• 热门标签

当前位置: 主页 > 航空资料 > 飞行资料 >

时间:2011-03-14 13:13来源:蓝天飞行翻译 作者:admin
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

activates


.  
Crew coordination and awareness are very important. Develop an awareness of normal values of airspeed, attitude, vertical speed, and airspeed build–up. Closely monitor vertical flight path instruments such as vertical speed and altimeters. The pilot not flying should be especially aware of vertical flight path instruments and call out any deviations from normal

.  
Should airspeed fall below the trim airspeed, unusual control
column forces may be required to maintain the desired pitch
attitude. Stick shaker must be respected at all times


.  
If windshear should be encountered near VR, and airspeed suddenly decreases, there may not be sufficient runway left to accelerate back to the normal VR. If there is insufficient runway left to stop, initiate a normal rotation at least 2000 feet before the end of the runway even if airspeed is low. Higher than normal attitudes may be required to lift–off in the remaining runway


Approach and Landing
.  
Use flaps 30 for landing

.  
Establish a stabilized approach no lower than 1000 feet above the airport to improve windshear recognition capability


Supplementary Procedures -Adverse Weather 737 Operations Manual

.  
Use the most suitable runway that avoids the areas of suspected
windshear and is compatible with crosswind or tailwind
limitations. Use ILS G/S, VNAV path or VASI/PAPI indications to
detect flight path deviations and help with timely detection of
windshear


.  
If the autothrottle is disengaged, or is planned to be disengaged
prior to landing, add an appropriate airspeed correction (correction
applied in the same manner as gust), up to a maximum of 20 knots


.  
Avoid large thrust reductions or trim changes in response to sudden
airspeed increases as these may be followed by airspeed decreases


.  
Crosscheck flight director commands using vertical flight path
instruments


.  
Crew coordination and awareness are very important, particularly
at night or in marginal weather conditions. Closely monitor the
vertical flight path instruments such as vertical speed, altimeters,
and glideslope displacement. The pilot not flying should call out
any deviations from normal. Use of the autopilot and autothrottle
for the approach may provide more monitoring and recognition
time

 

Recovery
Accomplish the Windshear Maneuver found in Non–Normal Maneuvers section of this manual.
Copyright . The Boeing Company. See title page for details.
SP.16.16   June 4, 2004

737 Operations Manual

Dimensions  . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .  1.10.1
Principal Dimensions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .  1.10.1 Turning Radius . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .  1.10.2
Instrument Panels . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .  1.20.1
Panel Arrangement . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .  1.20.1 Aft Flight Deck Overview . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .  1.20.2 Captain’s Instrument Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . .  1.20.5 First Officer’s Instrument Panel . . . . . . . . . . . . . . . . . . . . . . . . . .  1.20.6 Center Instrument Panel and Lightshield (Non–EIS Airplanes) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .  1.20.7 Center Instrument Panel and Light Shield (EIS Airplanes) . . . . .  1.20.8 Forward Overhead Panel  . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .  1.20.9 Aft Overhead Panel  . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .  1.20.11 Forward Electronic Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.20.12 Aft Electronic Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.20.13 Control Stand . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.20.19 Auxiliary Panels . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.20.20 Attendant Panels  . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.20.21 Controls and Indicators . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .  1.30.1
Flight Deck Lighting  . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .  1.30.1 Map Light Controls  . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .  1.30.1 Panel and Background Lighting . . . . . . . . . . . . . . . . . . . . . . .  1.30.1 AFDS Flood Light Control . . . . . . . . . . . . . . . . . . . . . . . . . . .  1.30.2 Flood and Aft Electronic Panel Lights Controls . . . . . . . . . .  1.30.2 Overhead/Circuit Breaker Panel Light Controls  . . . . . . . . . .  1.30.3 Dome Light Control  . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .  1.30.3 Master Lights Test and Dim Switch . . . . . . . . . . . . . . . . . . . .  1.30.4
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:737-300机组操作手册Flight Crew Operations Manual FCOM 1(78)