|
大翼加油面板 wing fueling panelAPU 燃油活门 fuel valve for the APU加油浮子电门 refuel float switch燃油泵低压灯 fuel pump LOW PRESSURE light燃油温度指示器 fuel temperature indicator加油面板燃油量指示器fuel quantity indicator on refuel panel显示 ARINC 错误信息shows ARINC error message增压泵跳开关拔出 boost pump circuit breaker open电门在测试油量表位时，显示不正确。Display is not correct with switch at TEST GAGES飞机接通地面电源时加油面板灯不亮。Refueling panel light light does not come on with ground power on the airplaneN1，N2，EGT 及燃油流量指示读数低或波动。N1, N2, EGT, and FF indications read low or fluctuate更换燃油滤滤筒 Replace fuel filter cartridge驾驶舱燃油量指示 Fuel quantity indication in flight compartment1) 波动，太高或太低。Fluctuates or is too high or too low3) 操作测试燃油量指示系统. Do the operational test of fuel quantity indicating system.燃油交输活门开灯 fuel crossfeed VALVE OPEN light1) 活门在过渡过程时，不亮。Does not come on when the valve is in transit2) 交输选择器移至关断位时，保持明亮。Stays on bright when the crossfeed selector is moved to the off position 3) 交输选择器移至接通位时，保持明亮。Stays on bright when the crossfeed selector is moved to the on position1) 所选活门打开且加油总管增压时，灯不亮。Light does not come on with valves selected open and refueling manifold pressurized2) 按压“按压测试”电门后，灯不灭。Light does not go off after pressing the press-to-test switch3) 所选活门打开且加油总管增压时，加油活门位置指示器灯不亮。Refuel valve position indicator light does not come on with valves selected open and refueling manifold pressurized4) 电门在关闭位时，保持亮。Stays on with switch at CLOSED1) 禁止进行所有的加油。All refueling is prevented 2) 通气集油箱燃油溢出。Fuel spill at surge tank 3) 电门在关闭位时活门不关闭。Valve does not close with switch at CLOSED流量控制活门 flow control valve压力控制活门 pressure control valve液压过热警告电门 hydraulic overheat warning switch刹车压力指示 brake press indicator1) 从液压油箱通气管道流出。Comes out of the reservoir vent line2) 从液压油箱通气管道排放口流出。Comes out of the reservoir vent line drain mast 4) 从 A 系统传输到 B 系统。Transfers from system A to system B5) 航后检查A系统回油滤组件内丢失一弹簧。 Do AF check and find one spring of A system return filter ASSY lost.6) 航后检查发现右发吊架上部有一根液压系统回油管接头漏油,检查为管接头破裂.. A fitting of the hydraulic system’s return line in the R/H is found leaking in AF check. The fitting has a crack after inspection.7) 勤务液压油箱 Serve hydraulic reservoirs8) 液压储压器的勤务 Serve hydraulic accumulator9) 航后检查发现B系统液压管路t型接头漏油.The T-type union of the hydraulic system B leaked oil during AF check.10) 更换液压地面加油滤 Replace hydraulic ground service filter11) 封严更换 Replace the seal12) 更换正释压活门滤滤芯 Replace SAF checkout relief valve filter elements13) 更换A系统液压系统回油滤 Replace system a hydraulic return filter液压油量指示 Hydraulic fluid quantity indication1) 在“大使用量”系统操作后不恢复原有量。 Does not return to the same level after operation of a 'heavy use' system3) 驾驶舱显示和液压油箱表读数不同。Flight compartment display and hydraulic reservoir gauge do not read the same4) 驾驶舱显示变化不稳定或在读数间跳跃。Flight compartment display moves erratically or jumps between readings 5) 液压油箱有液压油时驾驶舱显示器指示为零。Flight compartment display shows zero, but reservoir has hydraulic fluid6) 显示加注液压油（6%）。Shows RF (6%)7) 瞬时低于/高于……。Momentarily below/above……1) 航前发现左发EDP处有漏滑油迹象。 There is oil leakage around left engine EDP PF inspection.2) 航后检查发现右发EDP本体漏油.The EDP of the R/H engine leaks oil in AF check.3) 拆除并安装A系统EMDP Remove and install system A EMDP4) 更换液压PTU滤子 Replace hydraulic PTU filter5) 更换左发EDP Replace the L/H engine EDP6) 更换正释压活门滤子 Replace the positive pressure relief valve filers7) 更换发动机驱动泵管路滤芯 Replace the EDP line filter element总温传感器 total temperature sensor翼身过热灯 wing-body overheat light整流罩防冰灯 cowl anti-ice light热防冰活门 thermal anti-ice valve风挡传感器电门 windshield sensor switch防冰自动油门电门 anti-ice auto-throttle switch左/右侧窗户温度热控制组件 L / R side window heat control unit舱内湿度大，起雾或结冰。high humidity, fog, or ice in cabin机翼防冰左活门打开灯 wing anti-ice L valve open light1) 电门移至接通位时，从明亮到暗亮慢。 Slow to go from bright to dim when switch is moved to ON1) AF 检查发现左风挡雨刷胶皮破损。Do AF Check and find the L rain wiper is broken.2) 右侧雨刷不工作.The R/H rain wiper does not work.
|
