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protection system, standby altimeter, indicated airspeed
indicator and Cabin Pressure Acquisition Module.
(13) Land at the nearest suitable airport.
NOTE
For flight planning, a fuel burn correction of 5% should be used
when the ADG is deployed.
NOTE
If the ADG is not operating properly and the airplane is on
battery power only, then all electrical power may be lost after 30
minutes.
Hydraulic pump 3B will be inoperative when on battery power
only.
EMERGENCY PROCEDURES
Electrical
Vol. 1 03−11−3
REV 74, Nov 07/08
▼
CL−604 Operating Manual
PSP 604−6
1. ELECTRICAL (CONT'D)
A. Loss of All Normal Electrical Power (Cont’d)
Prior to landing:
(14) ADG manual deploy handle ..................................PULL
(15) GPWS/FLAP OVRD switch
(if installed) ...........................................................Select to OVRD, to mute the flap
aural warning.
(16) Final approach speed...........................VREF (Flaps 45°)
+ ΔVREF for flap setting position when
failure occurred, as shown by
table below.
(17) Actual landing distance .................................... Increase as applicable by factor given
below:
FLAPS
SETTING
(DEGREES)
Δ VREF
(KTS)
ALD FACTOR
WITHOUT THRUST
REVERSERS
WITH THRUST
REVERSERS
0 30 3.60 (260%) 2.50 (150%)
20 14 3.20 (220%) 2.20 (120%)
30 7 2.85 (185%) 2.05 (105%)
45 2.50 (150%) 1.85 (85%)
HYD 3 LO PRESS caution message is on:
Yes
(18) Landing Gear Manual
Extension Procedure ........................... Accomplish Refer to Chapter 5;
ABNORMAL PROCEDURES
– LANDING GEAR, WHEEL
AND BRAKE SYSTEM –
Landing Gear Manual
Extension.
− END −
No
(18) No further action required.
END
EMERGENCY PROCEDURES
Electrical
Vol. 1 03−11−4
REV 74, Nov 07/08
CL−604 Operating Manual
PSP 604−6
1. FLIGHT CONTROLS
A. Aileron System Jammed
Indication: Higher than normal flight control forces.
NOTE
With a jammed primary flight control, it may be necessary to
reduce airspeed to improve airplane handling.
(1) Autopilot ....................................................... Disconnect if coupled.
(2) Aileron controls............................................. Overpower Attempt to overpower jammed
condition.
Attempt to use aileron trim to
alleviate forces on controls, if
jam has occurred away from
neutral position.
Jam persists:
Yes
(3) Aileron controls..........................................Release Release pilot/copilot
differential pressure on the
controls.
(4) ROLL DISC handle......................PULL and TURN 90 degrees to lock.
(5) Jammed side ......................................... Determine If right side, do not re-engage
autopilot.
No
(3) Land at the nearest suitable airport.
NOTE
Controllability is reduced. Select longest runway available with
minimum turbulence and crosswind.
Prior to landing:
(4) GPWS/FLAP OVRD switch
(if installed) ...........................................................Select to OVRD, to mute the flap
aural warning.
(5) FLAPS ..................................................................Select to 20° for landing.
(6) Approach speed ...................................VREF (Flaps 45°)
+ 14 KIAS minimum.
(7) Actual landing distance .................................... Increase as applicable by factor given
below:
WITHOUT THRUST REVERSERS WITH THRUST REVERSERS
1.55 (55%) 1.50 (50%)
END
EMERGENCY PROCEDURES
Flight Controls
Vol. 1 03−12−1
REV 74, Nov 07/08
CL−604 Operating Manual
PSP 604−6
1. FLIGHT CONTROLS (CONT'D)
B. Elevator System Jammed
Indication: Higher than normal flight control forces.
NOTE
With a jammed primary flight control, it may be necessary to
reduce airspeed to improve airplane handling.
(1) Autopilot ....................................................... Disconnect if coupled.
(2) Elevator controls........................................... Overpower Attempt to overpower jammed
condition.
Use stabilizer trim to
compensate, if elevator jam
has occurred away from the
trimmed position.
Jam persists:
Yes
(3) Elevator controls........................................Release Release pilot/copilot
differential pressure on the
controls.
(4) PITCH DISC handle ....................PULL and TURN 90 degrees to lock.
　
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