相关题目
失去2号或3号液压系统使飞机仍有（ ）％对称刹车能力，并对工作刹车进行全面防滞控制。Loss of the No. 2 or No. 3 Hydraulic system leaves the airplane with（ ）% symmetric braking capability with full Anti-skid control to the working brakes.
在执行绕机检查时，刹车磨损指示器应在什么情况下进行检查? During External Walkaround, the brake wear indicator pins shall be checked provided that:
前起落架舱门是：Nose gear doors are:
万一出现擦机尾，给机组的指示是：In case of tail strike, indications for the crew will be:
主起落架保持在收上位依靠：The main landing gear are held up by:
哪个液压系统给内侧和外侧刹车提供动力？which hydraulic system(s) powers the inboard and outboard brakes?
防滞控制系统提供：The anti-skid control system provides:
刹车温度监控指示显示在：Brake temperature monitoring indications are presented:
转弯手柄可使前轮转向（ ）度和方向舵脚蹬可使前轮转向（ ）度。The steering tiller turns the nosewheel（ ）degree and the rudder pedals turn the nosewheel（ ）degree.
对于CRJ 900飞机，当人工释放起落架，前起落架上位锁人工释放作动筒释放依靠：On the CRJ900 aircraft, when the landing gear has been released manually, the nose landing gear uplock manual release actuator is released:
