Development milestones
First flight: 2 November 1992 ( 1992-11-02 )
Developed from: Airbus A300
VliegtuigbibliotheekAirbus A330 family
4300streetcar · CC BY 4.0 · Delta Air Lines A330-300Airbus A330 family
A long-haul twin whose family spans passenger, freight and specialist transport roles.
Airliner19 profielkeuzes
Ken het vliegtuig
Airbus developed the A330 alongside the four-engine A340. The two programmes shared substantial airframe and cockpit work, but the A330 used two engines. The initial A330-300 entered service in 1994; the shorter A330-200 followed in 1998.
The family includes several engine choices, different fuselage lengths and later A330neo developments. These distinctions reach inside the cockpit: engine indications and fuel arrangements are not identical across every version. The simulator products cover different variants, each with its own developer documentation.
Meer over dit vliegtuig op AirframeDB
Taking a twin-engine airliner to the Antarctic ice
Mirpuri's log describes the preparation behind Hi Fly's A330 mission from Cape Town to Wolf's Fang. The aircraft carried fuel for the return as well as the outward journey, and the team monitored fuel temperature, destination weather and runway condition throughout the flight. Forecast discussions began days beforehand. Ground power and starting equipment at the remote strip were also part of making the twin-engine operation possible.
Four pilots shared the long duty, supported by engineers, cabin crew, a ground coordinator and colleagues at both bases. Mirpuri recalls touching down just before midnight local time, when the Antarctic summer sun was still above the horizon and katabatic winds were beginning to rise. The aircraft stopped as planned, turned and taxied to parking before returning to Cape Town later. His airline-published account stresses the contribution of the whole team to a landing intended to feel uneventful.
A familiar flight deck and a sharper response on approach
Gerzanics flew the A330-800 test aircraft F-WTTO from Toulouse with Airbus test pilot Thomas Wilhelm. Although he did not routinely fly Airbus aircraft, the common cockpit felt familiar. The aircraft was still contributing to flight-control development, and a special display helped him practise the consistent sidestick input needed for the takeoff test. In the air, he found it easy to establish bank angles and roll out accurately on a heading.
On the return, the instrument landing system's glideslope went out of service. Wilhelm suggested using the head-up display while setting up an alternative ground-augmented satellite approach. Gerzanics then assessed the aircraft's response by deliberately offsetting from, and rejoining, the final approach course. He found the response crisp and the landing straightforward. This was an organised evaluation in an instrumented A330-800, including test manoeuvres.
Learning to wait for a larger aircraft’s response
After thirteen years flying the A320 family around Europe, Harder was preparing to return to long-haul work on the A330. He describes receiving the training assignment after applying for a conversion, then working through technical material at home before moving into procedural and full-flight simulators. His Airbus experience shortened part of the training, but the new aircraft still had different systems to learn.
Asked how the A330 felt in the simulator, he noticed a more delayed response to control inputs, reminding him of his earlier experience as a Boeing 747 first officer. He had to allow a little time for the larger aircraft to respond. At the time of the interview, his simulator check and line training still lay ahead. His conversion training took place in the simulator; he had not yet completed his A330 qualification.
Openbare bronnen 21
- Airbus A330Research background · Wikipedia revision 1373820047 · retrieved 2026-09-12
- Airbus A330
- Microsoft Flight Simulator aircraft manuals
- MSFS 2024 FAQ and edition aircraft inventory
- Airbus Beluga XL
- Airbus A330-300 POH
- X-Plane 12 Desktop Manual
- X-Plane aircraft and avionics manuals
- A330-900 change log
- A330 900Official developer / designated store catalogue · checked 2026-09-12
- Captain’s log: landing the first Airbus A330 in AntarcticaCarlos Mirpuri · 5 December 2025
- The flight test of Airbus’s refreshed widebody – the A330neoMike Gerzanics · 2019
- Umschulung auf den Airbus A330 – Upgrade für einen KapitänClaus Harder · 5 May 2023
- ICAO Doc 8643 — aircraft type designatorsPublic search data retrieved 2026-09-14; authority update 2026-09-03
- Aerosoft Aircraft A330 neoProduct listing captured 28 September 2026; A330-900neo, MSFS 2024
- A330-300Product listing captured 2026-09-24; edition scope from the reviewed catalogue
- A339X A330-900neoProduct listing captured 2026-09-24; edition scope from the reviewed catalogue
- JARDesign 330 Airliner -JARDesign-A330Product listing captured 2026-09-30; edition scope from the reviewed catalogue
- Airbus A330-200 exact product reviewProduct listing captured 2026-09-24; edition scope from the reviewed catalogue
- Airbus A330-300 exact product reviewProduct listing captured 2026-09-24; edition scope from the reviewed catalogue
- Airbus A330-900neo exact product reviewProduct listing captured 2026-09-24; edition scope from the reviewed catalogue
Hoe het profiel het modelleert
Airbus A330-900
Free + ProMSFS 2024X-Plane 11X-Plane 12
Airbus developed the A330 alongside the four-engine A340. The two programmes shared substantial airframe and cockpit work, but the A330 used two engines. The initial A330-300 entered service in 1994; the shorter A330-200 followed in 1998.
