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(14) ANTI-ICE, L and R COWL
switch/lights .....................................................Press out to select cowl anti-ice off.
EMERGENCY PROCEDURES
Power Plant
03−03−4
REV 76, Jul 17/09
▼
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. POWER PLANT (CONT'D)
C. Double Engine Failure (Cont’d)
WARNING
To avoid thermal seizure, increase airspeed as required to maintain at
least 4% N2 indicated. If the N2 is allowed to drop to 0%, the engine
may thermally seize and may not rotate even at higher airspeeds or
with starter engagement.
NOTE
1. Between 21,000 feet and 10,000 feet, a minimum of 12% N2 is
necessary for a windmill relight.
2. At 10,000 feet and below, a minimum of 10% N2 is necessary for a
windmill relight.
3. Acceleration to VMO is recommended to attain the necessary N2 for
a windmill relight.
4. The altitude loss when accelerating from 240 KIAS to VMO , could be
more than 5,000 feet.
5. A push-over to as steep as 15° nose down may be required.
Windmill relight is feasible:
Yes
(15) Glide airspeed .............................. Increase to VMO
CAUTION
The resulting high rate of descent (up to 7800 fpm) will
cause a significant reduction of available gliding distance.
On airplanes 5301 to 5407:
NOTE
With the ADG deployed, an airspeed of 330 knots is
permitted for 12 minutes, and an airspeed of between 331
to 348 knots is permitted for 4 minutes.
(16) Descent ....................................................... Initiate to 21,000 feet or below, at
VMO.
(17) FUEL, L and R BOOST
PUMP switch/lights..............................Confirm ON
At 21,000 feet and below, attempt to start both engines at the same time.
When ITT is ≤ 90°C and N2 is ≥ 12% (between 21,000 feet and 10,000 feet) or
N2 is ≥ 10% (10,000 feet and below):
(18) IGNITION, CONT switch/light..............Confirm ON
(19) Thrust levers (both) ........................................IDLE
EMERGENCY PROCEDURES
Power Plant
03−03−5
REV 76, Jul 17/09
▼
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. POWER PLANT (CONT'D)
C. Double Engine Failure (Cont’d)
(20) Engine indications ......................................Monitor engine acceleration, ITT and
oil pressure.
At least one engine relights within 25 seconds (stable IDLE within 2 minutes):
Yes
(21) Thrust lever(s)...............................As required
On airplanes 5301 to 5407:
NOTE
Maximum airspeed for continuous operation of the
ADG is 250 knots.
Operating engine(s):
(22) Applicable AC POWER,
GEN switch(es).....................................Check generator(s) set to ON.
Check applicable GEN 1 OFF
and/or GEN 2 OFF caution
message(s) out.
On airplanes 5301 to 5630 NOT incorporating Service Bulletin 604–49–006
or 604–49–009:
(23) AC POWER, APU GEN
switch....................................................Select to OFF.
(24) Applicable
AIR-CONDITIONING,
PACK switch/light(s) .......................... Press in to restart pack(s).
Check applicable PACK OFF
light(s) out.
NOTE
Use only one air-conditioning pack during single
engine operations, unless the APU is the bleed
source.
(25) IGNITION, CONT
switch/light .......................................Press out to select continuous ignition
off.
Check IGNITION A/B advisory
message out.
Re-establish normal power:
(26) ADG, PWR TXFR
OVERRIDE switch.................................Press to override.
(27) CAS messages................................... Review
EMERGENCY PROCEDURES
Power Plant
03−03−6
REV 76, Jul 17/09
▼
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. POWER PLANT (CONT'D)
C. Double Engine Failure (Cont’d)
(28) Affected systems ............................... Restore
Only one engine is operating:
Yes
(29) In-Flight Engine
Failure/Shutdown..................Accomplish Refer to Chapter 5;
ABNORMAL PROCEDURES
– POWER PLANT – In-Flight
Engine Failure/Shutdown.
− END −
No
(29) No further action required.
− END −
No
(21) Thrust levers (both) ..............................SHUT OFF
Another windmill relight attempt is feasible:
Yes
(22) Airspeed.....................................Maintain VMO
(23) Wait 30 seconds, then repeat windmill relight procedure.
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庞巴迪挑战者604飞机飞行手册CL604 Airplane Flight Manual 1(62)
