时间：2013-10-07 13:20来源：蓝天飞行翻译 作者：航空 点击：次
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TABLES: ONE ENGINE INOPERATIVE MAXIMUM CRUISE POWER AT 1900 RPM - ISA -30?233 ONE ENGINE INOPERATIVE MAXIMUM CRUISE POWER AT 1900 RPM - ISA -20?234 ONE ENGINE INOPERATIVE MAXIMUM CRUISE POWER AT 1900 RPM - ISA -10?235 ONE ENGINE INOPERATIVE MAXIMUM CRUISE POWER AT 1900 RPM - ISA ONE ENGINE INOPERATIVE MAXIMUM CRUISE POWER AT 1900 RPM - ISA +10?237 ONE ENGINE INOPERATIVE MAXIMUM CRUISE POWER AT 1900 RPM - ISA +20?238 ONE ENGINE INOPERATIVE MAXIMUM CRUISE POWER AT 1900 RPM - ISA +30?239 ONE ENGINE INOPERATIVE MAXIMUM CRUISE POWER AT 1900 RPM - ISA +33?240 GRAPHS: PRESSURIZATION CONTROLLER SETTING FOR LANDING HOLDING TIME TIME, FUEL, AND DISTANCE TO DESCEND CLIMB - BALKED LANDING LANDING DISTANCE WITHOUT PROPELLER REVERSING LANDING DISTANCE WITHOUT PROPELLER REVERSING - FLAPS UP LANDING DISTANCE WITH PROPELLER REVERSING 90-590024-217_Section6 SECTION 6 - WEIGHT AND BALANCE/EQUIPMENT LIST (ENGLISH UNITS) |
