曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

quantity.................................................................Check
No. 2 and No. 3 quantity readouts are less than 5%, or pressure is less than 1,800 psi,
or pressure is rapidly decreasing:
Yes
(4) HYDRAULIC pump switches
2B, 3A and 3B ..............................................Select to OFF, to prevent pump
overheat.
(5) Inoperative systems.................................... Review Refer to HYDRAULIC page.
(6) Land at the nearest suitable airport.
NOTE
1. Control is limited with No. 2 and No. 3 hydraulic
systems failed.
2. Select the longest runway available with minimal
crosswind and turbulence.
3. Rudder control is adequate for normal flight and should
be used in coordination with aileron, if necessary,
during turns.
Prior to landing:
(7) NOSE STEER switch ...................................Select to OFF.
(8) ANTI-SKID switch.........................................Select to OFF.
(9) Landing Gear Manual
Extension procedure............................ Accomplish Refer to LANDING GEAR,
WHEEL AND BRAKE
SYSTEM – Landing Gear
Manual Extension procedure
in this chapter.
NOTE
1. Unless it is possible to restore use of No. 2 hydraulic
system, landing gear extension relies upon gear free
fall after use of gear manual extension control.
2. A sideslip, for each side, must be performed to achieve
MLG down-lock. It may be required to increase
airspeed to ensure down-lock during sideslip.
(10) GPWS/FLAP OVRD switch
(if installed) ...................................................Select to OVRD, to mute the flap
aural warning.
ABNORMAL PROCEDURES
Hydraulic Power
Vol. 1 05−13−10
REV 74, Nov 07/08
▼
CL−604 Operating Manual
PSP 604−6
1. HYDRAULIC POWER (CONT'D)
N. System No. 2 and No. 3 Failure (Cont’d)
(11) FLAPS ..........................................................Select to 20° for landing.
(12) Approach speed ...........................VREF (Flaps 45°)
+ 14 KIAS minimum.
NOTE
The above double hydraulic system failure has an
extremely remote probability. If it occurs, maximum use of
reverse thrust must be used upon landing.
(13) Actual landing distance............................. Increase by a factor of 3.50 (250%).
CAUTION
Extreme caution is required during braking to avoid tire
damage. Maximize use of reverse thrust.
Upon landing:
(14) Both engines..................................................Apply maximum reverse thrust.
(15) Brakes ...........................................................Apply light to moderate braking until
safe taxi speed is maintained.
(16) Brake pressure ...........................................Monitor Approximately six (6) full
brake applications are
possible using brake
accumulator pressure.
NOTE
INBD and OUTBD BRAKE PRESS caution messages come
on at less than 1,015 psi.
− END −
No
(4) No further action required.
END
ABNORMAL PROCEDURES
Hydraulic Power
Vol. 1 05−13−11
REV 74, Nov 07/08
CL−604 Operating Manual
PSP 604−6
1. HYDRAULIC POWER (CONT'D)
O. System No. 1 and No. 3 Failure
Indication: HYD 1 LO PRESS and HYD 3 LO PRESS caution messages on.
(1) Airspeed ..........................................................200 KIAS maximum.
(2) HYDRAULIC pump switches (all).........................Select to ON.
(3) Hydraulic pressure and fluid
quantity.................................................................Check
No. 1 and No. 3 quantity readouts are less than 5%, or pressure is less than 1,800 psi,
or pressure is rapidly decreasing:
Yes
(4) HYDRAULIC pump switches
1B, 3A and 3B ..............................................Select to OFF.
(5) Inoperative systems.................................... Review Refer to HYDRAULIC page.
(6) NOSE STEER switch ...................................Select to OFF.
(7) ANTI-SKID switch......................................... Leave ARMED.
(8) Land at the nearest suitable airport.
NOTE
1. Flight path control is limited with No. 1 and No. 3
hydraulic systems failed.
2. Select the longest runway available with minimal
crosswind and turbulence.
3. Rudder control is adequate for normal flight and should
be used in coordination with aileron during turns.
(9) Landing Gear Manual
Extension procedure............................ Accomplish Refer to LANDING GEAR,
WHEEL AND BRAKE
SYSTEM – Landing Gear
Manual Extension procedure
in this chapter.
Prior to landing:
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：龐巴迪挑戰者604操作手冊 Operating Manual 2(25)