時間：2011-08-11 18:26來源：藍天飛行翻譯 作者：航空 點擊：次
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飛機電源正常工作時電動馬達驅動泵供電中斷。Electrical power of the electric motor-driven pump was interrupted during electrical power system operated normally MEC.拆裝MEC（main engine control） Remove and install MEC燃油控制盒的拆裝 Remove and install MEC fuel control box. 調節啟動控制推拉鋼索 Adjust the start control push-pull cable 推力手柄 Thrust lever 1) 復飛第二次按壓 TO/GA 電門時，推力手柄不能 達到全功率 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) 復飛第一次按壓 TO/GA 電門時，推力手柄不能 達到減推力 N1 位。Thrust lever did not go to reduced N1 position when TO/GA switch was pressed one time during go-around 3) 在收油門方式，推力手柄不能與自動油門一同收回。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) 按壓 TO/GA 電門后推力手柄不向前移。Thrust lever did not move forward when TO/GA switch was pressed. 6) 按壓 TO/GA 電門時，推力手柄不能前移。 Thrust lever did not move forward when TO/GA switch was pressed. 7) 雙發 N1 相同時手柄不一致。 Levers staggered (did not align) at the same N1 of both engines 8) 手柄不一致在自動油門接通時。Levers staggered with autothrottle engaged. 9) 推力方式在發動機顯示上不顯示。Thrust mode did not display on the engine display. 自動油門 Autothrottle 1) 接地后不自動斷開。Autothrottle did not disengaged automatically after touchdown 2) 推力手柄不一致時不斷開。Autothrottle did not disengage automatically when thrust levers split 3) 在N1方式不能保持N1極限值。Autothrottle did not keep N1 limit in N1 mode 4) 在速度方式不能保持調定的速度。Autothrottle did not keep set speed in SPEED mode 5) 發動機N1速度波動，發動機N1速度在自動油門關斷時正常。Engine N1 speed fluctuated, it was normal with autothrottle OFF 6) 按壓方式電門時方式不改變。Autothrottle mode did not change when mode switch was pressed. 7) 按壓斷開電門時不能斷開。Autothrottle can not be disengaged when switch was pressed. 8) A/T 琥珀色警告信號牌燈閃亮。A/T amber warning annunciator light flashed 9) 自動油門不能預位，預位燈不亮，飛行方式信號牌上不顯示 ARM（預位）。Autothrottle can not be armed, ARM light was not on, ARM didn’t display on the flight mode annunciator 馬赫空速表上選擇目標速度游標問題 Selected target speed bug problem on the mach airspeed indicator 1) 狀態方式不自動改變。Status mode did not change automatically. 2) 在自測交互式范圍檢查過程中油門解算器角度角度空白。Throttle resolver angle indication was blank during BITE interactive range check. EEC自測 EEC BITE 1) CDU 上顯示自測不工作。BITE INOP showed on the CDU 2) CDU 上顯示A/B 通道 EEC 數據不可用。CH A/B EEC DATA NOT AVAILABLE showed on the CDU. 3) 飛機在地面，CDU 上顯示發動機維護不能進行—發動機的飛行指 示 器 顯 示 飛 行。“ENGINE MAINTENANCE CAN NOT BE ACCESSED—THE ENGINE'S FLIGHT INDICATOR SHOWS FLIGHT” showed on the CDU, airplane was on the ground 4) 維護信息不能消除。Maintenance message can’t be erased 5) EAU（發動機輔助裝置）自檢程序8期間所有燈不亮。All lights did’t come on during the BITE procedure 8. ATA77 發動機指示 發動機指示 engine indicating EGT 指示 EGT indication 發動機失效信息 ENG FAIL message 發動機活門關閉燈 ENG VALVE CLOSED light 1) 當起動手柄移至切斷位/慢車位時，XX燈由明亮至暗亮的變化慢。XX light changed slowly from bright to dim when start lever moved to CUTOFF/ IDLE position. |
