Development milestones
Developed from: Cirrus SR20
FlugzeugbibliothekCirrus SR22
ZLEA · CC BY-SA 4.0 · Cirrus SR22 G2 GTS (N137SR, cn 1916) (4-13-2024).Cirrus SR22
A composite touring single with a whole-aircraft parachute and several generations of avionics.
General aviation7 Profiloptionen
Kenne das Flugzeug
The SR22 entered production in 2001 as a more powerful development of Cirrus's SR20. A low wing, fixed tricycle gear and side-yoke controls define the basic layout. The Cirrus Airframe Parachute System is a prominent part of the aircraft's design.
The SR22 family spans normally aspirated and turbocharged versions as well as different panel generations. The side controls use mechanical connections. Simulator implementations range from bundled aircraft to detailed add-ons with their own engine, maintenance and avionics models.
Cirrus SR22 · Specifications (SR22-G5) · real aircraft; source units retained
- Length
- 26 ft 0 in (7.92 m)↗
- Wingspan
- 38 ft 4 in (11.68 m)↗
- Height
- 8 ft 11 in (2.72 m)↗
- Empty weight
- 2,269 lb (1,029 kg)↗
- Gross weight
- 3,600 lb (1,633 kg)↗
- Powerplant
- 1 × Continental IO-550-N Six cylinder horizontally opposed aircraft engine, 310 hp (230 kW)↗
- Propellers
- 3-bladed↗
- Cruise speed
- 183 kn (211 mph, 339 km/h)↗
- Stall speed
- 60 kn (69 mph, 110 km/h) flaps down↗
- Range
- 1,049 nmi (1,207 mi, 1,943 km) with reserves at 65% power↗
Mehr über dieses Flugzeug auf AirframeDB
Learning to stay ahead of a more demanding trainer
Ambats moved from a Cessna 172 into an Avidyne-equipped SR22 during her private-pilot training at Santa Monica. Other pilots had questioned whether the powerful Cirrus was an appropriate student aircraft, and she initially shared their concern. Her first lessons brought stronger acceleration, much more right-pedal pressure on takeoff and a cockpit full of unfamiliar information. The side control felt natural, but sensitive electric trim and quicker responses made familiar exercises such as steep turns harder to perform neatly.
With instructor Liz DeStaffany, practice gradually made the busy cockpit manageable. Ambats learned to use the display pages she needed while keeping her attention outside, and to make small trim adjustments after establishing the attitude. The traffic pattern began to feel less hurried. When DeStaffany and Cirrus pilot Rachel Tanzer stepped out for her solo, apprehension had become excitement. Ambats remembers climbing away while the same 172 she had previously soloed circulated nearby, now seeming remarkably slow.
A biplane pilot discovers the appeal of a travelling aircraft
Lee approached the 2012 SR22T with the prejudices of a pilot who preferred biplanes and tailwheel flying. A trip from Southern California to the San Francisco Bay Area, accompanied by Cirrus representative Matt Bergwall and editor Jessica Ambats, changed his view. Hand-flying the first part of the journey, he found substantial, balanced control forces rather than a lightweight feel. The side control still required adjustment, but it freed space in front of him.
As the trip continued, the cabin, integrated avionics and straightforward presentation of information began to make sense as aids to an enjoyable journey. He describes cruising above California farmland, trying the satellite telephone and arriving at San Carlos without drama before a Golden Gate photo flight. On the return, Ambats flew while he stretched out in a reclining rear seat with a book. He still wanted his biplane for an open-air flying experience; the Cirrus had shown him why comfort and convenience matter when the purpose is getting somewhere with friends.
Seven years of trips, family flying and everyday compromises
Zimmerman writes after seven years flying an SR22, having spent his first thousand hours largely in Cessna singles. A real journey in the Cirrus convinced him that its popularity involved more than appearance. He values the comfortable passenger cabin, integrated avionics and relatively uncomplicated workload for its performance. The side control ceased to feel unusual after his first flight, and he enjoys both family trips and short solo outings in the aircraft.
