時(shí)間：2016-07-09 17:56來(lái)源：藍(lán)天飛行翻譯公司 作者：公務(wù)機(jī)翻譯 點(diǎn)擊：次
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AIRSPEED CALIBRATION TAKE-OFF DISTANCES GRADIENT OF CLIMB HEIGHT ICING UNFACTORED LANDING DISTANCE PERFORMANCE CONFIGURATIONS DEMONSTRATED CROSSWIND NOISE LEVELS Measured Noises PERFORMANCE ENGINE PERFORMANCE TAKE-OFF PERFORMANCE MAXIMUM ALLOWABLE TAKE-OFF WEIGHT TAKE-OFF ANALYSIS TAKE-OFF PROCEDURES TAKE-OFF PATH (ONE ENGINE INOPERATIVE) CLIMB PERFORMANCE TAKE-OFF CLIMB GRADIENTS (One Inoperative) ENROUTE CLIMB GRADIENTS (Net Flight Path; One Inoperative) APPROACH CLIMB GRADIENTS (One Inoperative) LANDING CLIMB GRADIENTS (Both s Operative) LANDING PERFORMANCE MAXIMUM ALLOWABLE LANDING WEIGHT UNFACTORED LANDING DISTANCE LANDING DISTANCE CORRECTIONS LANDING REFERENCE SPEED ICING SUMMARY OF CORRECTION FACTORS Static Take-off Thrust - N1 Setting; Anti-ice - Off Static Take-off Thrust - N1 Setting; Anti-ice - On Maximum Climb Thrust - N1 Setting; Final Segment; Anti-ice - Off Maximum Climb Thrust - N1 Setting; Final Segment; Anti-ice - On Enroute Climb Thrust - N1 Setting; Anti-ice - Off Enroute Climb Thrust - N1 Setting; Anti-ice - On Balked Landing / Approach Climb - N1 Setting; Anti-ice - Off Balked Landing / Approach Climb - N1 Setting; Anti-ice - On Airspeed Position Correction Take-off, Approach and Landing Configuration Altimeter Residual Error Take-off, Approach and Landing Configuration Airspeed Position Error, Altimeter and Machmeter Residual Error Wind Components Approved Altitude/Temperature Envelope Minimum Control Speed - Ground (VMCG) Flaps - 0? 12?and 20? Minimum Control Speed - Air (VMCA) Flaps - 0? 12?and 20? Reference Stall Speeds Horizontal Stabilizer Trim Setting for Take-off Buffet Boundary; Clean Configuration Take-off Weight Limitations (As Permitted by 2nd Segment Climb Requirements) Flaps - 20? Anti-ice - Off V1 Correction; Flaps - 0? Wet Runway Take-off Distance Corrections; Flaps 0? Wet Runway Maximum Take-off Weight (As Permitted By Brake Energy Requirements) Flaps - 12? Dry Runway Maximum Take-off Weight (As Permitted By Brake Energy Requirements) Flaps - 12? Wet Runway Maximum Take-off Weight (As Permitted By Brake Energy Requirements) Flaps - 0? Dry Runway Maximum Take-off Weight (As Permitted By Brake Energy Requirements) Flaps - 0? Wet Runway Take-off Paths Profiles (One Engine Inoperative) Close-in Obstacle Clearance for Basic Climb Profile Required Average Gross Climb Gradient Distant Obstacle Clearance for Basic Climb Profile Required Average Gross Climb Gradient Distant Obstacle Clearance for Extended 2ND Segment Profile Required Average Gross Climb Gradient Clearance Margin Vs. Horizontal Distance Conversion of Geometric Altitude to Pressure Altitude Increment Take-off Climb Gradients; 2nd Segment; Flaps - 20? Net Take-off Flight Path; 3rd Segment - Acceleration; Flaps - 20? Take-off Climb Gradients; 2nd Segment; Flaps - 12? Net Take-off Flight Path; 3rd Segment - Acceleration; Flaps - 12? Take-off Climb Gradients; 2nd Segment; Flaps - 0? Net Take-off Flight Path; 3rd Segment - Acceleration; Flaps - 0? Take-off Climb Gradients; Final Segment; Clean Configuration Flaps Retraction and Enroute Climb Speed Enroute Climb Gradients; Clean Configuration Approach and Landing Approach Climb Gradients; Flaps - 20? Gear - Up Approach Climb Speed; Flaps - 20? Landing Climb Gradients; Flaps - 40? Gear - Down Landing Weight Limitations (As Permitted by Approach Climb Requirements); Anti-ice - Off Landing Weight Limitations (As Permitted by Approach Climb Requirements; Anti-ice - On Landing Weight Limitations (As Permitted By Quick Turnaround Requirements) |
