A320 Systems — Autoflight

A320 Autoflight System — AP, FD, ATHR, FCU and FMA Logic

The A320 autoflight system does not merely fly the aircraft — it communicates its intentions through the FMA on every mode change. Pilots who understand that conversation rarely get surprised. Those who don't get caught in ATPL orals and, more importantly, in line operations.

Reviewed by the Captain Panel — 4 active airline captains, current DGCA ATPL·ATPL / Type Rating
A320 Systems Series
  1. 1. Hydraulic System — complete guide
  2. 2. Autoflight System — AP, FD, ATHR, FCU and FMA logic
  3. 3. Flight Controls — Normal law, Alternate law and Direct law
  4. 4. Electrical System
  5. 5. Pneumatics — Air conditioning, Pressurisation and Ventilation
  6. 6. Engines
  7. 7. APU
  8. 8. Fire Fighting
  9. 9. Landing Gear and Brakes
  10. 10. Ice and Rain Protection

The autoflight system on the A320 integrates three distinct but interdependent functions: the Autopilot (AP), the Flight Director (FD), and the Autothrust (ATHR). Each can operate independently, but in normal line operations they work as a coordinated system, managed through the Flight Control Unit (FCU) on the glareshield and monitored through the Flight Mode Annunciator (FMA) on the Primary Flight Display.

Understanding autoflight means understanding the FMA. Every mode engagement, every mode change, every armed-to-active transition is announced there. Pilots who read the FMA instinctively are ahead of the aircraft. Those who treat it as background noise are behind it.

System architecture — the four components

Diagram 1 — Autoflight system architecture
A320 Autoflight System ArchitectureFour components of the autoflight system: FCU (input), AP/FD, ATHR, and FMA (output), with their relationships and what each controls.FCUFlight Control UnitPilot input — glareshieldAPAutopilotControls flight surfacesvia FAC / ELAC / SEC2 independent APsFDFlight DirectorGuidance bars on PFDCommands to fly manuallyNo surface authorityATHRAutothrustControls thrust leversvia FADEC commandsSpeed or thrust modeFMAFlight Mode AnnunciatorTop of PFD — mode statuscommandscommandsannunciatesannunciatesCommand flowStatus / annunciation
The FCU is the pilot's interface. AP, FD, and ATHR are the execution layer. The FMA is the readback — it confirms what the system is actually doing.

Autopilot (AP): The A320 has two independent autopilots — AP1 and AP2. In normal operations only one is engaged at a time; both engage simultaneously only for CAT II & III approaches where independent monitoring is required. The AP sends commands to the flight control computers (ELAC, SEC, FAC) which move the control surfaces. Engaging the AP does not change what the FD shows — the AP simply follows the same guidance the FD was already presenting.

Flight Director (FD): The FD displays guidance bars on the PFD — pitch bar and bank bar — showing the pilot where to point the aircraft to follow the computed flight path. The FD has no authority over control surfaces. It is a display, not a controller. When flying manually with FD on, the pilot follows the bars. When the AP is engaged, the AP follows the bars automatically. Switching the FD off does not disconnect the AP.

Autothrust (ATHR): The ATHR controls thrust by commanding the FADECs. Unlike a conventional autothrottle, the A320's thrust levers do not move when ATHR is active — lever position defines the thrust envelope, not the commanded thrust. This is the most common source of confusion for pilots transitioning from aircraft with moving autothrottle levers. The levers set limits; the ATHR operates within them.

Flight Control Unit (FCU): The FCU on the glareshield is the crew's primary interface with the autoflight system. It controls target values (speed, heading/track, altitude, vertical speed/flight path angle) and switches between managed and selected guidance. Every FCU input either targets a specific value (selected) or hands control to the Flight Management System (managed).

Managed vs selected — the fundamental distinction

Every autoflight mode is either managed or selected. This is the distinction that ATPL orals probe most consistently, because it reveals whether a candidate understands the system or has merely memorised mode names.

Managed guidance means the FMS is in control of that parameter. The FCU window for that parameter shows dashes rather than a numerical value. The FMA annunciates the mode in magenta. The aircraft follows the FMS computed profile — the lateral route, the climb or descent profile, the speed schedule.

