时间：2013-10-07 13:20来源：蓝天飞行翻译 作者：航空 点击：次
|
POUNDS - KILOGRAMS CONVERSION INCHES - MILLIMETRES CONVERSION STALL SPEEDS - POWER IDLE CABIN ALTITUDE FOR VARIOUS AIRPLANE ALTITUDES MINIMUM TAKE-OFF POWER AT 1900 RPM WIND COMPONENTS MAXIMUM TAKE-OFF WEIGHT TO ACHIEVE POSITIVE ONE ENGINE INOPERATIVE CLIMB AT LIFT-OFF - FLAPS UP TAKE-OFF DISTANCE - FLAPS UP ACCELERATE-STOP DISTANCE - FLAPS UP ACCELERATE-GO DISTANCE - FLAPS UP TAKE-OFF CLIMB GRADIENT - ONE ENGINE INOPERATIVE - FLAPS UP MAXIMUM TAKE-OFF WEIGHT - FLAPS APPROACH TAKE-OFF DISTANCE - FLAPS APPROACH ACCELERATE-STOP DISTANCE - FLAPS APPROACH ACCELERATE-GO DISTANCE - FLAPS APPROACH TAKE-OFF CLIMB GRADIENT - ONE ENGINE INOPERATIVE - FLAPS APPROACH CLIMB - TWO ENGINE - FLAPS UP CLIMB - TWO ENGINE - FLAPS APPROACH CLIMB - ONE ENGINE INOPERATIVE SERVICE CEILING - ONE ENGINE INOPERATIVE TIME, FUEL, AND DISTANCE TO CRUISE CLIMB TABLES: MAXIMUM CRUISE POWER AT 1900 RPM - ISA -30 |
