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时间:2010-11-05 10:27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

Minimize reductions from the initial climb pitch attitude until
terrain and obstruction clearance is assured, unless stick shaker
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 monitoring should
be especially aware of vertical 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.
787 Flight Crew Operations Manual
Supplementary Procedures -
Adverse Weather
Boeing Proprietary SP.16.17
Approach and Landing
• Use either Flaps 25 or 30 for landing.
• Establish a stabilized approach no lower than 1000 feet above the
airport to improve windshear recognition capability.
• Use the most suitable runway that avoids the areas of suspected
windshear and is compatible with the 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 glide slope displacement. The pilot monitoring should call out
any deviations from normal. Use of autopilot and autothrottle for
the approach may provide more monitoring and recognition time.
Recovery
Accomplish the WINDSHEAR ESCAPE MANEUVER found in the
Non-Normal Maneuvers section of this manual.
787 Flight Crew Operations Manual
Supplementary Procedures -
Adverse Weather
SP.16.18 Boeing Proprietary
Intentionally
Blank
787 Flight Crew Operations Manual
Performance Dispatch Chapter PD
Table of Contents Section 0
Boeing Proprietary PD.TOC.0.1
P7D7.70 -P2e0rf0orEmRan cTe DRisEpaNtcTh-T8a9b2le Lof BCo FntAenAts
Takeoff . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PD.10.1
Takeoff Field Corrections . . . . . . . . . . . . . . . . . . . . . . . . . . . PD.10.1
Takeoff Field & Climb Limit Weights . . . . . . . . . . . . . . . . . PD.10.2
Takeoff Obstacle Limit Weight . . . . . . . . . . . . . . . . . . . . . . . PD.10.4
Brake Energy Limits VMBE . . . . . . . . . . . . . . . . . . . . . . . . PD.10.6
Takeoff Speeds . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PD.10.7
Enroute . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PD.11.1
Long Range Cruise Maximum Operating Altitude . . . . . . . PD.11.1
Long Range Cruise Trip Fuel and Time . . . . . . . . . . . . . . . . PD.11.3
Long Range Cruise Step Climb . . . . . . . . . . . . . . . . . . . . . . PD.11.5
Short Trip Fuel and Time . . . . . . . . . . . . . . . . . . . . . . . . . . . PD.11.6
Holding Planning . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PD.11.7
Crew Oxygen Requirements . . . . . . . . . . . . . . . . . . . . . . . . . PD.11.7
Net Level Off Weight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PD.11.8
Long Range Cruise Critical Fuel Reserves . . . . . . . . . . . . . . PD.11.9
Landing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PD.12.1
Landing Field Limit Weight - Dry Runway . . . . . . . . . . . . . PD.12.1
Landing Field Limit Weight -Wet Runway . . . . . . . . . . . . . PD.12.2
Landing Climb Limit Weight . . . . . . . . . . . . . . . . . . . . . . . . PD.12.3
Go-Around Climb Gradient . . . . . . . . . . . . . . . . . . . . . . . . . PD.12.4
Quick Turnaround Limit Weight . . . . . . . . . . . . . . . . . . . . . . PD.12.5
Gear Down . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PD.13.1
Takeoff Climb Limit Weight . . . . . . . . . . . . . . . . . . . . . . . . . PD.13.1
Landing Climb Limit Weight . . . . . . . . . . . . . . . . . . . . . . . . PD.13.2
Takeoff Obstacle Limit Weight . . . . . . . . . . . . . . . . . . . . . . . PD.13.3
 
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