This starting point selects Airbus A330-900. Its aircraft-level settings do not select a particular developer’s custom systems.
The spring stays independent of airspeed. Directed aerodynamic loading is omitted.
Pitch-trim relief is off. Autopilot following is off.
Deze exacte revisie is nog niet beschikbaar voor openbare installatie.
Controls and trim
The A330 cockpit uses Airbus sidesticks and fly-by-wire. The bundled manual separates the -200/-300 fuel and trim-tank arrangements, while the Beluga XL has its own flight-control and autopilot guide. A330neo, passenger-to-freighter and corporate configurations retain their model identities. Aircraft trim and autopilot guidance belong to the flight-control system; they do not establish surface-airload feedback through a passive stick.
About the values
The gains are normalized profile settings. They describe the chosen effect balance; hand force depends on the device and its output limits. IAS references are tuning values rather than operating limits. Physical acceptance of this revision remains pending.
Master gain & control system
Master gain85%
De uiteindelijke totaalschaal over alles wat het model produceert, vóór de apparaatbegrenzing.
Meer: alles (veer, belastingen, effecten) wordt samen sterker.
Minder: alles wordt samen zachter.
Waarom hier: Scales overall profile strength while preserving effect balance, subject to device and output limits.
Forces
Spring strength55%
De basiscentreerkracht die de stick terug naar het midden trekt. Elke andere kracht stapelt hierop. Te laag en de stick voelt slap in normale vlucht; te hoog en hij vecht tegen je hand en maskeert de kleinere signalen erbovenop.
Meer: een steviger centreren dat de hand meer weerstaat.
Minder: een slappere stick die alleen op aerodynamische belasting leunt.
Waarom hier: Fixed sidestick centering represents the Airbus control arrangement while keeping aircraft control-law behavior separate from hardware resistance. The baseline spring is 0.55. Low-speed spring blending is off.
Cockpit and flight control familiesAirbus A330Airbus Beluga XLSpring deadband1%
Een kleine neutrale zone rond het midden waar de veer stil blijft, zodat minieme bewegingen in rust niet ratelen. Breder is rustiger maar losser; smaller is preciezer maar kan rond het midden trillen.
Meer: een rustiger maar losser midden, met meer speling.
Minder: een strakker midden dat in rust kan trillen.
Waarom hier: Sets travel around the centre before the baseline spring resists. Smaller values engage it sooner.
Forces · Center starting force0.03
Waarom hier: The centre preload is 0.03. It ramps outside the 0.01 deadband across 0.05 travel, shaping the passive centre independently of aircraft autotrim.
Forces · Center starting force transition0.05
Waarom hier: Sets the travel used to ramp in centre preload. Wider intervals make its onset more gradual.
Overall aerodynamic load4%
Een masterschaal over beide aangehouden asbelastingen, toegepast vóór hun onafhankelijke balans. Profielen laten dit normaal met rust en stemmen de twee asbelastingen af.
Meer: beide assen laden zwaarder.
Minder: beide assen worden samen lichter.
Waarom hier: The stored 0.04 aerodynamic-load gain is inactive under the fixed-centre control law.
Airspeed blendingFalse
Schakelt het lage-snelheidsvenster van de veeraangrijping in (start/vol-knopen hierboven). Uit betekent een constante veer op alle snelheden.
Waarom hier: Allows baseline spring strength to rise with indicated airspeed where the control law permits it.
