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Yes
(3) Affected thrust lever.................... Confirm and
SHUT OFF
(4) In−Flight Engine
Failure/Shutdown..........................Accomplish Refer to Chapter 5;
ABNORMAL PROCEDURES
– POWER PLANT – In−Flight
Engine Failure/Shutdown.
− END −
No
(3) Affected thrust lever .............................................Adjust as required.
(4) Engine instruments.............................................Monitor
END
EMERGENCY PROCEDURES
Power Plant
Vol. 1 03−03−14
REV 76, Jul 17/09
CL−604 Operating Manual
PSP 604−6
1. POWER PLANT (CONT'D)
F. Uncommanded Thrust Reverser Deployment in Flight
Indication: L (R) REV UNLOCKED caution message.
Affected engine:
(1) Thrust lever ....................................... Confirm and IDLE
(2) THRUST REVERSER, L (R)
EMER STOW switch/light..................................Press in Note that:
• L (R) REV UNLOCKED
caution message will
remain,
• REV icon out, and
• Stow indicated by
improved airplane handling
and normal operation of
affected thrust lever.
(3) Airspeed .................................................. Not more than 200 KIAS.
Anti-ice is on:
Yes
(4) ANTI-ICE, WING switch ...............................Select to OFF.
(5) Affected ANTI-ICE, COWL
switch/light ...............................................Press out to select cowl anti-ice off.
No
Thrust reverser fails to stow:
Yes
Thrust lever locked at idle, and continued airplane buffet and yaw:
(4) In-Flight Engine
Failure/Shutdown................................. Accomplish Refer to Chapter 5;
ABNORMAL PROCEDURES
– POWER PLANT – In-Flight
Engine Failure/Shutdown.
CAUTION
Do not relight engine.
EMERGENCY PROCEDURES
Power Plant
Vol. 1 03−03−15
REV 76, Jul 17/09
▼
CL−604 Operating Manual
PSP 604−6
1. POWER PLANT (CONT'D)
F. Uncommanded Thrust Reverser Deployment in Flight (Cont’d)
(5) Land at the nearest suitable airport.
Anti-ice is required:
Yes
(6) BLEED AIR, 14TH
STAGE ISOL switch/light...................Press in to open ISOL valve.
Check 14TH ISOL OPEN light
on.
(7) ANTI-ICE, WING switch........................Select to NORM.
No
Prior to landing:
(6) Final approach speed ........................Not less than VREF (Flaps 45°) + 22 KIAS.
(7) Actual landing distance............................. Increase by a factor of 1.70 (70%).
− END −
No
CAUTION
Limit airspeed to not more than 200 KIAS.
(4) Thrust levers................................................ As required
(5) THRUST REVERSER, L and R
switches................................................................Select to OFF.
Check L and R REV ARMED
advisory messages out.
CAUTION
Do not arm thrust reverser.
(6) Land at the nearest suitable airport.
Anti-ice is required:
Yes
(7) ANTI-ICE, WING switch ...............................Select to NORM.
(8) Affected ANTI-ICE, COWL
switch/light .................................................Press in to select cowl anti-ice on.
EMERGENCY PROCEDURES
Power Plant
Vol. 1 03−03−16
REV 76, Jul 17/09
▼
CL−604 Operating Manual
PSP 604−6
1. POWER PLANT (CONT'D)
F. Uncommanded Thrust Reverser Deployment in Flight (Cont’d)
No
Prior to landing:
(7) GPWS/FLAP OVRD switch
(if installed) ...........................................................Select to OVRD (to mute flap aural
warning).
(8) FLAPS ..................................................................Select to 20° for landing.
(9) Final approach speed................................Not less than VREF (Flaps 45°) + 22 KIAS.
(10) Actual landing distance .................................... Increase by a factor of 1.70 (70%).
END
EMERGENCY PROCEDURES
Power Plant
Vol. 1 03−03−17
REV 76, Jul 17/09
CL−604 Operating Manual
PSP 604−6
1. POWER PLANT (CONT'D)
G. Post-Shutdown Engine Tail Pipe Fire
Indication: Engine ITT exceeds 350°C and ITT is rising rapidly, or if flame is reported
at engine tailpipe.
Affected engine:
(1) Dry motor..................................................... Accomplish until ITT is reduced below
150°C or starter limit.
NOTE
The APU or ground air source (if available) may be used to dry motor
the engine.
Tail pipe fire indications persist:
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庞巴迪挑战者604操作手册 Operating Manual 1(41)
