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Static labelled overviewSelected: Rudder
TAIL CONTROLSWING AND HIGH-LIFT DEVICESLANDING GEARFLIGHT DECK
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Read about Rudder

Guided journey

Core airflow: intake to exhaust

Follow the working fluid through the generic two-spool turbofan before tracing the shafts that return turbine work to the compressors and fan.

Step 1 of 8Intake

The intake presents the incoming air to the fan.

Trace the system

What connects to this part?

Select a turbofan flow-path or spool component to show its reviewed upstream and downstream links.

Identify the part

Find it in the model

Test spatial recall with the four reviewed low-pressure-system concepts.

Compare mode

See the difference

Compare where each high-lift device sits and how it changes the wing.

CompareTrailing-edge flapLeading-edge slat
LocationInboard trailing edgeWing leading edge
Primary effectIncreases camber and often areaOpens a slot that delays separation
Exam distinctionAdds substantial lift and dragHelps sustain attached flow at high angle of attack

Reviewed FAA source (2026-09-09)

Rudder

The rudder is a primary flight-control surface that controls yaw about the aircraft’s vertical axis.

Where it is
Hinged to the vertical stabilizer at the tail of the generic transport-aircraft model.
What it does
Its deflection creates a side force at the tail and changes the aircraft’s yawing moment.
Relationship
The rudder pedals command the yaw-control system; coordinated flight also depends on aileron input and the aircraft’s roll response.
Common confusion
The rudder controls yaw directly, not roll. Bank angle is controlled primarily by ailerons and, on some aircraft, roll spoilers.

Check yourself

Without looking back, can you explain where the rudder is, what it does, and which component drives it or is driven by it?

Scope: Generic transport-aircraft teaching model. Reviewed 2026-09-09.

Related concepts

Sources

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