Selected guidance means the pilot has assigned a specific value via the FCU. The FCU window shows the numerical value. The FMA annunciates the mode in green (active) or blue (armed). The aircraft tracks that value.

The FCU window tells you who is flying: Dashes in the speed window means the FMS is managing speed. A number means the pilot has selected a target. Same logic applies to heading and vertical guidance windows. Look at the windows — they tell the story at a glance.

The FMA — reading the annunciator

The Flight Mode Annunciator occupies the top strip of the Primary Flight Display and is divided into five columns. Reading the FMA correctly, every time, is non-negotiable for safe autoflight operation — and it is the most examined topic in A320 type rating oral assessments.

The five FMA columns, left to right:

Column 1 — Autothrust mode: What the ATHR is doing. Common modes: MAN THR (manual thrust, ATHR not active), SPEED (ATHR is maintaining a speed target), or a fixed thrust rating being commanded. The thrust rating appears below the mode — THR CLB, THR MCT, THR IDLE, etc.

Column 2 — Vertical mode: How the aircraft is managing altitude and vertical flight path. Modes include: ALT (holding an altitude), ALT* (capturing an altitude — transitioning), CLB / DES (managed climb or descent following FMS profile), OP CLB / OP DES (open climb or descent to selected altitude), V/S (vertical speed mode), FPA (flight path angle mode), G/S* (glideslope capturing), G/S (glideslope captured on ILS approach).

Column 3 — Lateral mode: How the aircraft is tracking laterally. Modes include: NAV (following FMS lateral route), HDG (tracking a selected heading), TRACK (tracking a selected track), LOC (localiser captured or capturing), RWY (runway track on takeoff).

Column 4 — Approach capability: The approach capability (CAT 1, CAT 2, CAT 3 SINGLE, CAT 3 DUAL) displayed during approach phase. AP OFF in amber indicates the autopilot has disconnected.

Column 5 — AP, FD and ATHR status: AP1 or AP2 engagement status, which flight directors are active (1 FD 2 means both are on, left and right), and whether the Autothrust is armed or active (A/THR).

The 10-second box rule:Any new mode engagement on the FMA is boxed for 10 seconds. This is the system drawing the crew's attention to a mode change. The correct response is always to look at the FMA, confirm the boxed mode is what you expected, and call it out. A boxed mode you did not expect is an immediate cue to understand why.

Vertical modes — the most examined area

Diagram 2 — Vertical mode logic: managed vs selected, and key transitions
A320 Vertical Mode TransitionsFlow diagram showing how vertical modes transition during a typical flight, from takeoff through cruise to approach.TAKEOFFCLIMBCRUISEDESCENT/APPRSRSSpeed ReferenceV2+10 target / TOGACLBManaged climbFMS speed + profileALT*Altitude captureTransitioning to levelALTLevel holdAt FCU altitudeOP CLBOpen climbSelected altitude, max thrustV/SVertical speedPilot-selected fpm targetDES / OP DESManaged / open descentFMS path or selected altG/SGlideslopeILS glidepath capturedFLAREAuto flareCAT 2/3 onlypull FCUaltitudeILS armed→ capturedManaged mode (FMS controls)Selected mode (pilot sets target)Approach / landing modesPulling the FCU altitude knob selects OP CLB/DES. Turning selects a target. Pushing engages managed.
Managed modes (green) follow the FMS profile. Selected modes (amber) track a pilot-assigned value. The FCU knob action — push for managed, pull for selected — drives the transition.

The push/pull logic — the most common oral examination question

The FCU altitude knob has two actions: push and pull. This is the single most examined autoflight concept in A320 oral assessments, and the one most candidates initially get wrong.

  • Pull the altitude knob → Open Climb (OP CLB) or Open Descent (OP DES). The aircraft climbs or descends to the FCU altitude at maximum performance. A selected value is shown in the FCU window. This is the selected guidance mode for the vertical axis.
  • Push the altitude knob → Managed CLB or managed DES. The FMS takes control of the vertical profile. Dashes appear in the altitude window — the FMS is managing. The aircraft follows the FMS computed climb or descent path, which may not use maximum performance.
Memory rule: Pull = take control (selected). Push = give control to FMS (managed). The same logic applies to the speed and heading knobs — pull gives you a selected value; push gives the FMS control and shows dashes in the window.

