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(10) Actual landing distance .................................... Increase by a factor of 1.70 (70%).
END
EMERGENCY PROCEDURES
Power Plant
03−03−17
REV 76, Jul 17/09
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
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:
Yes
(2) ENG FIRE PUSH switch/light ....................Press in to close fuel SOV to affected
engine. Check the following:
• BOTTLE ARMED PUSH TO
DISCH lights on, and
• L (R) ENG SOV CLSD
advisory message on.
(3) Passenger Evacuation
procedure ............................................ As required Refer to EMERGENCY
EVACUATION – Passenger
Evacuation procedure in this
chapter.
(4) Control tower ............................ Inform of condition and request fire fighting
assistance.
− END −
No
(2) No further action required.
END
EMERGENCY PROCEDURES
Power Plant
03−03−18
REV 76, Jul 17/09
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. POWER PLANT (CONT'D)
H. N1/N2 Overspeed
Indication: ENGINE warning message. Engine N1 or N2 readout indicates engine
limits being exceeded.
(1) Affected thrust lever .........................Confirm and retard until engine responds.
Engine limits continue to be exceeded:
Yes
(2) In-Flight Engine
Failure/Shutdown................................. Accomplish Refer to Chapter 5;
ABNORMAL PROCEDURES
– POWER PLANT – In-Flight
Engine Failure/Shutdown.
− END −
No
(2) Both thrust levers ................................................ Retard to below 79% N2.
(3) ENGINE CONTROL both ENG
SPEED switches .....................................................OFF to prevent asymmetric thrust.
NOTE
The APR system is inoperative when the ENG SPEED switches
are selected OFF.
(4) Affected thrust lever .........................................Advance
NOTE
Thrust lever controls are more sensitive to changes.
Engine accelerates to desired power:
Yes
(5) Affected engine...........................................Monitor
− END −
No
(5) In-Flight Engine Failure/Shutdown .............. Accomplish Refer to Chapter 5;
ABNORMAL PROCEDURES
– POWER PLANT – In-Flight
Engine Failure/Shutdown.
END
EMERGENCY PROCEDURES
Power Plant
03−03−19
REV 76, Jul 17/09
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. POWER PLANT (CONT'D)
I. Engine Overtemperature
Indication: ENGINE warning message. Engine ITT readout indicates engine limits
being exceeded.
(1) Affected thrust lever .........................Confirm and retard until ITT below limit range.
ITT limits continue to be exceeded:
Yes
(2) In-Flight Engine
Failure/Shutdown................................. Accomplish Refer to Chapter 5;
ABNORMAL PROCEDURES
– POWER PLANT – In-Flight
Engine Failure/Shutdown.
− END −
No
(2) No further action required.
END
EMERGENCY PROCEDURES
Power Plant
03−03−20
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
Indication: L (R) ENGINE START SOV warning message. L (R) ENGINE START light
and IGNITION A (B) advisory message on after 55% N2.
On ground:
Yes
(1) Affected ENG STOP
switch/light .................................................Press in to stop starter.
Starter cutout is confirmed:
Yes
(2) No further action required.
− END −
No
(2) Affected engine.......................................Shutdown
(3) Affected BLEED AIR, 10TH
STAGE, L (R) switch/light........................Press out to close bleed air valve.
Check L (R) 10TH STAGE
CLOSED light on.
(4) BLEED AIR, APU LCV
switch/light ...............................................Press out to close APU load control
valve.
Check APU LCV OPEN light
out.
Engine is still motoring:
　
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