相关题目
判断正误True or False：当飞机防滞功能受限或没有防滞功能时，将会严重影响飞机的刹车性能。Aircraft braking performance is severely affected when operating the aircraft with limited or no anti-skid protection.
飞行状态下满足以下哪些条件时，刹车温度信息将会从状态页移除：1.BTMS指示正常2.襟翼收上3.起落架收上并锁定。During flight, the brake temperature information is removed from the status page if conditions of the following is met: 1. BTMS indications are normal. 2. The flaps are up. 3. Landing gear is up and locked.
（多选题）着陆形态警告系统监控以下哪些参数？ （multiple choices）Which parameters of the following are monitored by Landing Configuration Warning System?
内侧和外侧刹车压力显示在液压简图页上。绿色指示：The inboard and outboard brake pressure are displayed on HYD synoptic page. Green indicates:
判断正误True or False：当起落架警告喇叭响，按压主警告电门/灯也可以消除音频警告。When the Landing gear warning horn ring, pushing the MASTER WARNING switch/light can silence the aural warning.
判断正误True or False：当刹车过热情况不再存在时，通过按压BTMS OVHTWARN RESET（刹车温度监控系统过热警告复位）电门可使系统复位。A BTMS OVHT WARN RESET switch is used to reset the system when the brake overheat condition no longer exists.
如果一个刹车温度传感器失效，则相应的读数将显示为（ ）的虚线。If a brake temperature sensor fails, the respective readout will turn to ( ) dashes.
前轮转弯操作由( )号液压系统提供。 Nosewheel steering is powered by hydraulic system ( ).
起落架位置、机轮承重（WOW）指示、反推位置和机身舱门位置的信息是由（ ）控制。The information of landing gear position, WOW indication, thrust reverser position and fuselage door position is controlled by ( ) .
刹车温度数值指示相应的刹车温度值。白色数值代表：Brake temperature readout indicates temperature value of respective brake. White readout represents:
