时间：2012-07-24 15:22来源：蓝天飞行翻译 作者：航空 点击：次
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05-14-10: Fuel Boost Pump Failure 05-14-20: Failure of Two Boost Pumps on One Side 05-14-30: Low Fuel State 05-14-40: Fuel Return Fail 05-14-50: Fuel Leak In Flight HYDRAULIC SYSTEM 05-15-10: Dual Hydraulic System (L SYS and R SYS) Failure 05-15-20: Left Hydraulic System (L SYS) Failure - Loss of Pressure and / or Fluid 05-15-30: Left Hydraulic System (L SYS) Failure - Loss of Pressure and Fluid 05-15-40: Left Hydraulic System (L SYS) Failure - Loss of Pressure Only 05-15-50: Right Hydraulic System (R SYS) Failure - Loss of Pressure and / or Fluid 05-15-60: Landing With The Standby Electrical Power System (HMG) On With Both Hydraulic Systems Operating 05-15-70: Landing With The Standby Electrical Power System (HMG) Operating On Single Hydraulic System INDICATING / RECORDING SYSTEM 05-16-10: Primary Flight Display (PFD) Malfunction 05-16-20: Display Unit (DU) Failure 05-16-30: Operation With An Air Data System (ADS) Failed 05-16-40: Traffic and Collision Avoidance System (TCAS) Failure 05-16-50: Enhanced Ground Proximity Warning System (EGPWS) Failure 05-16-60: Blocked Total Air Temperature (TAT) Probe 05-16-70: Modular Avionics Unit (MAU) Failure 05-16-80: MAU 1A Failure 05-16-90: MAU 1B Failure 05-16-100: MAU 2A Failure 05-16-110: MAU 2B Failure 05-16-120: MAU 3A Failure 05-16-130: MAU 3B Failure 05-16-140: Enhanced Vision System (EVS) Malfunctions 05-16-150: Head-Up Display (HUD) Malfunctions 05-16-160: Equipment Loss While In RVSM Airspace 05-16-170: Radio Failure / Mistune During A Dual Coupled ILS Approach |
