曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

CL−604 Airplane Flight Manual
PSP 604−1
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
05−02−10
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
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 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 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
05−03−1
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. SINGLE ENGINE PROCEDURES (CONT'D)
B. Engine Failure During Approach
(1) Autopilot ....................................................... Disconnect if coupled approach.
(2) Operating engine.............................................. Increase thrust as required.
(3) FLIGHT SPOILER lever .......................................Select to RETRACT.
Check EICAS indicates
spoilers retracted.
(4) FLAPS ..................................................................Select to 20° for landing.
(5) Airspeed ........................................................... Increase to VREF (Flaps 45°) + 14 KIAS
(6) Airplane ............................................................... Retrim and continue approach, or
go-around at pilot’s discretion
(Refer to Single Engine
Go-Around, in this section).
If required, autopilot may be
re-engaged, if above 800 feet
AGL.
If continuing the approach:
(7) AIR-CONDITIONING, L and R
PACKs.............................................................. Transfer to APU bleed air.
(8) Go-Around thrust........................................... Determine applicable single engine climb
thrust (APR rating) (Refer to
Chapter 6; PERFORMANCE –
THRUST SETTINGS).
(9) GPWS/FLAP OVRD switch
(if installed) ...........................................................Select to OVRD (to mute flap aural
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：龐巴迪挑戰者604飛機飛行手冊CL604 Airplane Flight Manual 1(129)