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Check APU LCV OPEN light
on.
EMERGENCY PROCEDURES
Power Plant
Vol. 1 03−03−7
REV 76, Jul 17/09
▼
CL−604 Operating Manual
PSP 604−6
1. POWER PLANT (CONT'D)
C. Double Engine Failure (Cont’d)
Attempt to start one engine at a time.
At 15,000 feet and below:
On airplanes 5301 to 5630 NOT incorporating Service Bulletin 604–49–006 or
604–49–009:
At 10,000 feet and below:
(19) IGNITION, CONT switch/light..............Confirm ON
(20) ENG, L (R) START
switch/light ......................................................Push Check L (R) ENG START light
on.
When ITT is 90°C or less and N2 reaches 28%:
(21) Thrust lever.....................................................IDLE
(22) Engine indications ......................................Monitor engine acceleration, ITT and
oil pressure.
Engine relights within 25 seconds (stable IDLE within 2 minutes):
Yes
(23) Thrust lever...................................As required
On airplanes 5301 to 5407:
NOTE
Maximum airspeed for continuous operation of the
ADG is 250 knots.
Operating engine:
(24) Applicable AC POWER,
GEN switch...........................................Check generator set to ON.
Check applicable GEN 1 OFF
and/or GEN 2 OFF caution
message out.
On airplanes 5301 to 5630 NOT incorporating Service Bulletin 604–49–006
or 604–49–009:
(25) AC POWER, APU GEN
switch....................................................Select to OFF.
(26) BLEED AIR, APU LCV
switch/light .......................................Press out to close LCV.
Check APU LCV OPEN light
out.
EMERGENCY PROCEDURES
Power Plant
Vol. 1 03−03−8
REV 76, Jul 17/09
▼
CL−604 Operating Manual
PSP 604−6
1. POWER PLANT (CONT'D)
C. Double Engine Failure (Cont’d)
(27) Applicable BLEED AIR,
10TH STAGE switch/light ..................Press in to open bleed air valve.
Check applicable 10TH
STAGE CLOSED light out.
(28) Applicable
AIR-CONDITIONING,
PACK switch/light .............................. Press in to restart pack.
Check applicable PACK OFF
light out.
NOTE
Use only one air-conditioning pack during single
engine operations, unless the APU is the bleed
source.
(29) IGNITION, CONT
switch/light .......................................Press out to select continuous ignition
off.
Check IGNITION A/B advisory
message out.
Re-establish normal power:
(30) ADG, PWR TXFR
OVERRIDE switch.................................Press to override.
(31) CAS messages................................... Review
(32) Affected systems ............................... Restore
(33) Other engine........................................... Start Refer to Chapter 5;
ABNORMAL PROCEDURES
– AIR START.
Only one engine is operating:
Yes
(34) In-Flight Engine
Failure/Shutdown..................Accomplish Refer to Chapter 5;
ABNORMAL PROCEDURES
– POWER PLANT – In-Flight
Engine Failure/Shutdown.
− END −
No
(34) No further action required.
− END −
No
(23) Affected thrust lever..............................SHUT OFF
EMERGENCY PROCEDURES
Power Plant
Vol. 1 03−03−9
REV 76, Jul 17/09
▼
CL−604 Operating Manual
PSP 604−6
1. POWER PLANT (CONT'D)
C. Double Engine Failure (Cont’d)
(24) Affected ENG STOP switch.......................Press in to stop starter.
Another APU bleed air relight attempt is feasible:
Yes
(25) Airspeed............................Maintain 240 KIAS minimum.
(26) Attempt relight on other engine.
No
(25) Proceed to All Engine Out Procedure.
No
All Engine Out Procedure:
(15) IGNITION, CONT switch/light..........................Press out to select continuous ignition
off.
Check IGNITION A/B advisory
message out.
(16) Airspeed .......................................................... Establish best glide speed.
Airplane Weight Target Airspeed Rate of Descent (Flaps 0°)
20,865 KG (46,000 LB) 211 KIAS 1835 fpm
13,607 KG (30,000 LB) 173 KIAS 1600 fpm
NOTE
1. Target glide speed provides a range of approximately
2.5 NM for each 1,000 feet altitude.
2. Refer to Flight Planning and Cruise Control Manual,
Chapter 6: Special Operational Data – Descent with
Two Engines Inoperative, for detailed descent
(time/distance) performance data.
　
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