His appreciation includes practical irritations. He dislikes the lack of nosewheel steering and rudder trim, finds the cabin noisy, and recalls climbs where engine temperatures required more attention than he wanted. Those are his operating impressions rather than a controlled comparison of every SR22 version. He also regards the parachute as useful equipment while explicitly saying he has never deployed it. For the kinds of journeys he regularly makes, the balance remains favourable: a capable travelling aircraft that is sufficiently straightforward for him to relax and enjoy flying.
Öffentliche Quellen 16
- Cirrus SR22Research background · Wikipedia revision 1374255854 · retrieved 2026-09-12
- Microsoft Flight Simulator aircraft manuals
- MSFS 2024 FAQ and edition aircraft inventory
- MSFS 2020 FAQ and edition aircraft inventory
- Cirrus SR 22 POH
- X-Plane 12 Desktop Manual
- X-Plane aircraft and avionics manuals
- SR22 G1000 version history
- SR22 product
- Reality Expansion Pack · Default XP12 Cirrus SR22Official developer / designated store catalogue · checked 2026-09-12
- SR22 / SR22TN EntegraOfficial developer / designated store catalogue · checked 2026-09-12
- SR22 / SR22TN G1000Official developer / designated store catalogue · checked 2026-09-12
- Learning to Fly in a Cirrus SR22Jessica Ambats · 1 November 2006
- Cirrus SR22 GTS: The Perfect Plane?Marc C. Lee · 24 April 2012
- The pros and the cons: Cirrus SR22John Zimmerman · 13 January 2025
- ICAO Doc 8643 — aircraft type designatorsPublic search data retrieved 2026-09-14; authority update 2026-09-03
Wie das Profil es modelliert
Carenado SR22 GTSx Turbo
Free + ProX-Plane 11Carenado
The SR22 entered production in 2001 as a more powerful development of Cirrus's SR20. A low wing, fixed tricycle gear and side-yoke controls define the basic layout. The Cirrus Airframe Parachute System is a prominent part of the aircraft's design.
This profile selects Carenado SR22 GTSx Turbo for X-Plane 11.
Spring resistance builds with the selected airspeed response. A separate aerodynamic term adds speed-dependent control load.
Valid trim provides the configured pressure relief. Autopilot following is off.
Controls and trim
Laminar's manual is titled SR22 but describes its simulated SR22T. It explains an electric motor and mechanical springs changing the side-control neutral instead of an elevator trim tab. The documented 50/100-percent flap settings and 150/110 KIAS limits belong to that aircraft. TorqueSim, REP and Carenado represent other engine and avionics configurations, so Laminar's assignments are not their qualified interfaces.
The selected implementation
Carenado SR22 GTSx Turbo XP11 uses Perspective G1000 based on the default unit, distinct from TorqueSim or REP systems.
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%
Die letzte Gesamtskalierung über alles, was das Modell erzeugt, vor der Gerätegrenze.
Mehr: alles (Feder, Lasten, Effekte) wird gemeinsam stärker.
Weniger: alles wird gemeinsam weicher.
Warum hier: Scales overall profile strength while preserving effect balance, subject to device and output limits.
Forces
Spring strength74%
Die Grundzentrierkraft, die den Stick zur Mitte zieht. Jede andere Kraft baut darauf auf. Zu niedrig fühlt sich der Stick im Normalflug schlaff an; zu hoch kämpft er gegen deine Hand und überdeckt die feineren Signale.
Mehr: festere Zentrierung, die der Hand jederzeit mehr widersteht.
Weniger: ein schlafferer Stick, der sich allein auf die aerodynamische Last stützt.
Warum hier: Mechanically connected side yokes motivate control loading; these controls are not passive Airbus-style sidesticks. The baseline spring is 0.74. Its low-speed blend reaches baseline strength at 80 KIAS.
