時(shí)間：2014-12-02 10:10來源：藍(lán)天飛行翻譯公司 作者：公務(wù)機(jī)翻譯 點(diǎn)擊：次
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OXYGEN SYSTEM ENGINE INSTRUMENTS AND CREW ALERTING SYSTEM (EICAS) OMS GENERAL EICAS RANGE MARKINGS COLORS POWERPLANT EICAS INDICATIONS FUEL EICAS INDICATIONS FUEL TANK TEMPERATURE INDICATIONS APU EICAS INDICATIONS APU RPM CAS MESSAGES AUXILIARY POWER UNIT (APU) APU OPERATION APU GENERATOR LOAD LIMITS MAXIMUM PERMISSIBLE EGT MAXIMUM ROTOR SPEED POWERPLANT ENGINE GROUND START ENGINE GROUND OPERATIONS ENGINE IN FLIGHT OPERATIONS ENGINE FUEL AND CONTROL SYSTEMS ENGINE FUEL TEMPERATURE PRIMARY ACCEPTABLE FUEL TYPES OTHER ACCEPTABLE TYPE FUELS ANTI-STATIC ADDITIVES EGME-BASED FUEL ICING INHIBITORS DiEGME-BASED FUEL ICING INHIBITORS RUSSIAN (CIS) FUEL SYSTEM ICING INHIBITORS FUNGICIDE/BIOCIDE INHIBITORS ANTI-CORROSION ADDITIVES ENGINE EXHAUST THRUST REVERSERS ENGINE OIL OIL INLET TEMPERATURE APPROVED OILS OIL PRESSURE Engine Oil Pressure ENGINE STARTING STARTER DUTY Section II - Emergency Procedures LIST OF FIGURES EICAS WARNING MESSAGES COLLECTOR CAS MESSAGE SA (SITUATIONAL AWARENESS) CAS MESSAGE GENERAL GUIDANCE WARNING MESSAGES (RED) ATA 21 - AIR CONDITION AND PRESSURIZATION RAPID DECOMPRESSION CABIN UNDERPRESSURIZATION Oxygen Duration; 123.4 CU FT Oxygen Pressure Versus Temperature EMERGENCY DESCENT BLEED AIR LEAK DUAL FAILURE SINGLE FAILURE CABIN OVER PRESSURIZATION ATA 22 - AUTO FLIGHT AUTOMATIC DESCENT MODE (ADM) ATA 26 - FIRE PROTECTION ENGINE FIRE ON GROUND ENGINE FIRE IN FLIGHT APU FIRE AIRCRAFT INTERIOR FIRE / SMOKE / FUMES SECTION A: FIRE / SMOKE / FUMES IN COCKPIT, CABIN, OR BAGGAGE COMPARTMENT SECTION B: SMOKE FROM AIR CONDITIONING OUTLETS (POSSIBLE BLEED AIR SOURCE) SECTION C: ELECTRICAL FIRE / SMOKE SOURCE UNKNOWN RIGHT AFT RADIO RACK HOT ATA 27 - FLIGHT CONTROLS Stall Recovery ATA 28 - FUEL FUEL LEAK A. FUEL LEAKAGE IS VISIBLE OR SUSPECTED FROM WING / FUSELAGE B. FUEL LEAKAGE IS NOT VISIBLE AND ONE OF THE FOLLOWING IS SUSPECTED FUEL PRESSURE LOW ATA 32 - LANDING BLOWN TIRE DURING TAKEOFF ATA 72-80 - ENGINE TAKEOFF ABORT ENGINE FAILURE DURING TAKEOFF ABOVE V1 SINGLE ENGINE FAILURE IN FLIGHT ENGINE EXCEEDANCE ENGINE SHUTDOWN IN FLIGHT ENGINE RESTART IN FLIGHT Engine Start Envelope A. STARTER-ASSIST AIR-START (CROSS-BLEED) B. WINDMILLING AIR-START C. APU-ASSIST AIR-START (BELOW 15,000 FT) D. AFTER START SINGLE-ENGINE APPROACH AND LANDING SINGLE ENGINE GO-AROUND DUAL ENGINE FAILURE DUAL ENGINE FAILURE EMERGENCY LANDING ENGINE OIL PRESSURE LOW THRUST REVERSER UNLOCKED OR DEPLOYED DURING TAKEOFF |
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