時(shí)間：2017-11-06 16:55來源：藍(lán)天飛行翻譯公司 作者：民航翻譯 點(diǎn)擊：次
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To view this page ensure that Adobe Flash Player version 9.0.124 or greater is installed. 7.2.2. MINIMUM CONTROL SPEEDS WITH DERATED THRUST
7.2.3. DERATED TAKEOFF AND RUNWAY STATE
7.2.4. DERATED TAKEOFF PROCEDURE
D. EN ROUTE LIMITATIONS
1. EN ROUTE FAILURE CASES
2. ENGINE FAILURE(S)
2.1. GENERAL DEFINITIONS
2.1.1. DRIFT DOWN PROCEDURE
2.1.2. GROSS AND NET DRIFT DOWN FLIGHT PATHS
2.1.3. TAKEOFF ALTERNATE AIRPORT
2.2. EN ROUTE OBSTACLE CLEARANCE – ONE ENGINE INOPERATIVE
2.2.1. LATERAL CLEARANCE
2.2.2. VERTICAL CLEARANCE
2.2.3. DIVERSION AIRFIELD
2.3. TWIN ENGINE AIRCRAFT
2.3.1. 60 MINUTE RULE
2.4. FOUR ENGINE AIRCRAFT
2.4.1. 90 MINUTE RULE
2.4.2. OBSTACLE CLEARANCE – TWO ENGINES INOPERATIVE
2.4.3. DIVERSION AIRFIELD – TWO ENGINES INOPERATIVE
3. IN-FLIGHT CABIN PRESSURIZATION FAILURE
3.1.1. OXYGEN SYSTEMS
3.1.2. PASSENGER OXYGEN REQUIREMENT
3.1.3. FLIGHT PROFILE
3.1.4. MINIMUM FLIGHT ALTITUDES
3.1.5. OBSTACLE CLEARANCE – CABIN PRESSURIZATION FAILURE
4. ROUTE STUDY
TABLE OF CONTENTS Getting to Grips with Aircraft Performance
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E. LANDING
1. INTRODUCTION
2. LANDING DISTANCE AVAILABLE (LDA)
2.1. WITH NO OBSTACLE UNDER LANDING PATH
2.2. WITH OBSTACLES UNDER LANDING PATH
3. LANDING PERFORMANCE
3.1. OPERATING LANDING SPEEDS
3.1.1. LOWEST SELECTABLE SPEED: VLS
3.1.2. FINAL APPROACH SPEED: VAPP
3.1.3. REFERENCE SPEED: VREF
3.2. ACTUAL LANDING DISTANCE (ALD)
3.2.1. MANUAL LANDING
3.2.2. AUTOMATIC LANDING
3.3. GO-AROUND PERFORMANCE REQUIREMENTS
3.3.1. APPROACH CLIMB
3.3.2. LANDING CLIMB
3.4. EXTERNAL PARAMETERS INFLUENCE
3.4.1. PRESSURE ALTITUDE
3.4.2. TEMPERATURE
3.4.3. RUNWAY SLOPE
3.4.4. RUNWAY CONDITIONS
3.4.5. AIRCRAFT CONFIGURATION
4. DISPATCH REQUIREMENTS
4.1. REQUIRED LANDING DISTANCE (RLD)
4.1.1. RLD DRY RUNWAYS
4.1.2. RLD WET RUNWAYS
4.1.3. RLD CONTAMINATED RUNWAYS
4.1.4. RLD WITH AUTOMATIC LANDING (DRY)
4.2. GO-AROUND REQUIREMENTS
4.2.1. NORMAL APPROACH
4.2.2. CAT II OR CAT III APPROACH
4.3. CONCLUSION
5. IN-FLIGHT REQUIREMENTS
5.1. IN-FLIGHT FAILURE
5.2. OVERWEIGHT LANDING REQUIREMENTS
5.3. FUEL JETTISONING CONDITIONS
F. CRUISE
1. GENERAL
1.1. INTRODUCTION
1.2. SPECIFIC RANGE
2. SPEED OPTIMIZATION
2.1. ALL ENGINE OPERATING CRUISE SPEEDS
2.1.1. MAXIMUM RANGE MACH NUMBER (MMR)
2.1.2. LONG-RANGE CRUISE MACH NUMBER (MLRC)
2.1.3. ECONOMIC MACH NUMBER (MECON)
2.1.4. CONSTANT MACH NUMBER
Getting to Grips with Aircraft Performance TABLE OF CONTENTS
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3. ALTITUDE OPTIMIZATION
3.1. OPTIMUM CRUISE ALTITUDE
3.1.1. AT A CONSTANT MACH NUMBER
3.1.2. WIND INFLUENCE
3.2. MAXIMUM CRUISE ALTITUDE
3.2.1. LIMIT MACH NUMBER AT CONSTANT ALTITUDE
3.2.2. MAXIMUM CRUISE ALTITUDE
3.3. EN ROUTE MANEUVER LIMITS
3.3.1. LIFT RANGE
3.3.2. OPERATING MANEUVER LIMITATIONS
3.4. CRUISE OPTIMIZATION: STEP CLIMB
4. FCOM CRUISE TABLE
G. CLIMB
1. FLIGHT MECHANICS
1.1. DEFINITIONS
1.2. CLIMB EQUATIONS
1.2.1. CLIMB GRADIENT (γ)
1.2.2. RATE OF CLIMB (RC)
1.2.3. SPEED POLAR
1.3. INFLUENCING PARAMETERS
1.3.1. ALTITUDE EFFECT
1.3.2. TEMPERATURE EFFECT
1.3.3. WEIGHT EFFECT
1.3.4. WIND EFFECT
2. CLIMB IN OPERATION
2.1. CLIMB MANAGEMENT
2.1.1. THRUST SETTING
2.1.2. ENERGY SHARING
2.1.3. CLIMB CEILING
2.2. CLIMB SPEEDS
2.2.1. CLIMB AT GIVEN IAS/MACH LAW
2.2.2. CLIMB AT MAXIMUM GRADIENT
2.2.3. CLIMB AT MAXIMUM RATE
2.2.4. CLIMB AT MINIMUM COST
2.3. FCOM CLIMB TABLE
2.4. CABIN CLIMB
H. DESCENT / HOLDING
1. FLIGHT MECHANICS
1.1. DEFINITIONS
1.2. DESCENT EQUATIONS
1.2.1. DESCENT GRADIENT (γ)
1.2.2. RATE OF DESCENT (RD)
1.2.3. SPEED POLAR
1.3. INFLUENCING PARAMETERS
1.3.1. ALTITUDE EFFECT
1.3.2. TEMPERATURE EFFECT
1.3.3. WEIGHT EFFECT
1.3.4. WIND EFFECT
TABLE OF CONTENTS Getting to Grips with Aircraft Performance
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2. DESCENT IN OPERATION
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