时间:2015-01-22 10:41来源:蓝天飞行翻译公司 作者:公务机翻译 点击:次
ALTITUDES HUMIDITY WIND ICE PROTECTION RUNWAY CONDITION PERCENTAGE OF STALL SPEED ADDITIONAL LANDING DISTANCES PERFORMANCE CONDITIONS CONFIGURATIONS MAXIMUM ALLOWABLE WEIGHTS BASIS FOR DATA; BLEED AIR CONDITIONS BASIS FOR DATA BLEED AIR CONDITIONS USE OF CHARTS - CORRECTIONS USE OF CHARTS; GRADIENT LOSS IN TURN (%) USE OF CHARTS GRADIENT LOSS IN TURN (%) WIND CORRECTED CLIMB GRADIENT CONVERSION CHARTS WIND COMPONENTS TAT / SAT TEMPERATURE CONVERSION TEMPERATURE CONVERSION CHART °F / °C WEIGHT CONVERSION CHART KG / LB PRESSURE CONVERSION CHART IN. HG / MBAR-HPA HEIGHT-PRESSURE ALTITUDE CONVERSION CHART PITOT-STATIC SYSTEM CALIBRATION ADS 1, 2, 3 AND 4 - GROUND RUN - ALL WHEELS ON GROUND ADS 1, 2, 3 AND 4 - GEAR UP AND GEAR DOWN ADS 1, 2, 3 AND 4 - RAT DEPLOYED STALLING SPEEDS AND BUFFETING REFERENCE STALL SPEEDS BUFFET ONSET ENVELOPE ENGINE POWER SETTING - WITHOUT ICE PROTECTION TAKE-OFF N1, TAKE-OFF RUN AND FIRST SEGMENT CLIMB MAXIMUM CONTINUOUS N1, ONE ENGINE INOPERATIVE, FINAL TAKE-OFF AND EN-ROUTE CLIMBS MAXIMUM CONTINUOUS N1, TWO ENGINES INOPERATIVE, FINAL TAKE-OFF AND EN-ROUTE CLIMBS ENGINE POWER SETTING - WITH ICE PROTECTION TAKE-OFF N1, TAKE-OFF RUN AND FIRST SEGMENT CLIMB MAXIMUM CONTINUOUS N1, ONE ENGINE INOPERATIVE, FINAL TAKE-OFF AND EN-ROUTE CLIMBS MAXIMUM CONTINUOUS N1, TWO ENGINES INOPERATIVE, FINAL TAKE-OFF AND EN-ROUTE CLIMBS TAKE-OFF SF2 EXAMPLE - DRY RUNWAY BALANCED FIELD LENGTH - DRY RUNWAY DECISION SPEED ASSOCIATED WITH BALANCED FIELD LENGTH - DRY RUNWAY MAXIMUM BRAKE ENERGY SPEED (VMBE) - DRY RUNWAY EXAMPLE - WET RUNWAY BALANCED FIELD LENGTH - WET RUNWAY DECISION SPEED ASSOCIATED WITH BALANCED FIELD LENGTH - WET RUNWAY MAXIMUM BRAKE ENERGY SPEED (VMBE) - WET RUNWAY |