時(shí)間：2012-05-18 08:48來源：藍(lán)天飛行翻譯 作者：航空 點(diǎn)擊：次
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AC Power Schematic Electrical Power Controls and Monitoring Generator Drive AC Voltmeter and Frequency Meter DC Voltmeter and Ammeter Electrical Power Controls and Monitoring Schematic DC Power System Transformer Rectifier Units Battery Power Battery Charger DC Power Receptacle DC Power System Schematic Standby Power System Normal Operation Alternate Operation Static Inverter Standby Power System Schematic All Generators Inoperative Airplane General, Emergency Equipment, Doors and Windows Air Systems Engines, APU Communications Electrical Flight Instruments Fire Protection Fuel Hydraulics Landing Gear Navigation Warnings Basic Equipment Operating – Instrument Panels Captain Instrument Panel First Officer Instrument Panel Electrical System Power Distribution No. 1 Generator Inoperative No. 2 Generator Inoperative 7-Engines, APU Table Of Contents 10 Controls and Indicatorsd Engine Instrument System (EIS) Primary Panel Reverser Unlocked, Autothrottle Limit, and Thrust Mode Display N1 Indications N1 Manual Set Knob EGT Indications N2 Indications Fuel Flow/Fuel Used Indications Engine Instrument System (EIS) Secondary Panel Caution Lights Total Air Temperature Indication Engine Oil Indications Engine Vibration Indications Hydraulic System Pressure and Quantity Indications Engine Start Switches Engine Panel Engine Controls APU APU Hours Indicator 20 Engine System Description |
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