时间：2015-01-20 10:34来源：蓝天飞行翻译公司 作者：公务机翻译 点击：次
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Section B: Smoke From Air Conditioning Outlets (possiblebleed air source) Section C: Electrical Fire / Smoke Source Unknown Right Aft Radio Rack Hot Flight Controls / Autoflight Index Flight Controls Electronic Architecture Lateral Control System Schematic Rudder Control System Schematic Elevator Control System Schematic Stall Recovery Jammed Elevator Jammed Roll Control Jammed Horizontal Stabilizer FCECU 1 Failure FCECU 2 Failure Abnormal Flaps Configuration Landing Rudder Failure Rudder Pedal Command Failure Stabilizer Trim Runaway Q-Feel Failure Stall Protection System Failure Autopilot Failure Yaw Damper Failure Fuel / Hydraulics Index Fuel System Schematic Diagram FQMS System Interface Hydraulic System Block Diagram Fuel Leak Fuel Pressure Low Fuel Standby Pump Inoperative Standby Pump ON Fuel Tank Temperature Low Fuel Imbalance Fuel Interconnect Valve Failure Fuel Jettison Jettison Valve Failure Jettison Auto Stop Inoperative Fuel Measurement Degraded Fuel Transfer Fault Hydraulic System / Component Availability per Failure Right Hydraulic System Failure Left Hydraulic System Failure Dual Hydraulic System Failure Hydraulic Reservoir Hot / Hydraulic Pressure High Instruments / Avionics Index Radio Interface Unit (RIU) Failures Tuning Inoperative Message On CDU Tune Page and/or DU Tune Window Inability To Tune COM / NAV Radios or UnexpectedTuning Behavior Check Standby Multifunction Controller (SMC) -Airdata Angle of Attack (AOA) Miscompare Unreliable Airspeed Indications Dual Air Data Computer (ADC) Failure Integrated Processor Cabinet (IPC) 1 or 2 or Both Failures Integrated Processor Cabinet (IPC) 3 Failure Probe Heat Failure Data Concentration Unit (DCU) Failure |
