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2 Limitations
CHAPTER 10 FLIGHT PLAN AND OTHERS
TOW MTOW
LDW MLDW
LWA MLWA
ZFW MZFW
TF RTF
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飛機(jī)性能工程
Airplane Performance Engineering
中國(guó)民用航空學(xué)院空中交通管理學(xué)院航務(wù)運(yùn)行管理工程系
Department of Flight Operation,Air Traffic Management College, CAUC
§1 FLIGHT PLAN
3 Re-dispatch Procedure
This procedure permits aircraft to carry less
contingency fuel than in the standard case. This is
interesting in case of fuel capacity, or takeoff limitations.
Operators select a point called the decision point
along the planned route.At this point, the pilot has two
possibilities:
Reach a suitable proximate diversion airport,
taking into account the maximum landing weight
limitation.
Continue the flight to the destination airport, when
the remaining fuel is sufficient.
CHAPTER 10 FLIGHT PLAN AND OTHERS
飛機(jī)性能工程
Airplane Performance Engineering
中國(guó)民用航空學(xué)院空中交通管理學(xué)院航務(wù)運(yùn)行管理工程系
Department of Flight Operation,Air Traffic Management College, CAUC
§1 FLIGHT PLAN
3 Re-dispatch Procedure
This procedure is interesting for flag and
supplemental operations, for which contingency fuel
depends on flight time.
CHAPTER 10 FLIGHT PLAN AND OTHERS
飛機(jī)性能工程
Airplane Performance Engineering
中國(guó)民用航空學(xué)院空中交通管理學(xué)院航務(wù)運(yùn)行管理工程系
Department of Flight Operation,Air Traffic Management College, CAUC
§1 FLIGHT PLAN
3 Re-dispatch Procedure
CHAPTER 10 FLIGHT PLAN AND OTHERS
飛機(jī)性能工程
Airplane Performance Engineering
中國(guó)民用航空學(xué)院空中交通管理學(xué)院航務(wù)運(yùn)行管理工程系
Department of Flight Operation,Air Traffic Management College, CAUC
§1 FLIGHT PLAN
3 Re-dispatch Procedure
Using this procedure, the fuel required is the
greatest of:
CHAPTER 10 FLIGHT PLAN AND OTHERS
飛機(jī)性能工程
Airplane Performance Engineering
中國(guó)民用航空學(xué)院空中交通管理學(xué)院航務(wù)運(yùn)行管理工程系
Department of Flight Operation,Air Traffic Management College, CAUC
§1 FLIGHT PLAN
4 ETOPS
CHAPTER 10 FLIGHT PLAN AND OTHERS
飛機(jī)性能工程
Airplane Performance Engineering
中國(guó)民用航空學(xué)院空中交通管理學(xué)院航務(wù)運(yùn)行管理工程系
Department of Flight Operation,Air Traffic Management College, CAUC
§2 AIRPLANE PERFORMANCE MONITORS
and OTHERS
1 Airplane performance monitors
CHAPTER 10 FLIGHT PLAN AND OTHERS
飛機(jī)性能工程
Airplane Performance Engineering
中國(guó)民用航空學(xué)院空中交通管理學(xué)院航務(wù)運(yùn)行管理工程系
Department of Flight Operation,Air Traffic Management College, CAUC
§2 AIRPLANE PERFORMANCE MONITORS
and OTHERS
2 EOSID
CHAPTER 10 FLIGHT PLAN AND OTHERS
飛機(jī)性能工程
Airplane Performance Engineering
中國(guó)民用航空學(xué)院空中交通管理學(xué)院航務(wù)運(yùn)行管理工程系
Department of Flight Operation,Air Traffic Management College, CAUC
§2 AIRPLANE PERFORMANCE MONITORS
and OTHERS
3 Oxygen
CHAPTER 10 FLIGHT PLAN AND OTHERS
飛機(jī)性能工程
Airplane Performance Engineering
中國(guó)民用航空學(xué)院空中交通管理學(xué)院航務(wù)運(yùn)行管理工程系
Department of Flight Operation,Air Traffic Management College, CAUC
§2 AIRPLANE PERFORMANCE MONITORS
and OTHERS
4 noise restrictions
CHAPTER 10 FLIGHT PLAN AND OTHERS
飛機(jī)性能工程
Airplane Performance Engineering
中國(guó)民用航空學(xué)院空中交通管理學(xué)院航務(wù)運(yùn)行管理工程系
Department of Flight Operation,Air Traffic Management College, CAUC
THANK YOU！
中國(guó)民航大學(xué)空管學(xué)院航務(wù)系
飛機(jī)性能Aircraft Performance
航路爬升：是指從飛機(jī)起飛飛行航跡結(jié)束點(diǎn)(通常取高
于離機(jī)場(chǎng)1500英尺高度的點(diǎn))到達(dá)規(guī)定的巡航高度和速
度為止的爬升過(guò)程；
推力：最大爬升推力；
目的：經(jīng)濟(jì)、安全；
重點(diǎn)：時(shí)間、油量、距離；
概述
中國(guó)民航大學(xué)空管學(xué)院航務(wù)系
飛機(jī)性能Aircraft Performance
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中國(guó)民航大學(xué)空管學(xué)院航務(wù)系
飛機(jī)性能Aircraft Performance
爬升參數(shù)的計(jì)算
爬升梯度（Climb Gradient)
. ( ) /(1 d )
d
N D
L
C G F C V V
W C g h
  
/ ( ) /(1 d )
d
N D
L
r c F C V V V
W C g h
  
剩余推力、剩余功率、加速因子
爬升率（Rate of Climb)
中國(guó)民航大學(xué)空管學(xué)院航務(wù)系
飛機(jī)性能Aircraft Performance
爬升參數(shù)的計(jì)算
影響因素分析
飛行速度
飛行高度
環(huán)境溫度
飛機(jī)重量
加速因子
風(fēng)速風(fēng)向
中國(guó)民航大學(xué)空管學(xué)院航務(wù)系
飛機(jī)性能Aircraft Performance
　
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