曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
introduce undesirable yaw moments. If a decision is made to
increase thrust during takeoff, do so smoothly and compensate
with rudder.
* * * *
737
Flight Manual
Continental
ENGINES, APU
Sec. 2.7 Page 15
Rev. 11/15/02 #41
TAKEOFF - ENGINE FAILURE AFTER V1
ENGINES, APU
Sec. 2.7 Page 16
Rev. 11/15/02 #41
Continental 737
Flight Manual
INTENTIONALLY LEFT BLANK
737
Flight Manual
Continental
ENGINES, APU
Sec. 2.7 Page 17
Rev. 11/15/02 #41
Engine Failure On Final Approach
Should an engine failure occur during final approach with the aircraft in the
landing configuration, the aircraft may not be able to maintain a normal
glideslope under the most adverse conditions in high headwinds and climb
performance limited gross weights.
Continue The Approach In The One Engine Inoperative Landing
Configuration
Upon recognition of an engine failure, disengage the autothrottle and increase
thrust concurrent with the selection of flaps 15. Speed should be increased to
VREF 30 or 40 speed plus 15 knots. This speed is equal to or greater than VREF
15. The internal speed bug may also be increased to this speed to provide
proper flight director pitch guidance for approach. Inhibit the GROUND
PROXIMITY FLAP INHIBIT switch to prevent a flap configuration warning.
Execute A Go-Around
If the Captain decides to go-around when the engine fails in the landing
configuration, disengage the autothrottle and increase thrust concurrent with the
selection of flaps 15. Speed should be increased to VREF 30 or 40 speed plus 15
knots. This speed is equal to or greater than VREF 15. The internal speed bug
may also be increased to this speed to provide proper flight director pitch
guidance for approach and go-around. After the aircraft has stabilized, the
normal single engine go-around procedures will then be accomplished.
Maintain VREF + 15, retract flaps to position 1, and continue the one engine
inoperative go-around. VREF + 15 knots is approximately equal to V2 for
flaps 1. Subsequent flap retraction should be made at 800 ft. AGL or higher
altitude if special procedures apply.
ENGINES, APU
Sec. 2.7 Page 18
Rev. 11/15/02 #41
Continental
737
Flight Manual
ENGINE FIRE / OVERHEAT DETECTOR FAULT
The detector FAULT light illuminated indicates both loops in any circuit have
failed. Neither the master caution nor the fire handle will illuminate.
The fire detection system in one or both engines is inoperative. Consideration
should be given to landing as soon as practicable.
* * * *
ENGINE HIGH OIL TEMPERATURE
Accomplish this procedure when oil temperature is in the yellow band or, at or
above the red radial.
IF Temperature Is In The Yellow Band:
Throttle (Affected Engine) ........................................................RETARD
Disconnect Autothrottles, if required.
Decreasing the thrust slowly may lower oil temperature into the green
band by reducing the amount of heat generated by the engine.
IF Temperature Exceeds >>@ 15 Minutes BCD 45 Minutes In
The Yellow Band, Or Is At Or Above Red Radial:
Accomplish the ENGINE FAILURE / FIRE / SHUTDOWN / SEVERE
DAMAGE / SEPARATION checklist.
* * * *
737
Flight Manual
Continental
ENGINES, APU
Sec. 2.7 Page 19
Rev. 11/15/02 #41
OR
ENGINE LIMIT / SURGE / STALL
Failure of engine or fuel control system components or loss of thrust lever
position feedback has caused loss of engine thrust control. Control loss may not
be immediately evident since many engines fail to some fixed RPM or thrust
lever condition. This fixed RPM or thrust lever condition may be very near the
commanded thrust level and therefore difficult to recognize.
Accomplish Checklist If One Or More Of The Following Conditions Exist:
· Engine RPM or EGT indications are abnormal, approaching or
exceeding limits
· No response to thrust lever movement
· Abnormal engine noises
Autothrottle .......................................................................................OFF
Thrust Lever (Affected Engine) .............................................RETARD
Retard until indications remain within appropriate limits or the thrust
lever is closed.
IF Indications Remain Abnormal Or EGT Continues To Increase:
Accomplish the ENGINE FAILURE / FIRE / SHUTDOWN / SEVERE
DAMAGE / SEPARATION checklist.
* * * *
IF Indications Are Stabilized Or EGT Decreases:
Thrust Lever (Affected Engine).....................................ADVANCE
Advance slowly. Check that RPM and EGT follow thrust lever
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
737 FLIGHT MANUAL 737飞行手册1(50)
