방향타 (Rudder) (Rudder)

What Is a Rudder?

The rudder is a hinged, movable flight control surface attached to the trailing edge of the vertical stabilizer — the upright fin that forms the central part of the empennage. Deflecting the rudder left or right changes the aerodynamic forces on the vertical tail, yawing the aircraft's nose in the corresponding direction. Unlike in a ship or a car, the rudder in an aircraft is rarely used alone to turn; rather, it coordinates with the ailerons to produce balanced, slip-free turns.

Function and Purpose

The rudder serves several critical flight functions. During coordinated turns, a small amount of rudder is applied in the direction of bank to cancel adverse yaw — the tendency of the aircraft's nose to swing opposite to the intended turn as one aileron rises and the other descends. In crosswind landings, pilots use sustained rudder input to align the aircraft's heading with the runway centerline while the aircraft drifts sideways with the wind, then apply opposite rudder just before touchdown to straighten the aircraft ("de-crab" technique). During an engine failure on a multi-engine aircraft, the rudder is the primary tool for counteracting the asymmetric thrust that would otherwise yaw the aircraft uncontrollably toward the failed engine.

Rudder authority is a critical certification requirement: the rudder must be powerful enough to maintain directional control at the minimum control speed on the ground (VMCG) and in the air (VMCA) even with the critical engine failed at maximum thrust.

Types and Variations

• Single-panel rudder: One hinged surface occupying the full height of the vertical fin trailing edge. Standard on most narrow-body jets (Boeing 737, Airbus A320).
• Multi-panel rudder: Large wide-body aircraft (Boeing 747, 777) use upper and lower rudder panels that can be driven independently or in combination, providing redundancy and finer control authority.
• Active side-slip control: Some advanced aircraft use rudder inputs computed by flight control computers to damp Dutch roll oscillations automatically — a function performed by the yaw damper system.

Notable Examples

The Airbus A380 rudder is split into upper and lower sections, each with its own hydraulic actuators, ensuring no single hydraulic failure can eliminate directional control. The Boeing 777 rudder system uses three independent hydraulic systems to power its large rudder, reflecting the criticality of directional control on a twin-engine wide-body. Following the American Airlines Flight 587 accident (2001), in which the rudder broke from the empennage due to excessive pedal reversals, rudder travel limiters became standard on all Airbus fly-by-wire aircraft above certain airspeeds.

Related Components

The rudder is structurally integrated with the vertical stabilizer of the empennage and works alongside flaps and ailerons during approach and landing. Rudder inputs are monitored and — on fly-by-wire aircraft — filtered and limited by flight control computers accessible from the cockpit. The yaw damper system automatically applies small, rapid rudder deflections to suppress the oscillatory Dutch roll mode inherent in swept-wing aircraft designs.