曝光台 注意防骗
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Yes
(5) Other engine ...................................Shutdown
− END −
No
(5) No further action required.
− END −
No
In-flight:
(1) Affected ENG STOP switch/light .......................Press in to stop starter.
(2) IGNITION, A (B) switch/light............................Press out to disarm applicable ignition
system.
Check ARM light out at
applicable switch/light.
(3) Affected ENG START circuit
breaker (L–1L10) (R–1L9)..................................... Open
EMERGENCY PROCEDURES
Power Plant
03−03−21
REV 76, Jul 17/09
▼
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. POWER PLANT (CONT'D)
J. Engine Starter Fails to Cutout (Cont’d)
Engine is still motoring:
Yes
(4) Affected 10 ST B/AIR SOV
circuit breaker (L–4C11)
(R–2F11) ....................................................... Open
(5) Land at the nearest suitable airport.
− END −
No
(4) No further action required.
END
EMERGENCY PROCEDURES
Power Plant
03−03−22
REV 76, Jul 17/09
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. POWER PLANT (CONT'D)
K. Uncommanded Acceleration
Indication: Engine accelerates to thrust settings other than as selected with thrust
lever.
On ground:
(1) Affected thrust lever .......................... Confirm and IDLE then SHUT OFF.
During flight:
(1) Affected thrust lever .......................... Confirm and IDLE Check engine response.
Engine responds:
Yes
NOTE
To prevent engine overspeed when selecting ENG SPEED
switches OFF, N2 indications should be referenced instead
of N1.
(2) Affected thrust lever......................................Adjust to below 79% N2.
(3) Affected ENGINE CONTROL
ENG SPEED switch.........................................OFF
(4) Affected thrust lever..................................Advance
(5) Affected engine...........................................Monitor
CAUTION
Do not change power settings abruptly as engine response
is degraded.
NOTE
1. To minimize asymmetric thrust, both ENG SPEED
switches should be selected OFF prior to approach and
landing.
2. Exercise caution to prevent overspeed during thrust
reverser use, when operating with ENG SPEED
switches OFF.
3. The APR system is inoperative when the ENG SPEED
switches are selected OFF.
− END −
No
(2) In-Flight Engine Failure/Shutdown .............. Accomplish Refer to Chapter 5;
ABNORMAL PROCEDURES
– POWER PLANT – In-Flight
Engine Failure/Shutdown.
END
EMERGENCY PROCEDURES
Power Plant
03−03−23
REV 76, Jul 17/09
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
EMERGENCY PROCEDURES
Power Plant
03−03−24
REV 76, Jul 17/09
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
THIS PAGE INTENTIONALLY LEFT BLANK
1. SMOKE/FIRE/FUMES
WARNING
Time is critical during smoke/fire/fumes emergencies. The flight
crew should consider an immediate landing anytime the situation
cannot be controlled.
The flight crew must don oxygen masks/goggles at the first
indication of a concentration of smoke or fumes or suspected
contaminated air.
CAUTION
Passenger oxygen masks should not be deployed when performing
smoke or fire procedures.
To continue to destination, the flight crew must acknowledge that
the threat has been positively identified, confirmed to be
extinguished and the smoke/fumes have dissipated.
NOTE
As part of Standard Operating Procedures for in-flight emergencies,
PASS SIGNS switches are assumed to have been selected ON.
A. Smoke or Fumes Removal Procedure
WARNING
Accomplish Smoke or Fumes Removal Procedure if at any time
smoke/fumes become the greatest threat or after the source
has been eliminated.
(1) Oxygen masks/goggles
(if required) .............................................................. Don Set to 100% and
EMERGENCY.
(2) Crew communication....................................... Establish Set MASK/BOOM switch to
MASK.
Prepare to land immediately at the nearest suitable airport.
(3) Descent ............................................................... Initiate to 10,000 feet or lowest safe
altitude, whichever is higher.
(4) Passenger oxygen................................................Select to CLOSED.
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庞巴迪挑战者604飞机飞行手册CL604 Airplane Flight Manual 1(67)
