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colour to indicate wing anti-ice
on.
(13) Leave icing conditions.
EMERGENCY PROCEDURES
Electrical
03−11−2
REV 71, Oct 31/07
▼
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. ELECTRICAL (CONT'D)
A. Loss of All Normal Electrical Power (Cont’d)
No
(12) CAS messages................................................... Review affected systems.
The following significant systems are not available when on emergency power
only:
• Yaw damper 2 and AFCS 2
• Flaps, ground spoilers
• Stabilizer trim channel 1
• Mach trim, aileron and rudder trim
• Hydraulic pumps 1B, 2B & 3A
• DME, FMS 2, GPS
On airplanes 5301 to 5386 not incorporating SB 604−24−002:
• FMS 1
• Copilot’s PFD, MFD, navigation & communication systems
• R Pack
• Right probe heaters, AOA vane heater and ice detector
• Nose wheel steering system, anti-skid system
• Both windshield heaters, right window heater
• Copilot’s instrument lights, NAV lights, and L & R landing lights
• SPS altitude compensation
NOTE
1. With Mach trim not available, do not exceed 250 KIAS
(0.7 M), unless the autopilot is engaged and functioning
normally.
2. Without probe and AOA vane heaters, do not rely on stall
protection system, standby altimeter, indicated airspeed
indicator and Cabin Pressure Acquisition Module.
(13) Land at the nearest suitable airport.
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.
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.
EMERGENCY PROCEDURES
Electrical
03−11−3
REV 71, Oct 31/07
▼
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. ELECTRICAL (CONT'D)
A. Loss of All Normal Electrical Power (Cont’d)
(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
03−11−4
REV 74, Nov 07/08
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
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.
　
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