Low-speed spring floor50%
Hoeveel van de veer overleeft bij stilstand, voordat luchtsnelheid aerodynamische kracht kan opbouwen. Een hoge vloer houdt de geparkeerde stick stevig; een lage geeft het losse, kabelslappe gevoel van een geparkeerd licht vliegtuig.
Meer: een stevigere stick geparkeerd en tijdens taxiën.
Minder: een slappe stick geparkeerd die pas met snelheid ontwaakt.
Waarom hier: Sets low-speed spring strength as a fraction of baseline when blending is enabled. One keeps full strength.
Spring engagement start20 kt
De snelheid waarbij de veer vanaf zijn lage-snelheidsvloer richting volle sterkte begint te klimmen: de besturing die 'tot leven komt' tijdens de startrol.
Waarom hier: Sets the IAS where the low-speed spring blend starts rising. This is a feel threshold, not a flight limit.
Spring engagement full90 kt
De snelheid waarbij de veer volle sterkte bereikt. Tussen het begin en dit punt wordt het centreren geleidelijk steviger naarmate de luchtstroom over de roeren groeit.
Waarom hier: Sets the IAS where the low-speed blend reaches baseline strength; high-speed stiffening also uses it.
Snelheid voor krachtafstemming270
De aangewezen snelheid waarbij de aerodynamische belasting haar ontworpen volle niveau bereikt. Hij verankert de hele belastingscurve aan het echte snelheidsbereik van het vliegtuig: een 172 laadt op tegen 110 knopen, een jet veel later.
Meer: belastingen komen later; de stick blijft langer licht.
Minder: belastingen komen eerder en de kruisvlucht weegt zwaarder.
Waarom hier: Sets the IAS reference for aerodynamic loading. It is an estimate, not published cruise TAS or a flight limit.
Centre firmness vs speed0%
Hoeveel het centreren zelf met snelheid verstijft, bovenop de uitslagbelastingen. Nul houdt het middengevoel constant; meer laat de stick harder centreren op kruissnelheid en losser in het circuit.
Meer: een midden dat duidelijk verhardt met snelheid.
Minder: een constant middengevoel op elke snelheid.
Waarom hier: Adds permitted spring resistance above the full-blend speed. Zero removes this high-speed increase.
Centre stiffening cap5
De bovengrens van snelheidsgedreven centreerverstijving, zodat zeer snelle vlucht de veer niet onbegrensd kan opwinden.
Meer: meer totale verstijving toegestaan op hoge snelheid.
Minder: de verstijving stopt eerder.
Waarom hier: Limits the squared airspeed ratio used for high-speed spring stiffening; it is not a device-force cap.
Aileron load100%
De aangehouden rolbelasting uit rolroeruitslag en snelheid, onafhankelijk van pitch gebalanceerd. Samen met de hoogteroerbelasting bepaalt dit de stuurharmonie waar recensenten het over hebben.
Meer: zwaardere rolkrachten.
Minder: lichtere, levendigere rolroeren.
Waarom hier: Roll and pitch aerodynamic scales are 1 and 1, respectively. These stored weights do not create directed aerodynamic loading while that term is inactive. The pitch spring-travel curve reaches output 1 at input 1. The roll spring-travel curve reaches output 0.3 at input 1. Spring-travel response contributes separately to axis balance.
Elevator load100%
De aangehouden pitchbelasting uit hoogteroeruitslag en snelheid, onafhankelijk van rol gebalanceerd. Dit is de hoofdhendel achter het pitchgewicht van een type. Hij raakt rolroer-, veer-, trim- of buffetkrachten niet.
Meer: zwaardere aangehouden pitchkrachten op snelheid.
Minder: een lichter hoogteroer, minder spierkracht om vast te houden.
Waarom hier: Scales pitch aerodynamic loading; pitch spring travel and trim responses are separate settings.
Max output force55%
Een plafond op elke gestage pitch- of rolkracht voordat die het apparaat bereikt, ter bescherming tegen beuken of verzadigen van de hardware bij stevige manoeuvres.
Meer: hogere gestage krachtpieken vóór afkapping.
Minder: een zachter plafond; harde manoeuvres vlakken eerder af.
Waarom hier: Caps directed-force output. Native spring effects and device limits remain separate.
Trim
Trim relief (elevator)0%
Hoe sterk hoogteroertrim de vastgehouden pitchkracht verlicht en verschuift waar de stick tot rust komt. Op 100 % heeft een goed getrimd vliegtuig geen vastgehouden druk nodig, de trim-de-last-weg-werkwijze van echt vliegen.
