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2. LANDING DISTANCE FACTORS
Landing distance factors are provided herein with and without the use of thrust reversers. No
operation should be predicated on the use of thrust reversers.
ABNORMAL PROCEDURES
Introduction
05−01−1
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
ABNORMAL PROCEDURES
Introduction
05−01−2
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
THIS PAGE INTENTIONALLY LEFT BLANK
1. POWER PLANT
A. Reverser Unsafe to Arm
Indication: L (R) REV UNSAFE caution message.
CAUTION
Do not arm affected thrust reverser during flight.
(1) Affected THRUST REVERSER
ARM switch .............................................................OFF L (R) REV ARMED advisory
message out.
CAUTION
Use remaining thrust reverser carefully upon landing.
END
B. In-Flight Engine Failure/Shutdown
Accomplish an engine shutdown only when flight conditions permit.
Shut down the engine if any of the following malfunction symptoms/indications occur:
• Excessive or uncontrollable power changes, or
• Indications outside the engine operating limitations, or
• Unsuccessful restart attempts after an unexplained flameout, or
• Any other condition that indicates advisability of engine shutdown.
(1) Affected engine, thrust lever.............. Confirm and IDLE
(2) Affected engine, thrust lever............ Confirm and SHUT
OFF
(3) FUEL, TAIL TANK TRANSFER,
MANUAL OVRD switch/light ...........................Press out if MANUAL light on, and if
rotor burst is suspected.
Anti-ice system is on:
Yes
(4) BLEED AIR, 14TH STAGE
ISOL switch/light........................................Press in to open 14th stage isolation
valve.
Check ISOL OPEN light on.
(5) ANTI-ICE, COWL L (R)
switch/light ...............................................Press out to select applicable cowl
anti-ice off.
No
ABNORMAL PROCEDURES
Power Plant
05−02−1
REV 66, Feb 01/07
▼
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. POWER PLANT (CONT'D)
B. In-Flight Engine Failure/Shutdown (Cont’d)
HYD 1 (2) HI TEMP caution message is out:
Yes
(4) HYDRAULIC pump switch............................Select applicable pump to ON.
• If left engine shut down,
turn 1B ON. Check that
HYD 1 LO PRESS caution
message out.
• If right engine shut down,
turn 2B ON. Check that
HYD 2 LO PRESS caution
message out.
No
(4) AIR-CONDITIONING,
L (R) PACK switch/light ...................................Press out to shutdown affected pack.
Check L (R) PACK OFF light
on.
(5) BLEED AIR, 10TH STAGE
L (R) switch/light ..............................................Press out to close affected shut-off
valve.
Check L (R) CLOSED light on.
NOTE
Use only one air-conditioning pack during single engine
operations, when the operating engine is the only 10th-stage
bleed source.
(6) AC POWER, GEN 1 (2) switch.............................Select affected generator to OFF.
Check GEN 1 (2) OFF caution
message on.
(7) APU (if available).................................................... Start when at or below 20,000 feet.
On airplanes 5301 to 5630 NOT incorporating Service Bulletin 604–49–006 or
604–49–009:
(7) APU (if available).................................................... Start when at or below 15,000 feet.
ABNORMAL PROCEDURES
Power Plant
05−02−2
REV 66, Feb 01/07
▼
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. POWER PLANT (CONT'D)
B. In-Flight Engine Failure/Shutdown (Cont’d)
On airplanes 5301 to 5630 NOT incorporating Service Bulletin 604–49–006 or
604–49–009:
CAUTION
Use of the APU generator in flight is not permitted unless both main
generators have failed or are off-line.
(8) AC POWER, APU GEN switch.............................Select to ON.
(9) Fuel system ..........................................................Check and monitor the following:
• Fuel quantity, and
• Fuel balance.
(10) Leave icing conditions (if possible).
NOTE
Icing conditions exist in flight at a TAT of 10°C (50°F) or below
and visible moisture in any form is encountered (such as
clouds, rain, snow, sleet or ice crystals), except when the SAT
is –40°C (−40°F) or below.
　
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