A、 更换有摩擦的导热垫。
B、 更换有磨损的隔热毯。
C、 更换有晃动的绝缘板。
答案:B
A、 更换有摩擦的导热垫。
B、 更换有磨损的隔热毯。
C、 更换有晃动的绝缘板。
答案:B
A. 为了达到在整个行业内以合理统一的形式向飞行员提供与特定飞机操作相关的所需、有用或可取信息之目的,手册起草者应在实际可行的范围内遵循本规范。
B. 为了在整个行业内给飞行员提供要求的,有用的或想要的关于某架飞机的信息,建议手册的起草者在实际编写中遵守此规范。
C. 为了实现这样的目的,即在整个行业内给飞行员提供要求的,有用的或想要的某架飞机的信息, 必须采用统一的形式,手册的编写者要结合实际情况遵守此规范。
A. Wire the cable to the structure.
B. Secure the cable to the structure.
C. Attach the cable to the structure with wire.
A. Do the troubleshooting procedure to find the cause of the malfunction
B. Do the troubleshooting procedure to look the result of the malfunction
C. Find the cause of the malfunction to do the troubleshooting procedure
A. 如果在测试过程中,流量指示器没有达到预定位置,则使用此备用程序
B. 如果在测试结束后,流量指示器没有达到设定位置,则使用此附加程序
C. 如果在测试结束后,流量指示器没有达到设定位置,则使用此备用程序
A. 在安装V型卡箍前先润滑。
B. 在安装V型卡箍前先涂润滑脂。
C. 在安装V型卡箍前先清洁润滑脂。
A. Set the suitable L PACK switch or the R PACK switch to the AUTO position. L PACK switch and the R PACK switch are on the p5-10 air conditioning panel.
B. Set L PACK Switch or R PACK Switch on Suitable p5-10 air conditioner panel to AUTO position.
C. Set the applicable L PACK switch or the R PACK switch to the AUTO position. The R PACK switch is on the p5-10 air conditioning panel.
A. The oil level on the sight gauge must be visible during the test;
B. The oil quantity on the sight gauge must be visible during the test;
C. The oil level on the sight indicator must be visible during the test;
A. If an engine overheat/fire detector can not operate, the engine and APU fire alarm unit alternatively changes to single loop operation. In the single loop module, only one loop must check the engine and APU fire detection module for an overheat or fire condition to give the alarm condition.
B. If an engine overheat/fire detector fails to operate, the engine and APU fire detection module automatically changes to single loop operation. In the single loop mode, only one loop must detect an overheat or fire condition for the engine and APU fire detection module to give the alarm condition.
C. If an engine overheat/fire detector is inoperative, the engine and APU fire detection module automatically changes to single loop operation. In the single loop mode, only one loop must detect an overheat or fire condition by the engine and APU fire detection module for the alarm condition.
A. Servo tab is connected on the trailing edge of primary flight control surface, moving in the opposite direction to that of primary control surface.
B. Servo tab is a small movable tab built into the trailing edge of an aircraft primary control surface, which is actuated by the cockpit control,moving in the same direction as that of the primary surface moving.
C. Servo tab is a small movable tab built into the trailing edge of an aircraft primary control surface. It moves as the primary flight control surface’s moving and not controlled by the cockpit.
A. This section provides procedures to calculate weight and moments for different phases of a scheduled flight and to make sure that the center of thrust is beyond approved limits.
B. The paragraph gives the weight and moments for calculating all kinds of phases of a planned fight and procedures for ensuring that center of gravity is within authorized limits.
C. This paragraph describes the procedures to calculate weight and moment for various phases of a planned flight and to ensure that the center of gravity is within approved limits.