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− 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
05−13−5
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
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:
Yes
(3) Associated HYDRAULIC
pump switch 1B or 2B...................................Select to OFF.
NOTE
The engine-driven pump (EDP) is operating without
hydraulic fluid; log length of time that EDP has been
running dry. Monitor fluid temperature readouts.
− END −
No
(3) No further action required.
END
ABNORMAL PROCEDURES
Hydraulic Power
05−13−6
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. HYDRAULIC POWER (CONT'D)
H. Electric Pump 1B Failure
Indication: HYD PUMP 1B caution message on.
(1) HYDRAULIC pump switch 1B .............................Select to ON.
HYD PUMP 1B caution message persists:
Yes
(2) HYDRAULIC pump switch
1B .................................................................Select to OFF.
− END −
No
(2) No further action required.
END
I. Electric Pump 2B Failure
Indication: HYD PUMP 2B caution message on.
(1) HYDRAULIC pump switch 2B .............................Select to ON.
HYD PUMP 2B caution message persists:
Yes
(2) HYDRAULIC pump switch
2B .................................................................Select to OFF.
− END −
No
(2) No further action required.
END
J. Electric Pump 3A Failure
Indication: HYD PUMP 3A caution message on.
(1) HYDRAULIC pump switches 3A
and 3B .................................................................Select both to ON.
HYD PUMP 3A caution message persists:
Yes
(2) HYDRAULIC pump switch
3A .................................................................Select to OFF.
− END −
No
(2) No further action required.
END
ABNORMAL PROCEDURES
Hydraulic Power
05−13−7
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. HYDRAULIC POWER (CONT'D)
K. Electric Pump 3B Failure
Indication: HYD PUMP 3B caution message on.
(1) HYDRAULIC pump switches 3A
and 3B .................................................................Select both to ON.
HYD PUMP 3B caution message persists:
Yes
(2) HYDRAULIC pump switch
3B .................................................................Select to OFF.
− END −
No
(2) No further action required.
END
L. Hydraulic Shut-Off Valve Failure After Engine Shutdown Due to Fire
Indication: HYD SOV 1 (2) caution message on.
(1) Land at the nearest suitable airport.
END
ABNORMAL PROCEDURES
Hydraulic Power
05−13−8
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. HYDRAULIC POWER (CONT'D)
M. System No. 1 and No. 2 Failure
Indication: HYD 1 LO PRESS and HYD 2 LO PRESS caution messages on.
(1) HYDRAULIC pump switches (all).........................Select to ON.
(2) Hydraulic pressure and fluid
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庞巴迪挑战者604飞机飞行手册CL604 Airplane Flight Manual 2(18)