Meer: trim neemt meer vastgehouden kracht weg; op 100 % heft volle trim hem op.
Minder: je blijft kracht houden, zelfs getrimd.
Waarom hier: Aircraft automatic trim is independent of the selected passive stick centre; the trim-tank arrangement is not a hardware trim command. Pitch relief is off, with stored authority 0; roll authority is 0.
Cockpit and flight control familiesAirbus A330Airbus Beluga XLTrim relief (aileron)0%
Dezelfde verlichting voor roltrim. De meeste GA-types hebben geen echte rolroertrim, dus dit blijft op nul; types met roltrim krijgen een passende waarde.
Meer: roltrim neemt meer vastgehouden kracht weg.
Minder: roltrim doet minder.
Waarom hier: Scales supported roll-trim relief and permitted centre movement. Zero removes roll response.
Effect gains · Ground
Runway rumble0%
Rollende oppervlaktetrilling uit wielsnelheid en ondergrondtype: asfalt, gras of grind onder het onderstel.
Meer: een sterkere oppervlaktetextuur in de stick.
Minder: gladder taxiën.
Waarom hier: Sets rolling texture strength, modified by speed, surface and undercarriage configuration.
Gear bumps0%
Korte losse stoten van uitzetvoegen, sporen en ruw oppervlak, die het doorlopende gerommel accentueren.
Meer: scherpere stoten van voegen en sporen.
Minder: zachtere gronddetails.
Waarom hier: Sets gear-bump texture during ground motion, separate from touchdown impact.
Effect gains · Airframe
Stall buffet6%
Casco-schudden bij het naderen van de overtrek en terwijl de overtrekwaarschuwing actief is: hoe luid deze vleugel aankondigt dat hij ontevreden is. Types met een scherpe afbreek krijgen bescheiden buffet en laten de hoorn de waarschuwing dragen.
Meer: een sterker trillen vóór de overtrek.
Minder: een discretere vleugel; de hoorn draagt de waarschuwing.
Waarom hier: Sets stall-buffet strength. Zero removes the cue without changing simulator stalls or warnings.
Mach buffet6%
Transsoon buffet bij het naderen van de Machlimiet. Betekenisvol voor jets nabij MMO, nul voor zuigers en turboprops die er nooit komen.
Meer: een sterker transsoon buffet nabij de Machlimiet.
Minder: gladder vliegen op hoge Mach.
Waarom hier: Sets high-Mach buffet strength; onset and full-strength thresholds are separate.
Flap buffet0%
Laagfrequente casco-trilling met kleppen uitgeslagen in de luchtstroom, in het snelheidsvenster waar ze de lucht echt bewerken.
Meer: ruwer vliegen met werkende kleppen.
Minder: zachtere naderingskleppen.
Waarom hier: Sets flap buffet at the configured position and speed gates. Flap movement texture is separate.
Gear buffet0%
Casco-getrommel van intrekbaar onderstel dat in de luchtstroom hangt. Nul voor types met vast onderstel, waar het casco nooit van vorm verandert.
Meer: meer getrommel met het onderstel uit.
Minder: schoner vliegen met onderstel uit.
Waarom hier: Sets gear aerodynamic buffet; movement and ground-contact cues are separate.
Stick shaker50%
De speciale stall-stickshakerzoem, geactiveerd door het eigen overtrekwaarschuwingssysteem van het vliegtuig. Alleen types met een echte shaker krijgen een waarde; de rest steunt op aerodynamisch buffet en de hoorn.
Meer: een hardere shaker.
Minder: een discretere shaker.
Waarom hier: Sets triggered shaker strength; inactive while the shaker feature is disabled.
Effect gains · Engine, mechanical & drag
Touchdown thump0%
De eenmalige dreun als de wielen de baan raken, geschaald op daalsnelheid: een zachte landing fluistert, een stevige aankomst bonkt.
Meer: een hardere dreun bij de landing.
Minder: zachtere aankomsten.
Waarom hier: Sets landing-impact strength; landing telemetry and response shape determine the pulse.
Reverse rumble0%
Uitroltrilling terwijl reverse thrust of props in beta werken. Nul voor types zonder reverse.
Meer: ruwer uitrollen onder reverse.
Minder: een discretere reverse.
Waarom hier: Sets reverse-thrust vibration with valid reverser and engine conditions. Zero removes the cue.
