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come on at less than 1,015 psi.
− END −
No
(4) No further action required.
END
ABNORMAL PROCEDURES
Hydraulic Power
05−13−11
REV 74, Nov 07/08
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
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:
(10) GPWS/FLAP OVRD switch
(if installed) ...................................................Select to OVRD, to mute the flap
aural warning.
(11) FLAPS ..........................................................Select to 20° for landing.
(12) Approach speed ...........................VREF (Flaps 45°)
+ 14 KIAS minimum.
ABNORMAL PROCEDURES
Hydraulic Power
05−13−12
REV 74, Nov 07/08
▼
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. HYDRAULIC POWER (CONT'D)
O. System No. 1 and No. 3 Failure (Cont’d)
(13) Actual landing distance............................. Increase as applicable by factor given
below:
WITHOUT THRUST REVERSERS WITH THRUST REVERSERS
2.40 (140%) 1.90 (90%)
NOTE
Maximize use of reverse thrust.
− END −
No
(4) No further action required.
END
ABNORMAL PROCEDURES
Hydraulic Power
05−13−13
REV 74, Nov 07/08
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
ABNORMAL PROCEDURES
Hydraulic Power
05−13−14
REV 74, Nov 07/08
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
THIS PAGE INTENTIONALLY LEFT BLANK
1. ICE AND RAIN PROTECTION
NOTE
1. With both 14th stage bleed air shut-off valves closed, cowl
anti-icing, wing anti-icing and thrust reversers are not available.
2. If above 40,000 feet, one air-conditioning unit or cowl anti-ice
must be selected on for each engine.
A. Ice Dispersal Procedure
After leaving icing conditions, and if ice accumulation is observed on the heated
portion of the wing leading edge:
(1) Airspeed ........................................................... Increase to VMO/MMO, if possible, to
disperse ice.
Impossible to remove ice from the wing leading edge:
Yes
Assure adequate stall margin:
(2) Maneuvering airspeed .......................Not less than
200 KIAS
Prior to landing:
(3) GPWS/FLAP OVRD switch
(if installed) ...................................................Select to OVRD, to mute the flap
aural warning.
(4) FLAPS ..........................................................Select to 20° for landing.
(5) Approach speed ...........................VREF (Flaps 45°)
+ 27 KIAS
(6) Actual landing distance............................. Increase as applicable by factor given
below:
WITHOUT THRUST REVERSERS WITH THRUST REVERSERS
1.80 (80%) 1.70 (70%)
At 50 feet AGL:
(7) Thrust levers...................................................IDLE and do not prolong the landing
flare.
WARNING
Even small accumulations of ice on the wing leading edge
can change the stall speed, stall characteristics or the
warning margins provided by the stall protection system.
− END −
No
　
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