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1. POWER PLANT (CONT'D)
J. Thrust Lever Inoperative
Indication: Affected thrust lever inoperative.
At a safe altitude, before commencing the approach:
(1) Affected ENG FIRE PUSH
switch/light .........................................................Press in to shutdown affected engine.
BOTTLE ARMED PUSH TO
DISCH lights and L (R) ENG
SOV CLSD advisory message
on.
NOTE
Ground spoilers may not be available upon landing.
Ground spoilers will operate only if affected engine is windmilling above
40% N1.
(2) Affected engine ..............................................Shutdown Refer to In-Flight Engine
Failure/Shutdown procedure in
this section.
(3) Actual landing distance .................................... Increase by a factor of 1.60 (60%), for a
flaps 20° landing without the
use of reverse thrust.
END
ABNORMAL PROCEDURES
Power Plant
Vol. 1 05−02−10
REV 76, Jul 17/09
CL−604 Operating Manual
PSP 604−6
1. POWER PLANT (CONT'D)
K. Fluctuating Engine Oil Pressure
Indication: Left or right oil pressure readout fluctuates in excess of ±5 psi and gradually
decreases, possibly with increasing oil temperature.
Oil pressure is below 25 psi:
Yes
(1) Engine Oil Pressure Low
procedure ............................................ Accomplish Refer to Chapter 3;
EMERGENCY
PROCEDURES – POWER
PLANT – Engine Oil Pressure
Low.
− END −
No
(1) Affected thrust lever .......................... Confirm and IDLE
(2) Descent (if required) ............................................ Initiate
to 29,000 feet or below, or until oil pressure
stabilizes.
When affected engine oil pressure stabilizes:
(3) Affected thrust lever .............................................Adjust as required.
NOTE
1. If necessary, keep descending to a lower altitude to maintain
a stable oil pressure, as cruise power setting is resumed.
2. If oil pressure fluctuations in excess of ±5 psi resume, select
affected thrust lever to IDLE, and descend to a lower
altitude.
END
ABNORMAL PROCEDURES
Power Plant
Vol. 1 05−02−11
REV 76, Jul 17/09
CL−604 Operating Manual
PSP 604−6
ABNORMAL PROCEDURES
Power Plant
Vol. 1 05−02−12
REV 76, Jul 17/09
CL−604 Operating Manual
PSP 604−6
THIS PAGE INTENTIONALLY LEFT BLANK
1. SINGLE ENGINE PROCEDURES
A. Engine Failure During Take-Off After Achieving V1
(1) Take-off ........................................................... Continue
(2) Airplane ............................................................... Rotate at VR to an initial take-off
attitude of 10 degrees, and
adjust pitch, as required, to
achieve an airspeed of V2 at
35 feet.
(3) Landing gear ...................................................... Retract when positive rate of climb is
established.
(4) Airspeed ........................................................... Maintain at V2 to engine-out level-off
height (Refer to the Airplane
Flight Manual, Chapter 6;
PERFORMANCE –
OBSTACLE CLEARANCE).
NOTE
If engine failure occurs above V2, maintain airspeed at current value
(not more than V2 + 10 KIAS).
Wing anti-ice system selected on:
Yes
(5) BLEED AIR, 14TH STAGE
ISOL switch/light........................................Press in to open ISOL valve.
Check ISOL OPEN light on.
No
At not less than 400 feet AGL or the engine-out level off height:
(6) Thrust ....................................................................... Set thrust to maximum continuous
thrust (MCT) (Refer to the
Airplane Flight Manual,
Chapter 6; PERFORMANCE –
THRUST SETTINGS).
(7) Airspeed ........................................................Accelerate in level flight to VFTO.
(8) FLAPS ..................................................................Select to UP, at VFTO – 5 KIAS.
(9) Climb ................................................................... Initiate at VFTO.
At a safe altitude:
(10) Single Engine Procedure............................. Accomplish Refer to Single Engine
Procedure in this section.
END
ABNORMAL PROCEDURES
Single Engine Procedures
Vol. 1 05−03−1
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
1. SINGLE ENGINE PROCEDURES (CONT'D)
B. Engine Failure During Approach
(1) Autopilot ....................................................... Disconnect if coupled approach.
　
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