判断正误：APU 最关键的转速是在 4%到 30%之间，因为 APU 转速小于4%时，不会产生足够的热量而造成轴承损伤，而转速大于30%时，能够确保有足够的冷却滑油保障轴承的正常润滑。True or False: The critical rotation speed is between 4% and 30% rpm. RPM below 4% does not produce enough heat to cause bearing damage, while RPM above 30% ensures sufficient cooling oil is available to ensure proper bearing lubrication.

精密进近时，机场标高以上（ ） 英尺或距接地点（ ）海里（以先到者为准），应开始建立着陆形态。For precision approach, （ ） ft above airport elevation or（ ） nautical miles away from touch-ground point (whichever comes first)，the Landing configuration should be established.

进近时，襟翼1到位后，PF应设置速度游标为（ ）KIAS。During approach, after Flap 1 in position， the PF should set the speed bug to （ ）KIAS.

在不低于机场标高（ ）英尺必须建立稳定进近。Establish a stable approach at a minimum of（ ） feet above the landing airport elevation.

在不低于机场标高（ ）英尺必须建立着陆形态。 Landing configuration is completed at a minimum of （ ） feet above the landing airport elevation.

NDB进近，在不低于着陆机场标高以上（ ）英尺完成着陆型态，在不低于着陆机场标高以上（ ）英尺建立稳定进近。For NDB approach, complete the Landing configuration at a minimum of （ ） feet above the landing airport elevation; Establish a stable approach at a minimum of （ ）feet above the landing airport elevation.

非精密进近，自动驾驶使用的限制高度为（ ）英尺AGL或DDA，以较高者为准，飞行机组任何时候都必须遵守。For non precision approach, the use of autopilot is limited to a height of （ ） feet AGL or DDA, whichever is higher, and the flight crew must observe this limit at all times.

带有梯级下降点（SDF）的进近，最晚在计算的TOD之前（ ）海里飞机必须建立着陆形态。For approach with step-down descent point (SDF)，as late as（ ）mile prior to the calculated TOD, the airplane must establish a landing configuration

华夏航空公司规定，特定决断高度/高由公布的MDA/H+( )英尺 。Chinaexpress specifies that the designated decision altitude/height (DDA/ H) is increased by ( ) feet from the published MDA/ H.

阵风条件下，五边进近速度设置为（ ） 。In gust conditions, the final approach airspeed should be set to （ ）.

盲降进近高于下滑道时，截获航向道并建立着陆形态后，可以使用不大于（ ）尺/分钟的下降率从上方切入下滑道，场高（ ）尺（AGL）前，必须截获下滑道。如无法满足以上条件，立即执行复飞。When ILS approach is above the glideslope, after capturing localizer and establishing landing configuration, the glideslope can be intercepted from the above by using not more than 1500ft/min descent rate, the glideslope must be captured before （ ）ft AGL. If the above condition cannot be satisfied, go-around must be carried out.