Aviation & Real-World Flying 8 min read 241 views

How does autothrottle work in an airliner?

Ian Stephens
In short

Learn what an airliner autothrottle does, how Airbus autothrust differs from Boeing autothrottle, and why selected speed may not be held.

An airliner’s autothrottle automatically manages engine thrust to hold a commanded speed or Mach number, or to maintain a calculated thrust setting, depending on the active flight mode. It uses air-data, engine and guidance inputs; it does not fly the aircraft’s path, and it can operate independently of the autopilot.

For our Aviation & Real-World Flying readers, autothrottle, auto throttle and automatic throttle describe the same general function. Airbus usually calls it autothrust, abbreviated A/THR, while Boeing commonly uses autothrottle, abbreviated A/T. Exact mode names and capabilities vary by aircraft, so the flight-mode annunciator, or FMA, is the authoritative indication of what the automation is doing.

What does an auto throttle system in an aircraft actually control?

An auto throttle system controls commanded engine thrust, but it is not necessarily controlling airspeed at every moment.

  1. A target and mode are established. The target may be a selected speed, an FMS-managed speed, a Mach number or an engine thrust reference such as a take-off or climb limit.
  2. The system measures aircraft and engine performance. Inputs can include indicated airspeed, Mach, acceleration, altitude, configuration, engine parameters and the active flight-guidance mode.
  3. The control law calculates a thrust command. In speed mode it adds or removes thrust according to speed error and trend. In a thrust mode it holds the calculated engine setting instead.
  4. The command reaches the engines. Some installations use servos to move the cockpit thrust levers. Others send an electronic demand to the engine-control computers while the levers remain stationary.
  5. The system monitors the result. It continually updates the command as wind, drag, configuration and flight path change, while respecting engine and thrust limits.

Large turbofan engines cannot change thrust instantly. Their spool time, aircraft inertia and the non-linear relationship between lever position and thrust explain why speed may move briefly after a configuration change or gust. Our explanation of how throttle position becomes engine thrust in a simulator covers this delay in more detail.

How does autothrottle work with the autopilot?

The autopilot controls the aircraft’s attitude and flight path, while autothrottle controls thrust; the active vertical mode determines which system is responsible for airspeed.

Typical situationAutothrottle commandWhat mainly controls speed
Level flight with a speed mode activeVaries thrustAutothrottle
Climb at a fixed climb-thrust settingMaintains the permitted climb thrustAircraft pitch
Idle descentCommands idle or near-idle thrustPitch, flight path and drag
Approach with speed mode activeVaries thrust as configuration and wind changeAutothrottle, within available thrust limits

This division is a frequent source of confusion. During a climb, the FMA may show a thrust mode such as THR CLB while the autopilot adjusts pitch to maintain speed. In a steep descent the autothrottle may already be at IDLE; because it cannot remove more thrust, the aircraft must use a shallower path, lower pitch or additional drag to stop accelerating.

Autopilot and autothrottle can normally operate separately. A pilot may hand-fly while autothrottle manages speed, or use the autopilot with manual thrust. See our guide to how pitch and thrust divide airspeed control across automation modes for the mode logic behind that relationship.

Autothrust vs autothrottle: how do Airbus and Boeing throttle systems differ?

Autothrust versus autothrottle is mainly a difference in manufacturer terminology and implementation, not a difference in aerodynamic purpose.

FeatureAirbus A320-style autothrustBoeing 737-style autothrottle
Common nameAutothrust, or A/THRAutothrottle, or A/T
Lever behaviourThrust levers normally remain in a selected detentServos normally move the thrust levers as commanded thrust changes
Engine commandFADEC varies thrust within the authority established by lever position and modeThe autothrottle servo repositions the levers; the engine controls then schedule thrust
Normal indicationFMA, thrust-limit indication and engine instrumentsFMA, lever movement and engine instruments
After take-offThe crew normally moves the levers to the climb detent at the appropriate pointThe active autothrottle mode normally moves the levers from take-off to climb thrust

When simmers compare an Airbus throttle with a Boeing throttle, this visible lever behaviour is usually the difference they mean. Stationary A320 thrust levers in the climb detent do not mean autothrust is inactive: engine thrust should still change as A/THR manages speed. Our guide to A320 lever detents, autothrust authority and FADEC commands explains the correct quadrant technique.