Carenado SR22 GTSx Turbo for X-Plane 11SR22 control and trim cartridge handbook excerptsTorqueSim SR22 exact product / manualTorqueSim SR22 exact product / manualCirrus SR 22 POHSpring deadband4%
Eine kleine neutrale Zone um die Mitte, in der die Feder ruhig bleibt, damit kleinste Bewegungen im Stand nicht flattern. Breiter ist ruhiger, aber lockerer; enger ist präziser, kann aber um die Mitte zittern.
Mehr: eine ruhigere, aber lockerere Mitte mit mehr Spiel.
Weniger: eine straffere Mitte, die in Ruhe zittern kann.
Warum hier: Sets travel around the centre before the baseline spring resists. Smaller values engage it sooner.
Overall aerodynamic load80%
Ein Gesamtmaß über beide anhaltenden Achslasten, vor ihrer Einzelbalance angewendet. Profile lassen es normalerweise stehen und stimmen die beiden Achslasten ab.
Mehr: beide Achsen laden härter auf.
Weniger: beide Achsen werden gemeinsam leichter.
Warum hier: The aerodynamic-load gain is 0.8 with an indicated-speed reference of 160 KIAS. This supplies speed-dependent loading alongside the spring.
Airspeed blendingTrue
Aktiviert das Niedrigfahrt-Einblendfenster der Feder (Beginn/Voll in Knoten oben). Aus bleibt die Feder bei jeder Fahrt konstant.
Warum hier: Allows baseline spring strength to rise with indicated airspeed where the control law permits it.
Low-speed spring floor50%
Wie viel Feder im Stillstand übrig bleibt, bevor Fahrt überhaupt aerodynamische Kraft aufbauen kann. Ein hoher Sockel hält den geparkten Stick straff; ein niedriger ergibt das lose Seilzuggefühl eines geparkten Leichtflugzeugs.
Mehr: ein festerer Stick beim Parken und Rollen.
Weniger: ein schlaffer geparkter Stick, der erst mit Fahrt aufwacht.
Warum hier: Sets low-speed spring strength as a fraction of baseline when blending is enabled. One keeps full strength.
Spring engagement start22.4 kt
Die Fahrt, ab der die Feder vom Niedrigfahrt-Sockel Richtung volle Stärke steigt: der Beginn des "Lebendigwerdens" der Ruder im Startlauf.
Warum hier: Sets the IAS where the low-speed spring blend starts rising. This is a feel threshold, not a flight limit.
Spring engagement full80.0 kt
Die Fahrt, bei der die Feder volle Stärke erreicht. Zwischen Beginn und diesem Punkt strafft sich die Zentrierung zunehmend mit der Anströmung.
Warum hier: Sets the IAS where the low-speed blend reaches baseline strength; high-speed stiffening also uses it.
Geschwindigkeit zur Kraftabstimmung160
Die angezeigte Fahrt, bei der die aerodynamische Last ihr ausgelegtes Vollniveau erreicht. Sie verankert die gesamte Lastkurve am realen Geschwindigkeitsbereich: eine 172 lädt bis 110 Knoten auf, ein Jet viel später.
Mehr: Lasten kommen später; der Stick bleibt bis zu höherer Fahrt leicht.
Weniger: Lasten kommen früher, und die Reise fühlt sich schwerer an.
Warum hier: Sets the IAS reference for aerodynamic loading. It is an estimate, not published cruise TAS or a flight limit.
Centre firmness vs speed15%
Wie stark sich die Zentrierung selbst mit der Fahrt strafft, zusätzlich zu den Ausschlaglasten. Null hält das Mittengefühl konstant; mehr lässt den Stick im Reiseflug härter und im Anflug lockerer zentrieren.
Mehr: eine Mitte, die mit Fahrt spürbar härter wird.
Weniger: konstantes Mittengefühl bei jeder Fahrt.
Warum hier: The high-speed spring-stiffening gain is 0.15. It strengthens the permitted spring response above 80 KIAS, with the squared-speed ratio capped at 5.
Centre stiffening cap5
Die Obergrenze der fahrtabhängigen Mittenstraffung, damit sehr hohe Fahrt die Feder nicht grenzenlos aufzieht.
