時間：2016-07-09 17:56來源：藍(lán)天飛行翻譯公司 作者：公務(wù)機翻譯 點擊：次
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AFTER TAKE-OFF BEFORE DESCENT VREF for Slats/Krueger - 0?and Flaps - 20?Configuration BEFORE LANDING TAKE-OFF WITH SLATS/KRUEGER RETRACTED PERFORMANCE CORRECTIONS Take-off Speeds; SLATS - 0? Flaps - 20?Dry and Wet Runway Take-off Speeds; Slats - 0? Flaps - 20? Maximum take-off weight as permitted by brake energy requirements Slats - 0o; flaps - 20o; Dry and Wet runway Maximum Take-off Weight As Permitted By Brake Energy Requirements Slats - 0? Flaps - 20? HONEYWELL ENHANCED GROUND PROXIMITY WARNING SYSTEM (EGPWS) Honeywell ENHANCED GROUND PROXIMITY WARNING SYSTEM (EGPWS) MK. V WITH COLLINS PROLINE 4 V6.1 USER SELECTABLE CALLOUTS GENERAL TERRAIN PROXIMITY WARNING Terrain Awareness Display ALERTS AND WARNINGS EGPWS Controls and Indicators ROCKWELL COLLINS FMS-6100 FLIGHT MANAGEMENT SYSTEM Rockwell COLLINS FMS-6100 FLIGHT MANAGEMENT SYSTEM VSPEEDS FUNCTION BRAKE COOLING BRAKE KINETIC ENERGY (BKE) AND BRAKE COOLING GENERAL MAXIMUM BRAKE ENERGY BKE DETERMINATION DURING LANDING OR RTO OPERATIONS FLIGHT PLANNING REDUCED BKE PROCEDURES TAXI BKE BRAKE COOLING FOR QUICK TURN-AROUND AND MULTIPLE BRAKING OPERATIONS BRAKE KINETIC ENERGY (BKE) CONSIDERATIONS DURING TRAINING FLIGHTS AND FLIGHT/GROUND TESTING FUSE PLUG INTEGRITY ZONES USE OF BKE AND COOLING CHART BKE/Cooling chart. Sheet 1 of 2 BKE/Cooling chart. Sheet 2 of 2 Supplement 12 - MAXIMUM TAKE-OFF WEIGHT = 35,650 LB MAXIMUM Take-off WEIGHT = 35,650 LB WEIGHT LIMITATIONS CENTER-OF-GRAVITY LIMITATIONS Center-of-Gravity Envelope CONTAMINATED RUNWAY OPERATIONS Take-off Distance - Flaps - 20?Weight = 35,650 LB; Runway Contaminated by Slush, Standing Water or Loose Snow; Landing Distance Corrections WEIGHT LIMITATIONS Maximum Fuel - Zone 2 Center-of-Gravity Envelope Center Of Gravity Envelope Limits WEIGHT LIMITATIONS Maximum Fuel Loading - Zone 2 Metric Measurements Center-of-Gravity Envelope Center Of Gravity Envelope Limits Metric Measurements TAKE-OFF AND LANDING OPERATIONS AT ULAANBAATAR, MONGOLIA (ZMUB) TAKE-OFF AND LANDING OPERATIONS AT ULAANBAATAR, MONGOLIA (ZMUB) GENERAL TAKE-OFF REQUIREMENTS LANDING REQUIREMENTS Ulaanbaatar Airport (ZMUB) Layout OIS 1- TAKE-OFF CLIMB GRADIENT CORRECTIONS FOR BANK ANGLES TAKE-OFF CLIMB GRADIENT CORRECTIONS FOR BANK ANGLES TAKE-OFF CLIMB GRADIENT CORRECTIONS FOR BANK ANGLES AFFECTED PERFORMANCE CHARTS TAKE-OFF CLIMB GRADIENT CALCULATION EXAMPLE TAKE-OFF 2ND SEGMENT CLIMB GRADIENT CORRECTION FOR STEADY BANKED TURN; FLAPS - 20? TAKE-OFF 2ND SEGMENT CLIMB GRADIENT CORRECTION FOR STEADY BANKED TURN; FLAPS - 12? TAKE-OFF 2ND SEGMENT CLIMB GRADIENT CORRECTION FOR STEADY BANKED TURN; FLAPS - 0? FINAL SEGMENT CLIMB GRADIENT CORRECTION FOR STEADY BANKED TURN; CLEAN CONFIGURATION TAKE-OFF AND LANDING IN CROSSWIND CONDITIONS TAKE-OFF AND LANDING IN CROSSWIND CONDITIONS CROSSWIND TAKE-OFF PROCEDURE CROSSWIND LANDING PROCEDURE Landing Distance Increase for Crosswind Landings Based on Unfactored Dry, Wet, or Contaminated Landing Distances Maximum Roll Angle at Landing USE OF CROSSWIND CHART Contaminated Runway Crosswind Components RUNWAY SURFACE CONTAMINATION (RSC), Canadian Runway Friction Index (CRFI) EQUIVALENT AND ESTIMATED LANDING BRAKING COEFFICIENT Supplments Not Incorporated Into This AFM Performance LIST OF FIGURES GENERAL INFORMATION COMPLIANCE STANDARD PERFORMANCE CONDITIONS VARIABLE FACTORS AFFECTING PERFORMANCE DEFINITIONS GENERAL ATMOSPHERIC AIRSPEEDS UNIT CONVERSIONS |