On a 737-style system, moving virtual thrust levers are expected because the autothrottle uses a servo. The active mode still matters: A/T may be controlling speed, setting take-off thrust or holding a thrust limit. The practical relationship between 737 autothrottle, MCP speed and VNAV modes shows when thrust controls speed and when pitch takes over.

These are familiar examples, not universal Airbus and Boeing rules. Individual aircraft families have different engagement logic, protections and landing behaviour. In a home simulator, a non-motorised physical Boeing throttle will also remain still even though the virtual cockpit levers move.

What does autothrottle do from take-off to landing?

The autothrottle’s job changes with the flight phase and active guidance mode.

  • Take-off: it sets or maintains a calculated take-off thrust. It is not trying to hold rotation speed while the aircraft accelerates along the runway.
  • Climb: it often holds a climb-thrust limit while pitch maintains the commanded speed or Mach number.
  • Cruise: it normally varies thrust to maintain selected or FMS-managed speed or Mach.
  • Descent: it may vary thrust to hold speed, or remain at idle while pitch, vertical path and drag determine speed.
  • Approach: it typically adjusts thrust as flap, landing gear, wind and glide-path corrections alter the power required. The crew must still verify that the selected or managed approach speed is appropriate.
  • Flare and landing: retard logic is type-specific. Some systems drive thrust towards idle, while an A320 crew normally moves the levers to idle in response to the RETARD callout. Automatic landing thrust behaviour must never be assumed from another aircraft type.

Why is the autothrottle not holding the selected speed?

If an autothrottle does not hold the selected speed, the usual cause is an unexpected mode, a thrust limit or an unwanted simulator control input rather than failed automation.

A mistake we see constantly in home simulators is chasing the speed-window value while the FMA says THR CLB or IDLE. In those modes, autothrottle is doing exactly what it was commanded to do; pitch or flight path is responsible for speed.

  1. Read the FMA first. Confirm whether autothrottle is active, merely armed or disconnected, then identify the active thrust mode. An illuminated arm switch does not prove that speed mode is controlling thrust.
  2. Check the target source. Verify selected versus FMS-managed speed and IAS versus Mach. A mode transition may change the target even though the speed-window value still looks familiar.
  3. Identify which system owns speed. In level flight or a vertical-speed descent, thrust may control speed. During a fixed-thrust climb or idle descent, pitch and flight path usually control it.
  4. Look for an authority limit. At maximum permitted thrust, an aircraft may still lose speed in an excessive climb. At idle, it may still accelerate down an overly steep descent. Autothrottle cannot deploy speedbrakes or create thrust beyond the engine limit.
  5. Verify lever and engagement states. A320-style autothrust normally requires the levers in the correct detent after thrust reduction. Boeing logic depends on both the A/T arm state and the active mode.
  6. Inspect simulator control assignments. Duplicate throttle bindings, axis noise, an uncalibrated Airbus detent, a reverse-thrust zone or assistance features can override the automated command. Check every connected controller, not just the quadrant being used.
  7. Allow for engine response. A sudden flap, gear or pitch change can produce a temporary speed deviation before the engines spool. Repeated manual throttle corrections often make the oscillation worse.
  8. Check for a recorded failure or disconnect. Warning messages, unavailable engine data or a latched disconnect may require the aircraft-specific re-engagement procedure. Do not assume that cycling the arm switch is a universal reset.

In a real aircraft, crews use the type-specific checklist or quick-reference procedure. Failure indications, manual override rules and restrictions on re-engagement differ between installations.

Can pilots disconnect or override autothrottle?

Pilots can disconnect autothrottle and control thrust manually while leaving the autopilot engaged, but the transfer must be deliberate and closely monitored.

The correct technique depends on the aircraft. It may require matching the physical levers to commanded thrust, pressing dedicated disconnect switches and acknowledging an alert. Moving an Airbus lever out of its normal detent can change or remove autothrust authority; manually moving a Boeing lever does not have identical consequences in every mode or model.

Does autothrottle prevent a stall or overspeed?

Autothrottle is not universal stall or overspeed protection. Some aircraft have low-speed recovery, automatic maximum-thrust or angle-of-attack functions, but these depend on aircraft design, flight-control law, configuration and system health.

Even a functioning speed mode cannot overcome an impossible energy state, an inappropriate target or insufficient engine performance. Pilots must monitor the FMA, airspeed trend and engine indications, then intervene when the commanded mode is not suitable.

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