Engine rumble0%
Doorlopende motortrilling die het toerental volgt tussen stationair en vol vermogen, de altijd aanwezige herinnering dat er voorin iets brandstof verbrandt.
Meer: meer motor in de stick.
Minder: een discretere motor.
Waarom hier: Sets estimated engine vibration using configured telemetry and response, not measured cockpit vibration.
Flap motion0%
Doorlopende trilling alleen terwijl de sim meldt dat de klepvlakken daadwerkelijk bewegen. Volgt echte actuatorbeweging en storingen, geen geschatte timer.
Meer: meer trilling met bewegende kleppen.
Minder: discretere klepbewegingen.
Waarom hier: Sets texture from observed flap movement; a command without movement does not establish the cue.
Autopilot follow
AP follow authority5%
Hoe ver autopilootcommando's de stick fysiek mogen bewegen. Piepklein gehouden in MSFS, waar een bewogen as kan worden teruggelezen als pilooteninvoer; nul schakelt volgen volledig uit.
Meer: de autopiloot beweegt je stick zichtbaar meer.
Minder: een nauwelijks merkbaar volgen.
Waarom hier: Sets admitted AP-follow gain, not a percentage of travel. Runtime ownership and input limits still apply.
Spring response
SpringResponse · Travel enabledTrue
Whether this feature is active in this profile.
Waarom hier: Applies the configured pitch and roll spring travel curves.
SpringResponse · Output1
Waarom hier: Sets response at the second pitch-curve point; it is an endpoint only if its input position is full travel.
SpringResponse · Output0.3
Waarom hier: Sets response at the second roll-curve point; its input position and other points determine the travel law.
Stick feel
StickFeel · Trim feel enabledFalse
Whether this feature is active in this profile.
Waarom hier: Retained for compatibility and group membership. Trim relief, rather than this flag, controls centre movement.
StickFeel · Trim relief enabledFalse
Whether this feature is active in this profile.
Waarom hier: Allows trim relief with supported control law and valid telemetry. Axis authorities set its amount.
StickFeel · Force trim enabledFalse
Whether this feature is active in this profile.
Waarom hier: Enables local force trim, separate from aircraft-owned trim and add-on integration qualification.
StickFeel · G load enabledFalse
Whether this feature is active in this profile.
Waarom hier: Allows load-factor changes to modify permitted spring laws. Passive fly-by-wire feel can suppress it.
StickFeel · Rate damping enabledFalse
Whether this feature is active in this profile.
Waarom hier: Enables rate damping with the configured coefficients and control law.
Autopilot
Autopilot · Follow enabledFalse
Whether this feature is active in this profile.
Waarom hier: Autopilot following is off; the configured spring and load retain the hardware feel. Separate neutral hold is on at strength 0.28, when a supported autopilot state admits it.
Autopilot · Neutral hold enabledTrue
Whether this feature is active in this profile.
Waarom hier: Permits centering hold during a supported AP state, separate from following a moving target.
Autopilot · Neutral hold strength0.28
Waarom hier: Sets admitted AP neutral-hold strength; inactive while neutral hold is disabled.
Aero
Aero · EnabledTrue
Whether this feature is active in this profile.
Waarom hier: Enables aerodynamic cues; each still needs nonzero strength and its simulator conditions.
Aero · Max flap index4
Where this effect reaches full strength (or has fully faded, for washouts).
Meer: a more gradual build to a later peak.
Minder: a quicker build.
Waarom hier: Sets the final flap index for detent normalization. UP plus three detents uses maximum index3.
Aero · Min flap index2
Where this effect begins fading in.
Meer: the effect begins later.
Minder: it begins earlier.
Waarom hier: Sets the first flap detent that admits buffet; this is a handle index, not degrees.
Aero · Shaker enabledFalse
Whether this feature is active in this profile.
Waarom hier: Permits shaker at supported warning conditions; the switch does not establish aircraft equipment.
Ground
Ground · EnabledFalse
Whether this feature is active in this profile.
Waarom hier: Enables ground effects; each still needs its own strength and contact or motion telemetry.
Engine
Engine · EnabledFalse
Whether this feature is active in this profile.
Waarom hier: Enables engine cues with nonzero settings and valid running-engine telemetry.
Mechanical
Mechanical · EnabledTrue
Whether this feature is active in this profile.
