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No
(5) R PACK ................................................................................ OFF
(6) Cabin altitude ..............................................................MONITOR
(7) Descent ...............................................................AS REQUIRED
On airplanes 5301 to 5407:
CAUTION
Do not exceed 250 KIAS with ADG
deployed.
(8) GEN 1 and GEN 2................................................... OFF/RESET
then ON.
Any generator comes on-line:
Yes
Re-establish normal power:
No
(9) APU (20,000 feet and below) ...........................................START
On airplanes 5301 to 5630 without SB 604–49–006 or
604–49–009:
(9) APU (15,000 feet and below) ...........................................START
(10) APU GEN ............................................................................... ON
EMER 9-2
REV 71, Oct 31/07
▼
QUICK REFERENCE HANDBOOK
PSP 604-15 ELECTRICAL EMERGENCY
EMER PWR ONLY (Cont’d)
Any generator comes on-line:
Yes
Re-establish normal power:
(11) ADG PWR TXFR...............................................OVERRIDE
(12) HYDRAULIC pump 3B ........................................ AUTO/ON
(13) CAS messages...................................................... REVIEW
(14) Affected systems ................................................ RESTORE
− END −
No
(11) Descent .....................................................................CONTINUE
to 10,000 feet or lowest safe altitude, if required.
Wing anti-ice is required:
Yes
(12) WING ANTI-ICE ......................................................... STBY
(13) Leave icing conditions.
No
(12) CAS messages.............................................................. REVIEW
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 trims,
• Hydraulic pumps 1B, 2B & 3A,
• DME, FMS 2, GPS,
On airplanes 5301 to 5386 without SB 604−24−002:
• FMS 1
• Copilot’s PFD, MFD, NAV and COMM systems,
• Right pack,
• Right probe heaters, AOA vane heater and ice detector,
• Nose wheel steering system, anti-skid system.
• Both windshield heaters, right window heaters,
• Copilot’s instrument lights, NAV, and L & R landing lights,
• SPS altitude compensation.
NOTE
With Mach trim not available, do not exceed 250 KIAS
(0.7 M), unless the autopilot is engaged and functioning
normally.
EMER 9-3
REV 74, Nov 07/08
▼
QUICK REFERENCE HANDBOOK
PSP 604-15 ELECTRICAL EMERGENCY
EMER PWR ONLY (Cont’d)
NOTE
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
1. For flight planning, a fuel burn correction of 5%
should be used when the ADG is deployed.
2. 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.
3. Hydraulic pump 3B will be inoperative when on
battery power only.
Prior to landing:
(14) ADG manual deploy handle ................................................PULL
(15) GPWS/FLAP OVRD (if installed)....................................... OVRD
to mute flap aural warning.
(16) Final approach speed.............................................VREF + ΔVREF
See 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
(See ABNORM 13–9)
− END −
No
(18) No further action required.
END
EMER 9-4
REV 74, Nov 07/08
QUICK REFERENCE HANDBOOK
PSP 604-15 ELECTRICAL EMERGENCY
CONTENTS PAGE
Primary Flight Controls
• Aileron System Jammed .............................................. EMER 10−2
　
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