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WHEEL AND BRAKE
SYSTEM – Landing Gear
Manual Extension procedure
in this chapter.
(8) 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 −
No
(3) HYDRAULIC pump switch 3B .............................. Leave at ON.
(4) Hydraulic pressure and fluid
quantity...............................................................Monitor
END
ABNORMAL PROCEDURES
Hydraulic Power
Vol. 1 05−13−3
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
1. HYDRAULIC POWER (CONT'D)
D. System No. 1 High Temperature
Indication: HYD 1 HI TEMP caution message on and temperature readouts greater than
96°C (205°F).
NOTE
Disregard HYD 1 HI TEMP caution if one other hydraulic system has
already failed.
During flight:
Temperature is less than 107°C (225°F):
Yes
(1) HYDRAULIC pump switch
1B .................................................................Select to OFF.
(2) System No. 1 temperature..........................Monitor
− END −
No
Temperature is less than 135°C (275°F):
Yes
(1) HYDRAULIC pump switch
1B .................................................................Select to OFF.
(2) System No. 1 temperature..........................Monitor
(3) Land at the nearest suitable airport.
− END −
No
(1) HYDRAULIC pump switch 1B ..............................Select to OFF.
(2) Left engine......................................................Shutdown Refer to POWER PLANT –
In-Flight Engine
Failure/Shutdown in this
chapter.
(3) Inoperative systems ........................................... Review Refer to HYDRAULIC page.
(4) Actual landing distance .................................... Increase by a factor of 1.60 (60%).
END
ABNORMAL PROCEDURES
Hydraulic Power
Vol. 1 05−13−4
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
1. HYDRAULIC POWER (CONT'D)
E. System No. 2 High Temperature
Indication: HYD 2 HI TEMP caution message on and temperature readouts greater than
96°C (205°F).
NOTE
Disregard HYD 2 HI TEMP caution if one other hydraulic system has
already failed.
During flight:
Temperature is less than 107°C (225°F):
Yes
(1) HYDRAULIC pump switch
2B .................................................................Select to OFF.
(2) System No. 2 temperature..........................Monitor
− END −
No
Temperature is less than 135°C (275°F):
Yes
(1) HYDRAULIC pump switch
2B .................................................................Select to OFF.
(2) System No. 2 temperature..........................Monitor
(3) Land at the nearest suitable airport.
− END −
No
(1) HYDRAULIC pump switch 2B ..............................Select to OFF.
(2) Right engine ...................................................Shutdown Refer to POWER PLANT –
In-Flight Engine
Failure/Shutdown in this
chapter.
(3) Inoperative systems ........................................... Review Refer to HYDRAULIC page.
(4) Actual landing distance .................................... Increase by a factor of 2.25 (125%).
END
ABNORMAL PROCEDURES
Hydraulic Power
Vol. 1 05−13−5
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
1. HYDRAULIC POWER (CONT'D)
F. System No. 3 High Temperature
Indication: HYD 3 HI TEMP caution message on and temperature readouts greater than
96°C (205°F).
During flight:
(1) HYDRAULIC pump switches 3A
and 3B ..................................................................Select to OFF.
(2) System No. 3 temperature .................................Monitor
Temperature is more than 107°C (225°F):
Yes
(3) Land at the nearest suitable airport.
No
Prior to landing:
(3) HYDRAULIC pump switches 3A
and 3B ...................................................... Select to ON.
END
G. Engine-Driven Pump Failure
Indication: HYD EDP 1A (2A) caution message on.
(1) Associated HYDRAULIC pump
switch 1B or 2B ....................................................Select to ON.
(2) Hydraulic pressure and fluid
quantity.................................................................Check
System quantity low:
　
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