Waarom hier: Enables accessory cues with configured strengths and observed accessory movement.
Mechanical · Gain0
The strength of this effect.
Meer: a stronger effect.
Minder: a weaker one.
Waarom hier: Sets texture from observed gear movement, separate from aerodynamic and touchdown effects.
Alle profielinstellingen
| Parameter | Waarde | Wat het regelt en waarom |
|---|---|---|
| Spring strength | 0.55 | Fixed sidestick centering represents the Airbus control arrangement while keeping aircraft control-law behavior separate from hardware resistance. The baseline spring is 0.55. Low-speed spring blending is off. |
| Spring deadband | 0.01 | Sets travel around the centre before the baseline spring resists. Smaller values engage it sooner. |
| Forces · Center starting force | 0.03 | The centre preload is 0.03. It ramps outside the 0.01 deadband across 0.05 travel, shaping the passive centre independently of aircraft autotrim. |
| Forces · Center starting force transition | 0.05 | Sets the travel used to ramp in centre preload. Wider intervals make its onset more gradual. |
| Force gain | 0.04 | The stored 0.04 aerodynamic-load gain is inactive under the fixed-centre control law. |
| Master gain | 0.85 | Scales overall profile strength while preserving effect balance, subject to device and output limits. |
| Dynamic-pressure blend | False | Allows baseline spring strength to rise with indicated airspeed where the control law permits it. |
| Minimum spring factor | 0.5 | Sets low-speed spring strength as a fraction of baseline when blending is enabled. One keeps full strength. |
| Spring wake-up speed | 20 kt | Sets the IAS where the low-speed spring blend starts rising. This is a feel threshold, not a flight limit. |
| Spring full-strength speed | 90 kt | Sets the IAS where the low-speed blend reaches baseline strength; high-speed stiffening also uses it. |
| Snelheid voor krachtafstemming | 270.0 kt | Sets the IAS reference for aerodynamic loading. It is an estimate, not published cruise TAS or a flight limit. |
| Airspeed spring stiffening | 0 | Adds permitted spring resistance above the full-blend speed. Zero removes this high-speed increase. |
| Airspeed stiffening cap | 5 | Limits the squared airspeed ratio used for high-speed spring stiffening; it is not a device-force cap. |
| Aileron force scale | 1 | Roll and pitch aerodynamic scales are 1 and 1, respectively. These stored weights do not create directed aerodynamic loading while that term is inactive. The pitch spring-travel curve reaches output 1 at input 1. The roll spring-travel curve reaches output 0.3 at input 1. Spring-travel response contributes separately to axis balance. |
| Elevator force scale | 1 | Scales pitch aerodynamic loading; pitch spring travel and trim responses are separate settings. |
| Maximum output force | 0.55 | Caps directed-force output. Native spring effects and device limits remain separate. |
| SpringResponse · Travel enabled | True | Applies the configured pitch and roll spring travel curves. |
| SpringResponse · Output | 1 | Sets response at the second pitch-curve point; it is an endpoint only if its input position is full travel. |
| SpringResponse · Output | 0.3 | Sets response at the second roll-curve point; its input position and other points determine the travel law. |
| StickFeel · Trim feel enabled | False | Retained for compatibility and group membership. Trim relief, rather than this flag, controls centre movement. |
| StickFeel · Trim relief enabled | False | Allows trim relief with supported control law and valid telemetry. Axis authorities set its amount. |
| StickFeel · Elevator authority | 0 | Aircraft automatic trim is independent of the selected passive stick centre; the trim-tank arrangement is not a hardware trim command. Pitch relief is off, with stored authority 0; roll authority is 0. |
| StickFeel · Aileron authority | 0 | Scales supported roll-trim relief and permitted centre movement. Zero removes roll response. |
| StickFeel · Force trim enabled | False | Enables local force trim, separate from aircraft-owned trim and add-on integration qualification. |
| StickFeel · G load enabled | False | Allows load-factor changes to modify permitted spring laws. Passive fly-by-wire feel can suppress it. |
| StickFeel · Rate damping enabled | False | Enables rate damping with the configured coefficients and control law. |
| Autopilot · Follow enabled | False | Autopilot following is off; the configured spring and load retain the hardware feel. Separate neutral hold is on at strength 0.28, when a supported autopilot state admits it. |