Mehr: mehr Gesamtstraffung bei hoher Fahrt erlaubt.
Weniger: die Straffung klemmt früher ab.
Warum hier: Limits the squared airspeed ratio used for high-speed spring stiffening; it is not a device-force cap.
Aileron load72%
Die anhaltende Rolllast aus Querruderausschlag und Fahrt, unabhängig vom Nick balanciert. Zusammen mit der Höhenruderlast bestimmt sie die Ruderharmonie, von der Testberichte sprechen.
Mehr: schwerere Rollkräfte.
Weniger: leichtere, quirligere Querruder.
Warum hier: Roll and pitch aerodynamic scales are 0.72 and 1, respectively. They set the aerodynamic axis balance. No custom spring-travel curve is enabled.
Elevator load100%
Die anhaltende Nicklast aus Höhenruderausschlag und Fahrt, unabhängig von der Rollachse balanciert. Der Haupthebel für das Nickgewicht eines Musters. Er verändert weder Querruder, Feder, Trimmung noch Schüttelkräfte.
Mehr: schwerere anhaltende Nickkräfte bei Fahrt.
Weniger: ein leichteres Höhenruder, das weniger Muskel braucht.
Warum hier: Scales pitch aerodynamic loading; pitch spring travel and trim responses are separate settings.
Max output force55%
Eine Kappe je stetiger Nick- oder Rollkraft vor dem Gerät. Der Schutz davor, die Hardware in harten Manövern zu überfahren oder zu sättigen.
Mehr: stärkere Spitzenkräfte vor dem Abschneiden.
Weniger: eine sanftere Decke; harte Manöver flachen früher ab.
Warum hier: Caps directed-force output. Native spring effects and device limits remain separate.
Trim
Trim relief (elevator)30%
Wie stark Höhenrudertrimmung die gehaltene Nickkraft abbaut und den Ruhepunkt des Sticks verschiebt. Bei 100 % braucht ein sauber getrimmtes Flugzeug keinen gehaltenen Druck: das Wegtrimmen der Last wie im echten Fliegen.
Mehr: Trimmung nimmt mehr der gehaltenen Nickkraft; bei 100 % nullt volle Trimmung sie.
Weniger: du hältst auch getrimmt weiter Kraft.
Warum hier: Electric spring-based trim changes neutral, providing mechanism context for pressure relief without deriving an exact hardware authority. Pitch authority 0.3 provides load relief and permitted centre movement; roll authority is 0.
Carenado SR22 GTSx Turbo for X-Plane 11SR22 control and trim cartridge handbook excerptsTorqueSim SR22 exact product / manualTorqueSim SR22 exact product / manualCirrus SR 22 POHTrim relief (aileron)0%
Dieselbe Entlastung für Rolltrimmung. Die meisten GA-Muster haben keine echte Querrudertrimmung, daher bleibt sie bei null; Muster mit Rolltrimmung bekommen einen passenden Wert.
Mehr: Rolltrimmung nimmt mehr gehaltene Rollkraft.
Weniger: Rolltrimmung bewirkt weniger.
Warum hier: Scales supported roll-trim relief and permitted centre movement. Zero removes roll response.
Effect gains · Ground
Runway rumble40%
Rollende Untergrundvibration aus Radgeschwindigkeit und Oberflächenart: die Textur von Asphalt, Gras oder Schotter unter dem Fahrwerk.
Mehr: lautere Oberflächentextur durch den Stick.
Weniger: ruhigeres Rollen.
Warum hier: Sets rolling texture strength, modified by speed, surface and undercarriage configuration.
Gear bumps25%
Kurze einzelne Stöße von Dehnfugen, Spurrillen und rauem Belag: die Interpunktion über dem kontinuierlichen Rumpeln.
Mehr: schärfere Stöße von Fugen und Rillen.
Weniger: weichere Bodendetails.
Warum hier: Sets gear-bump texture during ground motion, separate from touchdown impact.