V/S and FPA modes — and their risk

V/S (Vertical Speed) and FPA (Flight Path Angle) modes are selected by turning and pulling the FCU vertical speed/FPA knob. They allow the pilot to set a specific climb or descent rate.

The significant operational risk of V/S mode: the ATHR will attempt to maintain the commanded vertical speed even if doing so requires thrust settings that cause the aircraft to decelerate toward minimum speed or accelerate to maximum speed. V/S mode does not protect speed in the way that managed modes do. If an excessive descent rate is selected at a low thrust setting, the aircraft can approach minimum speed while still in an ostensibly normal descent. This is not a theoretical risk — it has been a factor in incidents. V/S must be used with awareness of the speed and thrust state.

Autothrust modes — speed vs thrust

The ATHR operates in one of two fundamental modes at any time:

Speed mode: The ATHR adjusts thrust to maintain the target speed. This is the normal mode during cruise and approach. The FMA annunciates SPEED in column 1. The aircraft holds the speed; altitude is managed by the pitch axis.

Thrust mode: The ATHR commands a fixed thrust rating — CLB, MCT, IDLE, or TOGA — and holds it regardless of speed variation. Speed is then controlled by the pitch axis (the FD and AP pitch commands). This is the normal mode during climb and descent in managed guidance. The FMA annunciates the thrust rating (CLB, MCT, etc.) in column 1.

ATHR modeWhat it controlsFMA column 1Typical phase
SPEEDAdjusts thrust to maintain speed targetSPEEDCruise, approach
THR CLBHolds climb thrust ratingTHR CLBManaged climb
THR MCTHolds maximum continuous thrustTHR MCTEngine-out climb
THR IDLECommands idle thrustTHR IDLEManaged descent
A.FLOORCommands TOGA — automatic protectionA.FLOORAlpha floor activation
TOGA LKTOGA locked after alpha floor — requires resetTOGA LKAfter alpha floor event

Alpha Floor is the ATHR protection mode that automatically applies TOGA thrust when the aircraft reaches a high angle of attack threshold, regardless of thrust lever position. Once activated, it locks to TOGA LK on the FMA — the crew must manually move thrust levers to TOGA and then select a lower setting to reset. Alpha Floor activation in normal operations is an abnormal event requiring crew action and understanding of the reset procedure.

Key numbers and limitations

ParameterValue
Autopilots available2 (AP1, AP2)
AP engagement minimum height (takeoff)100 ft AGL
AP engagement minimum height (approach)Per approach type
Both APs engaged simultaneouslyCAT 2/3 approach
FMA new mode box duration10 seconds
Alpha floor activation AoA (approx.)~9.5° (conf 0) to ~14° (conf full) — varies by aircraft
ATHR speed mode typical activationWhen thrust mode no longer required
FCU altitude knob — pullOP CLB / OP DES (selected)
FCU altitude knob — pushManaged CLB / DES (FMS)

Summary

The A320 autoflight system rewards pilots who understand the logic rather than memorise the modes. The FCU is the interface — every knob push or pull either takes authority away from the FMS or gives it back. The FMA is the readback — it tells you what the system is actually doing, and it boxes every mode change for 10 seconds specifically to demand your attention.

The managed vs selected distinction runs through every aspect of the system: managed speed shows dashes and annunciates in magenta; selected speed shows a number and annunciates in green. The ATHR is either managing speed or holding a thrust rating — not both simultaneously. The vertical mode is either following the FMS profile or tracking a pilot-selected value.

Understand those three distinctions clearly and the system becomes predictable. A predictable autoflight system is a safe one.

Note:This article reflects general A320 family autoflight architecture. Specific mode logic, engagement conditions, and limitations vary by aircraft variant, software standard, and operator procedures. Always refer to your aircraft's approved FCOM and your operator's Operations Manual for authoritative procedures. Content reviewed by the ProPilotLicence Captain Panel — four or more active commercial airline captains holding current DGCA CPL and ATPL licences.
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