时间：2011-08-11 18:26来源：蓝天飞行翻译 作者：航空 点击：次
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飞机电源正常工作时电动马达驱动泵供电中断。Electrical power of the electric motor-driven pump was interrupted during electrical power system operated normally MEC.拆装MEC（main engine control） Remove and install MEC燃油控制盒的拆装 Remove and install MEC fuel control box. 调节启动控制推拉钢索 Adjust the start control push-pull cable 推力手柄 Thrust lever 1) 复飞第二次按压 TO/GA 电门时，推力手柄不能 达到全功率 N1 位。Thrust lever can not go to full rated N1 position when TO/GA switch was pressed a second time during go-around 2) 复飞第一次按压 TO/GA 电门时，推力手柄不能 达到减推力 N1 位。Thrust lever did not go to reduced N1 position when TO/GA switch was pressed one time during go-around 3) 在收油门方式，推力手柄不能与自动油门一同收回。Thrust lever did not move back synchronously with autothrottle in RETARD mode 4) 在RETARD（收回）方式下推力手柄不回收。 Thrust lever did not move back in RETARD mode 5) 按压 TO/GA 电门后推力手柄不向前移。Thrust lever did not move forward when TO/GA switch was pressed. 6) 按压 TO/GA 电门时，推力手柄不能前移。 Thrust lever did not move forward when TO/GA switch was pressed. 7) 双发 N1 相同时手柄不一致。 Levers staggered (did not align) at the same N1 of both engines 8) 手柄不一致在自动油门接通时。Levers staggered with autothrottle engaged. 9) 推力方式在发动机显示上不显示。Thrust mode did not display on the engine display. 自动油门 Autothrottle 1) 接地后不自动断开。Autothrottle did not disengaged automatically after touchdown 2) 推力手柄不一致时不断开。Autothrottle did not disengage automatically when thrust levers split 3) 在N1方式不能保持N1极限值。Autothrottle did not keep N1 limit in N1 mode 4) 在速度方式不能保持调定的速度。Autothrottle did not keep set speed in SPEED mode 5) 发动机N1速度波动，发动机N1速度在自动油门关断时正常。Engine N1 speed fluctuated, it was normal with autothrottle OFF 6) 按压方式电门时方式不改变。Autothrottle mode did not change when mode switch was pressed. 7) 按压断开电门时不能断开。Autothrottle can not be disengaged when switch was pressed. 8) A/T 琥珀色警告信号牌灯闪亮。A/T amber warning annunciator light flashed 9) 自动油门不能预位，预位灯不亮，飞行方式信号牌上不显示 ARM（预位）。Autothrottle can not be armed, ARM light was not on, ARM didn’t display on the flight mode annunciator 马赫空速表上选择目标速度游标问题 Selected target speed bug problem on the mach airspeed indicator 1) 状态方式不自动改变。Status mode did not change automatically. 2) 在自测交互式范围检查过程中油门解算器角度角度空白。Throttle resolver angle indication was blank during BITE interactive range check. EEC自测 EEC BITE 1) CDU 上显示自测不工作。BITE INOP showed on the CDU 2) CDU 上显示A/B 通道 EEC 数据不可用。CH A/B EEC DATA NOT AVAILABLE showed on the CDU. 3) 飞机在地面，CDU 上显示发动机维护不能进行—发动机的飞行指 示 器 显 示 飞 行。“ENGINE MAINTENANCE CAN NOT BE ACCESSED—THE ENGINE'S FLIGHT INDICATOR SHOWS FLIGHT” showed on the CDU, airplane was on the ground 4) 维护信息不能消除。Maintenance message can’t be erased 5) EAU（发动机辅助装置）自检程序8期间所有灯不亮。All lights did’t come on during the BITE procedure 8. ATA77 发动机指示 发动机指示 engine indicating EGT 指示 EGT indication 发动机失效信息 ENG FAIL message 发动机活门关闭灯 ENG VALVE CLOSED light 1) 当起动手柄移至切断位/慢车位时，XX灯由明亮至暗亮的变化慢。XX light changed slowly from bright to dim when start lever moved to CUTOFF/ IDLE position. |
