时间:2013-05-27 15:51来源:蓝天飞行翻译 作者:航空 点击:次
ENGINE EEC FAIL TRANSMISSION SYSTEM FAILURES MAIN GEARBOX OIL PRESSURE LOW OIL TEMPERATURE HIGH MAIN ROTOR CONTROLS BINDING TAIL ROTOR SYSTEM FAILURES YAW CONTROL DIAGNOSTICS TAIL ROTOR DRIVE FAILURE TAIL ROTOR CONTROL SYSTEM FAILURE TAIL ROTOR CONTROL BINDING ELECTRICAL SYSTEM DOUBLE DC GENERATOR FAILURE EXTENDED FLIGHT ENDURANCE AFTER DOUBLE DC GENERATOR FAILURE SERVICES AVAILABLE ON ESSENTIAL BUS 1 AND 2 SERVICES LOST DURING BUS FAILURES MAIN AND AUXILIARY BATTERY HOT LANDING GEAR LANDING GEAR FAILS TO LOCK DOWN LIGHTNING STRIKE STATIC PORT OBSTRUCTION EMERGENCY EXITS MALFUNCTION PROCEDURES CAUTION SYSTEM CAUTIONS WITH VOICE MESSAGES TABLE OF CAS CAUTION MESSAGES TABLE OF PFD AND MFD MESSAGES ENGINE MALFUNCTIONS COMPRESSOR STALL UNUSUAL ENGINE NOISE ENGINE LIMIT EXCEEDANCE ENGINE OIL TEMPERATURE |