Effect gains · Airframe
Stall buffet35%
Zellenschütteln vor dem Überziehen und bei aktiver Überziehwarnung: wie laut diese Fläche ihr Unbehagen ankündigt. Muster mit sauberem Abriss bekommen moderates Schütteln, das Horn trägt die Warnung.
Mehr: lauteres Schütteln vor dem Überziehen.
Weniger: eine leisere Fläche; das Horn trägt die Warnung.
Warum hier: Sets stall-buffet strength. Zero removes the cue without changing simulator stalls or warnings.
Mach buffet0%
Transsonisches Schütteln nahe der Machgrenze. Relevant für Jets nahe MMO, null für Kolben und Turboprops, die nie dort ankommen.
Mehr: stärkeres transsonisches Schütteln nahe der Machgrenze.
Weniger: ruhigerer Flug bei hohem Mach.
Warum hier: Sets high-Mach buffet strength; onset and full-strength thresholds are separate.
Flap buffet14%
Niederfrequente Zellenvibration mit Klappen im Fahrtwind, im Fenster, in dem sie wirklich Luft arbeiten.
Mehr: ein rauerer Lauf mit arbeitenden Klappen.
Weniger: ruhigere Anflugklappen.
Warum hier: Sets flap buffet at the configured position and speed gates. Flap movement texture is separate.
Gear buffet0%
Zellentrommeln vom ausgefahrenen Einziehfahrwerk im Fahrtwind. Null für Festfahrwerke, deren Zelle nie die Form ändert.
Mehr: mehr Trommeln mit hängendem Fahrwerk.
Weniger: saubererer Flug mit Fahrwerk.
Warum hier: Sets gear aerodynamic buffet; movement and ground-contact cues are separate.
Stick shaker50%
Der dedizierte Stall-Stickshaker-Buzz, ausgelöst von der Überziehwarnanlage des Flugzeugs. Nur Muster mit echtem Shaker bekommen einen Wert; alle anderen verlassen sich auf Schütteln und Horn.
Mehr: ein härterer Shaker-Buzz.
Weniger: ein dezenterer Shaker.
Warum hier: Sets triggered shaker strength; inactive while the shaker feature is disabled.
Effect gains · Engine, mechanical & drag
Touchdown thump65%
Der Einmalstoß beim Aufsetzen, skaliert mit der Sinkrate: ein Butterlander flüstert, ein fester Aufsetzer wummst.
Mehr: ein härterer Tritt beim Aufsetzen.
Weniger: weichere Ankünfte.
Warum hier: Sets landing-impact strength; landing telemetry and response shape determine the pulse.
Reverse rumble0%
Ausrollvibration bei Schubumkehr oder Beta-Verstellung. Null für Muster ohne Umkehr.
Mehr: ein rauerer Ausrollvorgang unter Umkehrschub.
Weniger: leisere Umkehr.
Warum hier: Sets reverse-thrust vibration with valid reverser and engine conditions. Zero removes the cue.
Engine rumble12%
Kontinuierliche Triebwerksvibration, die der Drehzahl von Leerlauf bis Volllast folgt: die allgegenwärtige Erinnerung, dass vorn etwas Kraftstoff verbrennt.
Mehr: mehr Triebwerk im Stick.
Weniger: ein leiseres Triebwerk.
Warum hier: Sets estimated engine vibration using configured telemetry and response, not measured cockpit vibration.
Flap motion12%
Dauervibration nur, solange der Simulator tatsächlich fahrende Klappenflächen meldet. Folgt echter Aktuatorbewegung und Ausfällen, keinem geschätzten Timer.
Mehr: mehr Vibration bei fahrenden Klappen.
Weniger: leisere Klappenläufe.
Warum hier: Sets texture from observed flap movement; a command without movement does not establish the cue.
Autopilot follow
AP follow authority10%
Wie weit Autopilotbefehle den physischen Stick bewegen dürfen. In MSFS winzig gehalten, weil eine bewegte Achse als Pilotene ingabe zurückgelesen werden kann; null schaltet das Folgen ab.
