Control Arm

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Control Arm is a critical component of an aircraft's flight control system, responsible for transmitting forces from the pilot to the aircraft's flight surfaces. Its primary function is to convert rotational motion into linear motion, enabling precise control over the aircraft's pitch and yaw axes. The control arm is typically made of high-strength materials such as aluminum or carbon fiber, which provide exceptional strength-to-weight ratios and resistance to fatigue. To ensure optimal performance, the control arm must be precisely calibrated and adjusted during regular maintenance checks.