| Autopilot · Follow authority | 0.05 | Sets admitted AP-follow gain, not a percentage of travel. Runtime ownership and input limits still apply. |
| Autopilot · Neutral hold enabled | True | Permits centering hold during a supported AP state, separate from following a moving target. |
| Autopilot · Neutral hold strength | 0.28 | Sets admitted AP neutral-hold strength; inactive while neutral hold is disabled. |
| Aero · Enabled | True | Enables aerodynamic cues; each still needs nonzero strength and its simulator conditions. |
| Aero · Gain | 0.06 | Sets stall-buffet strength. Zero removes the cue without changing simulator stalls or warnings. |
| Aero · Gain | 0.06 | Sets high-Mach buffet strength; onset and full-strength thresholds are separate. |
| Aero · Gain | 0 | Sets flap buffet at the configured position and speed gates. Flap movement texture is separate. |
| Aero · Max flap index | 4 | Sets the final flap index for detent normalization. UP plus three detents uses maximum index3. |
| Aero · Min flap index | 2 | Sets the first flap detent that admits buffet; this is a handle index, not degrees. |
| Aero · Gain | 0 | Sets gear aerodynamic buffet; movement and ground-contact cues are separate. |
| Aero · Shaker enabled | False | Permits shaker at supported warning conditions; the switch does not establish aircraft equipment. |
| Aero · Amplitude | 0.5 | Sets triggered shaker strength; inactive while the shaker feature is disabled. |
| Ground · Enabled | False | Enables ground effects; each still needs its own strength and contact or motion telemetry. |
| Ground · Gain | 0 | Sets rolling texture strength, modified by speed, surface and undercarriage configuration. |
| Ground · Gain | 0 | Sets gear-bump texture during ground motion, separate from touchdown impact. |
| Ground · Gain | 0 | Sets landing-impact strength; landing telemetry and response shape determine the pulse. |
| Ground · Gain | 0 | Sets reverse-thrust vibration with valid reverser and engine conditions. Zero removes the cue. |
| Engine · Enabled | False | Enables engine cues with nonzero settings and valid running-engine telemetry. |
| Engine · Gain | 0 | Sets estimated engine vibration using configured telemetry and response, not measured cockpit vibration. |
| Mechanical · Enabled | True | Enables accessory cues with configured strengths and observed accessory movement. |
| Mechanical · Gain | 0 | Sets texture from observed flap movement; a command without movement does not establish the cue. |
| Mechanical · Gain | 0 | Sets texture from observed gear movement, separate from aerodynamic and touchdown effects. |
Openbare bronnen 22
- Airbus A330Research background · Wikipedia revision 1373820047 · retrieved 2026-09-12
- Cockpit and flight control familiesAirbus cockpit family descriptions; Airbus cockpit commonality, sidestick philosophy; Airbus cockpit commonality
- Airbus A330Airbus A330 family
- Airbus Beluga XLAirbus A330 family
- Microsoft Flight Simulator aircraft manuals
- MSFS 2024 FAQ and edition aircraft inventory
- Airbus A330-300 POH
- X-Plane 12 Desktop Manual
- X-Plane aircraft and avionics manuals
- A330-900 change log
- A330 900Official developer / designated store catalogue · checked 2026-09-12
- Captain’s log: landing the first Airbus A330 in AntarcticaCarlos Mirpuri · 5 December 2025
- The flight test of Airbus’s refreshed widebody – the A330neoMike Gerzanics · 2019
- Umschulung auf den Airbus A330 – Upgrade für einen KapitänClaus Harder · 5 May 2023
- ICAO Doc 8643 — aircraft type designatorsPublic search data retrieved 2026-09-14; authority update 2026-09-03
- Aerosoft Aircraft A330 neoProduct listing captured 28 September 2026; A330-900neo, MSFS 2024
- A330-300Product listing captured 2026-09-24; edition scope from the reviewed catalogue
- A339X A330-900neoProduct listing captured 2026-09-24; edition scope from the reviewed catalogue
- JARDesign 330 Airliner -JARDesign-A330Product listing captured 2026-09-30; edition scope from the reviewed catalogue
- Airbus A330-200 exact product reviewProduct listing captured 2026-09-24; edition scope from the reviewed catalogue
- Airbus A330-300 exact product reviewProduct listing captured 2026-09-24; edition scope from the reviewed catalogue
- Airbus A330-900neo exact product reviewProduct listing captured 2026-09-24; edition scope from the reviewed catalogue
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