時間：2014-03-26 10:28來源：藍(lán)天飛行翻譯 作者：航空 點擊：次
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Fuel Temperature Less than 5°C Fuel Boost Pump Failure Motive Flow Failure Scavenge Ejector Failure Primary Tail Tank Pump Failure (Manual Mode) Secondary Tail Tank Pump Failure (Manual Mode) Tail Tank to Aux Tank Automatic Transfer Failure Tail Tank Transfer is Inhibited Excessive Fuel Load – Aux Tank Excessive Fuel Load – Tail Tank Tail Dump SOV Failed (SOV not in commanded position) Tail Transfer SOV Failed Closed Tail Transfer SOV Failed Open Tail Transfer SOV Failed in Middle Position L/R TO AUX Crossflow Valve Open L/R TO AUX Crossflow Valve Fails to Close Auxiliary Tank Contents Increasing (abnormally) During L/R TO AUX Crossflow Dump Valve Open for More than 5 Minutes Loss of Auxiliary Tank Fuel Quantity Indication Loss of Wing Tank Fuel Quantity Indication 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 |
