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Yes
(5) FUEL, L (R) TO AUX
XFLOW switch/light ........................... Press in to open affected crossflow
valve.
Check L (R) TO AUX XFLOW
ON light on.
NOTE
Anticipate increasing lateral trim and control forces.
When trim or control forces becomes excessive:
(6) FUEL, L (R) TO AUX
XFLOW switch/light .........................Press out to close affected crossflow
valve.
Check L (R) TO AUX XFLOW
ON light out.
ABNORMAL PROCEDURES
Fuel
05−12−27
REV 74, Nov 07/08
▼
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. FUEL (CONT'D)
AC. Fuel Leak Procedure (Cont’d)
(7) Repeat steps (5) and (6), as necessary to conserve as much fuel as possible
from the leaking tank.
(8) Fuel tank quantity
readouts..............................................Monitor
NOTE
Consider use of asymmetric thrust to maintain fuel
imbalance within limits.
No
(5) Fuel tank quantity readouts ................................Monitor
NOTE
Consider use of asymmetric thrust to maintain fuel imbalance
within limits.
Landing with a FUEL IMBALANCE caution message:
Yes
NOTE
Select the longest runway available with minimum turbulence
and crosswind.
Prior to landing:
(6) GPWS/FLAP OVRD switch
(if installed) ...................................................Select to OVRD, to mute the flap
aural warning.
(7) FLAPS ..........................................................Select to 20° for landing.
(8) Approach speed ...........................VREF (Flaps 45°)
+ 14 KIAS minimum.
(9) Actual landing distance............................. Increase as applicable by factor given
below:
WITHOUT THRUST REVERSERS WITH THRUST REVERSERS
1.55 (55%) 1.50 (50%)
− END −
No
(6) No further action required.
END
ABNORMAL PROCEDURES
Fuel
05−12−28
REV 74, Nov 07/08
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. HYDRAULIC POWER
A. System No. 1 Failure
Indication: HYD 1 LO PRESS caution message on.
(1) HYDRAULIC pump switch 1B ..............................Select to ON.
(2) Hydraulic pressure and fluid
quantity.................................................................Check
No. 1 quantity readout is less than 5%, or pressure is less than 1,800 psi, or pressure is
rapidly decreasing:
Yes
(3) HYDRAULIC pump switch
1B .................................................................Select to OFF.
(4) Land at the nearest suitable airport.
(5) Inoperative systems.................................... Review Refer to HYDRAULIC page.
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.
(6) ANTI-SKID switch......................................... Leave ARMED.
(7) GPWS/FLAP OVRD switch
(if installed) ...................................................Select to OVRD, to mute the flap
aural warning.
(8) FLAPS ..........................................................Select to 20° for landing.
(9) Approach speed ...........................VREF (Flaps 45°)
+ 14 KIAS minimum.
(10) Actual landing distance............................. Increase as applicable by factor given
below:
WITHOUT THRUST REVERSERS WITH THRUST REVERSERS
1.60 (60%) 1.55 (55%)
− END −
No
(3) HYDRAULIC pump switch 1B .............................. Leave at ON.
(4) Hydraulic pressure and fluid
quantity...............................................................Monitor
END
ABNORMAL PROCEDURES
Hydraulic Power
05−13−1
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. HYDRAULIC POWER (CONT'D)
B. System No. 2 Failure
Indication: HYD 2 LO PRESS caution message on.
(1) HYDRAULIC pump switch 2B ..............................Select to ON.
(2) Hydraulic pressure and fluid
quantity.................................................................Check
No. 2 quantity readout is less than 5%, or pressure is less than 1,800 psi, or pressure is
rapidly decreasing:
Yes
(3) HYDRAULIC pump switch
2B .................................................................Select to OFF.
(4) Land at the nearest suitable airport.
(5) Inoperative systems.................................... Review Refer to HYDRAULIC page.
NOTE
The engine-driven pump (EDP) is operating without
hydraulic fluid; log length of time that EDP has been
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庞巴迪挑战者604飞机飞行手册CL604 Airplane Flight Manual 2(16)