Mehr: der Autopilot bewegt deinen Stick sichtbar weiter.
Weniger: ein kaum wahrnehmbares Folgen.
Warum hier: Sets admitted AP-follow gain, not a percentage of travel. Runtime ownership and input limits still apply.
Stick feel
StickFeel · Trim feel enabledTrue
Whether this feature is active in this profile.
Warum hier: Retained for compatibility and group membership. Trim relief, rather than this flag, controls centre movement.
StickFeel · Trim relief enabledTrue
Whether this feature is active in this profile.
Warum 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.
Warum hier: Enables local force trim, separate from aircraft-owned trim and add-on integration qualification.
StickFeel · G load enabledTrue
Whether this feature is active in this profile.
Warum hier: Allows load-factor changes to modify permitted spring laws. Passive fly-by-wire feel can suppress it.
StickFeel · Rate damping enabledTrue
Whether this feature is active in this profile.
Warum hier: Enables rate damping with the configured coefficients and control law.
Autopilot
Autopilot · Follow enabledFalse
Whether this feature is active in this profile.
Warum hier: Autopilot following is off; the configured spring and load retain the hardware feel.
Autopilot · Neutral hold enabledFalse
Whether this feature is active in this profile.
Warum hier: Permits centering hold during a supported AP state, separate from following a moving target.
Autopilot · Neutral hold strength0.6
Warum hier: Sets admitted AP neutral-hold strength; inactive while neutral hold is disabled.
Aero
Aero · EnabledTrue
Whether this feature is active in this profile.
Warum hier: Enables aerodynamic cues; each still needs nonzero strength and its simulator conditions.
Aero · Max flap index2
Where this effect reaches full strength (or has fully faded, for washouts).
Mehr: a more gradual build to a later peak.
Weniger: a quicker build.
Warum 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.
Mehr: the effect begins later.
Weniger: it begins earlier.
Warum 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.
Warum hier: Permits shaker at supported warning conditions; the switch does not establish aircraft equipment.
Ground
Ground · EnabledTrue
Whether this feature is active in this profile.
Warum hier: Enables ground effects; each still needs its own strength and contact or motion telemetry.
Engine
Engine · EnabledTrue
Whether this feature is active in this profile.
Warum hier: Enables engine cues with nonzero settings and valid running-engine telemetry.
Mechanical
Mechanical · EnabledTrue
Whether this feature is active in this profile.
Warum hier: Enables accessory cues with configured strengths and observed accessory movement.
Mechanical · Gain0
The strength of this effect.
Mehr: a stronger effect.
Weniger: a weaker one.
Warum hier: Sets texture from observed gear movement, separate from aerodynamic and touchdown effects.
Alle Profileinstellungen
| Parameter | Wert | Was es steuert und warum |
|---|---|---|
| Spring strength | 0.74 | Mechanically connected side yokes motivate control loading; these controls are not passive Airbus-style sidesticks. The baseline spring is 0.74. Its low-speed blend reaches baseline strength at 80 KIAS. |
| Spring deadband | 0.045 | Sets travel around the centre before the baseline spring resists. Smaller values engage it sooner. |
| Force gain | 0.8 | The aerodynamic-load gain is 0.8 with an indicated-speed reference of 160 KIAS. This supplies speed-dependent loading alongside the spring. |
| Master gain | 0.85 | Scales overall profile strength while preserving effect balance, subject to device and output limits. |
| Dynamic-pressure blend | True | 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 | 22.4 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 | 80.0 kt | Sets the IAS where the low-speed blend reaches baseline strength; high-speed stiffening also uses it. |
| Geschwindigkeit zur Kraftabstimmung | 160.0 kt | Sets the IAS reference for aerodynamic loading. It is an estimate, not published cruise TAS or a flight limit. |
| Airspeed spring stiffening | 0.15 | The high-speed spring-stiffening gain is 0.15. It strengthens the permitted spring response above 80 KIAS, with the squared-speed ratio capped at 5. |
