时间：2017-09-27 08:31来源：蓝天飞行翻译公司 作者：民航翻译 点击：次
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MAXIMUM ALLOWABLE EPR REDUCTION FOR REDUCED THRUST EXAMPLE PROBLEMS Problem Solving Procedures Procedure GENERAL TAKEOFF ANALYSIS TAKEOFF ANALYSIS WITH IMPROVED CLIMB PERFORMANCE OBSTACLE LIMITED TAKEOFF WEIGHT ANALYSIS DISTANT OBSTACLE LIMITED TAKEOFF WEIGHT ANALYSIS OBSTACLE LIMITED TAKEOFF WEIGHT WITH OBSTACLE IN FINAL SEGMENT TAKEOFF FLIGHT PATH EXAMPLE 5 OBSTACLE LIMITED TAKEOFF WEIGHT ANALYSIS WITH IMPROVED CLIMB PERFORMANCE VMC LIMITED TAKEOFF BRAKE ENERGY LIMITED TAKEOFF WEIGHT ANALYSIS CHART INTERPOLATION ALL ENGINES OPERATING CORRECTED RUNWAY LENGTH (FLAPS 1, 5, 15, & 20) ENGINE INOPERATIVE CORRECTED TAKEOFF DISTANCE (FLAPS 1, 5, 15, S 20) CORRECTED ACCELERATE-STOP DISTANCE (FLAPS 1, 5, 15, & 20) RUNWAY LENGTH & Vl ADJUSTMENTS (FLAPS 5 & 15) FIELD LENGTH LIMITS (FLAPS 5) - A/C PACKS ON (FLAPS 15) - A/C PACKS ON TAKEOFF CLIMB LIMITS (FLAPS 5) - A/C PACKS ON TAKEOFF CLIMB LIMITS (FLAPS 15) - A/C PACKS ON TIRE SPEED LIMITS (225 MPH TIRES) TAKEOFF SPEEDS (FLAPS 5) TAKEOFF SPEEDS (FLAPS 15) BRAKE ENERGY LIMITS (FLAPS 5 & 15) MINIMUM V1 FOR CONTROL ON THE GROUND (V]/MCG) ) TAKEOFF CLIMB (IMPROVED CLIMB PERFORMANCE) IMPROVED CLIMB PERFORMANCE (FLAPS 5, 15, & 20) TAKEOFF CLIMB (FLAPS 15) - A/C PACKS ON CLOSE-IN OBSTACLE CLEARANCE (FLAP 5 & 15) DISTANT OBSTACLE CLEARANCE (FLAPS 5&15) OBSTACLE DISTANCE TRADE LINES MAXIMUM LEVEL-OFF HEIGHT (FLAPS 15) THIRD SEGMENT DISTANCE (FLAPS 15) FINAL TAKEOFF CLIMB (FLAPS UP) - A/C PACKS ON GRADIENT CORRECTIONS (TAKEOFF/FINAL TAKEOFF CLIMB) GRADIENT CORRECTIONS (TAKEOFF/FINAL TAKEOFF CLIMB) MINIMUM V1 FOR CONTROL ON THE GROUND AIR MINIMUM CONTROL SPEED ALTERNATE THRUST SETTING METHOD (% N1 RPM) (RB211-535E4 ENGINES) CERTIFICATE LIMITATIONS General EMERGENCY PROCEDURES OPERATING PROCEDURES PERFORMANCE Performance Adjustements Use of Weight Decrements Takeoff Weight Determination Procedure TAKEOFF WEIGHT DETERMINATION PROCEDURE Weight Decrements Takeoff Speeds Brake Energy ENGINE DATA Thrust Setting TAKEOFF N1 POWER SETTING GO-AROUND N1 POWER SETTING INFLIGHT N1 POWER SETTING (MAX CONTINUOUS) CONFIGURATION DEVIATION LIST (CDL) MODEL 757-200/-300 SERIES GENERAL LIMITATIONS 21 AIR CONDITIONING Cabin Pressure Safety Relief Valve Flapper Door 23 COMMUNICATIONS Interphone Access Door - Wing-to-Body Fairing Static Discharger - Trailing and Tip Type 27 FLIGHT CONTROLS Rudder-to-Body Edge Seal Inboard Trailing Edge Flap Seal Plate (Elephant Ear) Flap Track Fairing Flap Track Fairing Seals 28 FUEL |
