yes
CAUTION
Do not stow LANDING GEAR MANUAL RELEASE handle until
gear locking pins are installed.
Nose wheel steering may not be available upon landing.
(6) No further action required.
− END −
ABNORMAL PROCEDURES
Landing Gear, Wheel and Brake System
Vol. 1 05−16−10
REV 74, Nov 07/08
▼
CL−604 Operating Manual
PSP 604−6
1. LANDING GEAR, WHEEL AND BRAKE SYSTEM (CONT'D)
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：龐巴迪挑戰(zhàn)者604操作手冊 Operating Manual 2(33)