時(shí)間：2016-07-09 17:56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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WHEEL BRAKE FIRE COCKPIT OR CABIN FIRE/SMOKE ELECTRICAL FIRE/SMOKE ELECTRICAL FIRE/SMOKE IN COCKPIT OR CABIN Cockpit Overhead Circuit Breaker Panel (Partial) Bus Load Distribution SMOKE / FUME REMOVAL APU TAIL PIPE FIRE ON GROUND EMERGENCIES DURING TAKE-OFF TAKE-OFF ABORT ENGINE FAILURE DURING TAKE-OFF ABOVE V1 ENGINE FAILURE DURING COUPLED APPROACH ELECTRICAL FAILURES FAILURE OF BOTH GENERATORS EMERGENCY BUS FAILURE ENGINE OIL PRESSURE LOW ENGINE OIL TEMPERATURE HIGH BLEED AIR LEAK BLEED AIR FAILURE MODES BLEED LINE OVERPRESSURE /OVERTEMPERATURE DUCT TEMPERATURE HIGH RAPID DECOMPRESSION CABIN UNDERPRESSURIZATION EMERGENCY DESCENT JAMMED RUDDER JAMMED ELEVATOR JAMMED AILERON FAILURE OF BOTH ENGINES EMERGENCY LANDING (Both Engines Inoperative) PASSENGER EVACUATION DITCHING PREPARATIONS APPROACH BEFORE TOUCHING WATER AFTER DITCHING EMERGENCY EXIT LOSS OF ALL CABIN PRESSURE INDICATIONS AND CONTROL Abnormal Procedures LIST OF FIGURES EICAS CAUTION, ADVISORY AND STATUS MESSAGES EICAS Display - Primary Page CAUTION MESSAGES ADVISORY MESSAGES STATUS MESSAGES FADEC FAILURES FADEC FAULTY MESSAGE HOT START - GROUND ENGINE FAILURE/FLAMEOUT DURING FLIGHT ENGINE SLOW RESPONSE ENGINE SHUTDOWN IN FLIGHT AIR STARTS Air Start Envelope (Windmilling and Starter-Assist) WINDMILLING AIR START (IF AUTO IGNITION IS UNSUCCESSFUL) STARTER-ASSIST AIR START AFTER COMPLETE SHUT- DOWN SINGLE-ENGINE OPERATIONS SINGLE-ENGINE LANDING SINGLE-ENGINE GO-AROUND ELECTRICAL SYSTEM FAILURES BATTERY OVERHEAT BATTERY DISCONNECTED FAILURE OF ONE GENERATOR APU GENERATOR FAILURE EMERGENCY BUS ALTERNATE FEED UNCOMMANDED STARTER GENERATOR ENGAGEMENT APU SHUT-DOWN FAILURE MAIN BATTERY DISCHARGE EMERGENCY BATTERY DISCONNECTED EMERGENCY BATTERY OVERHEAT EMERGENCY BATTERY DISCHARGE GENERATOR OVER LOAD APU GENERATOR OVER LOAD ENGINE/NACELLE ANTI-ICE SYSTEM FAILURE ENVIRONMENTAL CONTROL SYSTEM FAILURES CABIN OVERPRESSURIZATION UNPRESSURIZED DISPATCH AND FLIGHT AIR DATA COMPUTER FAILURES BOTH ADC 1 & 2 INOPERATIVE DE-ICING SYSTEM FAILURE FLIGHT CONTROL SYSTEM FAILURES ELEVATOR CONTROL FAILURES AILERON CONTROL FAILURE HORIZONTAL STABILIZER TRIM FAILURE INADVERTENT GROUND / FLIGHT AIR BRAKES DEPLOYMENT IN FLIGHT SLATS/FLAPS FAIL TO MOVE JAMMED HORIZONTAL STABILIZER SLATS, KRUEGER OR FLAPS FAILURES FUEL SYSTEM ABNORMAL FUEL TANK TRANSFER FUEL JETTISON WING FUEL UNBALANCE FUEL BOOST JET PUMP FAILURE FUEL PRESSURE LOW FUEL LEVEL LOW FQMC FAILURE ABNORMAL FUEL TANK TEMPERATURE FUEL FILTER CLOGGED OIL SYSTEM FAILURES ENGINE CHIP DETECTOR OIL FILTER CLOGGED ENGINE VIBRATION THRUST REVERSER FAILURE THRUST REVERSER READY LIGHT IN FLIGHT MAIN HYDRAULIC SYSTEM FAILURES FAILURE OF ONE HYDRAULIC PUMP FAILURE OF COMPLETE MAIN HYDRAULIC SYSTEMS HYDRAULIC SYSTEM OVER HEAT LANDING GEAR SYSTEM FAILURES EMERGENCY LANDING GEAR EXTENSION LANDING GEAR DOES NOT LOCK UP LANDING GEAR DOES NOT LOCK DOWN LANDING GEAR FAILURE TO RETRACT LANDING WITH ABNORMAL LANDING GEAR CONDITIONS PREPARATION FOR LANDING WITH ABNORMAL GEAR CONDITION LANDING WITH NOSE GEAR UNSAFE OR RETRACTED, BOTH MAIN GEAR DOWN & LOCKED LANDING WITH NOSE AND ONE MAIN LANDING GEAR DOWN AND LOCKED, OPPOSITE MAIN GEAR UNSAFE OR RETRACTED |