| 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 | 0.72 | Roll and pitch aerodynamic scales are 0.72 and 1, respectively. They set the aerodynamic axis balance. No custom spring-travel curve is enabled. |
| Elevator force scale | 1.0 | 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. |
| StickFeel · Trim feel enabled | True | Retained for compatibility and group membership. Trim relief, rather than this flag, controls centre movement. |
| StickFeel · Trim relief enabled | True | Allows trim relief with supported control law and valid telemetry. Axis authorities set its amount. |
| StickFeel · Elevator authority | 0.3 | Electric spring-based trim changes neutral, providing mechanism context for pressure relief without deriving an exact hardware authority. Pitch authority 0.3 provides load relief and permitted centre movement; 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 | True | Allows load-factor changes to modify permitted spring laws. Passive fly-by-wire feel can suppress it. |
| StickFeel · Rate damping enabled | True | 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. |
| Autopilot · Follow authority | 0.1 | Sets admitted AP-follow gain, not a percentage of travel. Runtime ownership and input limits still apply. |
| Autopilot · Neutral hold enabled | False | Permits centering hold during a supported AP state, separate from following a moving target. |
| Autopilot · Neutral hold strength | 0.6 | 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 | 0.35 | Sets stall-buffet strength. Zero removes the cue without changing simulator stalls or warnings. |
| Aero · Gain | 0 | Sets high-Mach buffet strength; onset and full-strength thresholds are separate. |
| Aero · Gain | 0.14 | Sets flap buffet at the configured position and speed gates. Flap movement texture is separate. |
| Aero · Max flap index | 2 | 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 | True | Enables ground effects; each still needs its own strength and contact or motion telemetry. |
| Ground · Gain | 0.4 | Sets rolling texture strength, modified by speed, surface and undercarriage configuration. |
| Ground · Gain | 0.25 | Sets gear-bump texture during ground motion, separate from touchdown impact. |
| Ground · Gain | 0.65 | 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 | True | Enables engine cues with nonzero settings and valid running-engine telemetry. |
| Engine · Gain | 0.12 | 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 | 0.12 | 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. |
Öffentliche Quellen 18
- Cirrus SR22Research background · Wikipedia revision 1374255854 · retrieved 2026-09-12
- Carenado SR22 GTSx Turbo for X-Plane 11Cirrus SR22
- SR22 control and trim cartridge handbook excerptsCirrus POH/AMM via NTSB, scanned PDF1-4,7,10,12 ; Cirrus original POH/AMM archived through NTSB; prior visual review
- TorqueSim SR22 exact product / manualSR22G3 and SR22TNG3 product, XP12 supportOfficial developer / designated store catalogue · checked 2026-09-12
- TorqueSim SR22 exact product / manualSR22 EntegraR8 product and available purchaseOfficial developer / designated store catalogue · checked 2026-09-12
- Cirrus SR 22 POHCirrus SR22
- Microsoft Flight Simulator aircraft manuals
- MSFS 2024 FAQ and edition aircraft inventory
- MSFS 2020 FAQ and edition aircraft inventory
- X-Plane 12 Desktop Manual
- X-Plane aircraft and avionics manuals
- SR22 G1000 version history
- SR22 product
- Reality Expansion Pack · Default XP12 Cirrus SR22Official developer / designated store catalogue · checked 2026-09-12
- Learning to Fly in a Cirrus SR22Jessica Ambats · 1 November 2006
- Cirrus SR22 GTS: The Perfect Plane?Marc C. Lee · 24 April 2012
- The pros and the cons: Cirrus SR22John Zimmerman · 13 January 2025
- ICAO Doc 8643 — aircraft type designatorsPublic search data retrieved 2026-09-14; authority update 2026-09-03
Community & Korrekturen
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Pilotenkorrekturen
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Hangargespräche
Offene Unterhaltung über das Fliegen und Tunen der Cirrus SR22, im Community-Forum. Korrekturen oben gehen privat an den Maintainer; Hangargespräche sind öffentlich.
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Community
Community-Profile für dieses Luftfahrzeug
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