当飞机在飞行过程中，如果出现内部APU故障，APU将会：if an internal APU fault occurs, while the aircraft is in flight, the APU will:

应在( ) 海里前将反推收至慢车。 Reverser idle thrust should be achieved before ( ) knots.

前轮接地后应尽早使用( )。Use ( ) as soon as possible after nose wheel on the ground.

如果着陆的速度大于VREF，可能会导致（ ）先接地。When touchdown speed is greater than VREF, ( ) may touch down first as a result.

着陆技术（收油门的技术）会受到以下哪些因素影响? The landing technique (power reduction) is influenced by a number of variables including（）。

坡度超过（ ）度会导致翼尖擦地。Bank angles in excess of （） will result in a wingtip strike.

俯仰角度超过 ( )度会导致机尾擦地。Pitch angles in excess of （）will result in a tail strike.

不要过早地使用手轮来控制方向，原则上，待速度减到（ ）海里以下或正常滑行速度后再使用前轮转弯手柄脱离跑道，严禁利用余 速大速度脱离跑道。Don’t use tiller to control direction too early; principally, use the tiller to vacate from runway until speed reduced below（）knots or at normal taxi speed, it’s forbidden to vacate from runway with remaining high speed.

如果在发动机关车后，ITT 超过 （ ）℃并急速上升，应立即冷转发动机以降低 ITT。If ITT rises over （）℃ and is increasing rapidly following engine-shutdown, carry out a dry motoring immediately to reduce ITT.

低于（ ）N2稳定转速的滑行时间，可以作为 2 分钟的冷却时间。Taxi at a stable speed with （）N2 or below, this process can be counted as 2 minutes cooling time.

如需在跑道里 180°转弯掉头，地速不得大于（ ）节, 严禁利用余速转弯掉头，正常情况下应沿线滑行，如在跑道中段掉头或管制员有特殊要求时，应给转弯半径留出足够的余地，防止偏出跑道。If 180° turn need to be complete on runway, the ground speed cannot be more than （） knots, it’s forbidden to use remaining speed for normal and U turn. Under normal condition, taxi along the line. If making a U turn at intermediate runway or there is special requirement from controller, sufficient margin shall be left for the radius of turn in order to avoid runway excursion.