时间：2014-03-26 10:28来源：蓝天飞行翻译 作者：航空 点击：次
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Loss of Tail Tank Fuel Quantity Indication Loss of Total Fuel Quantity Indication Fuel Leak Procedure Hydraulic Power Hydraulic Power System No. 1 Failure System No. 2 Failure System No. 3 Failure System No. 1 High Temperature System No. 2 High Temperature System No. 3 High Temperature Engine-Driven Pump Failure Electric Pump 1B Failure Electric Pump 2B Failure Electric Pump 3A Failure Electric Pump 3B Failure Hydraulic Shut-Off Valve Failure After Engine Shutdown Due to Fire System No. 1 and No. 2 Failure System No. 2 and No. 3 Failure System No. 1 and No. 3 Failure Ice and Rain Protection Ice and Rain Protection Ice Dispersal Procedure Ice Detected One Ice Detector Failed Both Ice Detectors Failed Wing Anti-Ice Sensor Failure Cowl Anti-Ice Failure Wing Leading Edge Temperature and Pressure Low Insufficient Heat for Wing Anti-Icing Probe Heater Failures Windshield Heat Failure Window Heat Failure Windshield Outer Face Ply Failure Instruments System Instruments System Primary Flight Display Failure Display Control Panel Failure EFIS Comparator Failure Multifunction Display Failure Cursor Control Panel Failure PFD Cross-Talk Failure EFIS Parameter Miscompare Air Data Computer Failure Radio Altimeter Failure Inertial Reference System Failure FMS V Speed Failure Landing Gear, Wheel and Brake System Landing Gear, Wheel and Brake System Inboard Anti-Skid Failure Outboard Anti-Skid Failure Anti-Skid (Inboard and Outboard) Failure Inboard/Outboard Brake Pressure Low Parking Brake Shut-Off Valve Failure Main Landing Gear Overheat Detector Failure Nose Wheel Steering System Failure Weight-on-Wheels Input Fault Weight-on-Wheels Output Fault |
