Development milestones
First flight: February 29, 1960
Developed from: Beechcraft Travel Air
FlugzeugbibliothekBeechcraft Baron 58 / G58
Matti Blume · CC BY-SA 4.0 · Beechcraft Baron.Beechcraft Baron 58 / G58
A low-wing piston twin that carries the Beechcraft touring-aircraft lineage into two-engine flying.
General aviation15 Profiloptionen
Kenne das Flugzeug
The Baron entered the Beechcraft range in 1961, developing from the earlier Travel Air. Its retractable landing gear and two wing-mounted piston engines provide the familiar outline of a light touring twin. Several fuselage and engine combinations appeared over the family's long history.
The Model 58 and glass-cockpit G58 share a recognisable shape while representing different equipment generations. The simulator products span conventional-instrument aircraft and modern G58s, with avionics and systems described for each.
Beechcraft Baron · Specifications (B55) · real aircraft; source units retained
- Length
- 28 ft 0 in (8.53 m)↗
- Wingspan
- 37 ft 10 in (11.53 m)↗
- Height
- 9 ft 7 in (2.92 m)↗
- Wing area
- 199.2 sq ft (18.51 m² )↗
- Empty weight
- 3,156 lb (1,432 kg)↗
- Max takeoff weight
- 5,100 lb (2,313 kg)↗
- Powerplant
- 2 × Continental IO-470-L air-cooled six-cylinder horizontally opposed engines, 260 hp (190 kW) each↗
- Maximum speed
- 205 kn (236 mph, 380 km/h) at sea level↗
- Cruise speed
- 180 kn (210 mph, 330 km/h) at 12,000 ft (3,700 m) (55% power)↗
- Stall speed
- 73 kn (84 mph, 135 km/h) IAS , power off, wheels and flaps lowered↗
Mehr über dieses Flugzeug auf AirframeDB
Smooth airwork in a fast, well-equipped twin
Twombly's G58 demonstration began near sea level and close to maximum weight, yet the initial climb reached about 1,800 feet per minute. At 11,000 feet, he recorded roughly 200 knots true airspeed before exploring reduced fuel-flow settings. The pace reinforced his view that a Baron transition deserves substantial preparation. Once settled into airwork, however, he particularly enjoyed the smooth response during steep turns and the familiar Beechcraft cockpit around the modern Garmin displays.
The evaluation also included flight on one engine. In the cold conditions of that particular demonstration, he reported a continuing climb at 11,000 feet, with rudder and aileron trim helping reduce the workload. That observation should not be read as performance available at every temperature or loading. Returning to land required firm back pressure, followed by the satisfying touchdown he associated with the type. His report combines enthusiasm for the handling with a clear sense of how quickly a powerful twin can keep its pilot occupied.
A contractor puts an early glass-cockpit Baron to work
Hill had operated one of the first Garmin-equipped G58s for nearly five months when Cox interviewed him. His construction business took him around Arizona, Nevada and California several times a week, usually with bankers, investors or employees aboard. Moving from a Bonanza made the cabin and panel layout familiar, while the twin's rear double doors proved popular with his passengers. He expected to fly about 500 hours annually if that early pattern continued.
He praised the climb and tightly coordinated controls, saying the aircraft's weight was less apparent in flight than he had expected. Learning the G1000 brought a clearer picture of his position in instrument conditions. His equipment choices reflected the work: relatively short trips and infrequent use of every seat allowed him to choose the smaller standard fuel capacity and preserve payload. For Hill, the appeal was how well the Baron fitted recurring business journeys, with enough speed and accommodation to meet the needs he actually had.
Eight years sharing a Baron for travel and relief flights
Lincoln had shared his 1984 Baron 58 with a partner for eight years when Courtney spoke with him. Their flying included journeys from Connecticut along the American East Coast, trips through the Bahamas and humanitarian work connected with Haiti's 2010 earthquake. He remembered feeling comfortable in the aeroplane from the first flight. The yoke felt substantial, but the response was precise, giving him a strong sense of connection with the aircraft.
He was preparing to sell because his own flying needs had changed and he expected fewer long journeys. That decision did not diminish his affection for the Baron. He regarded it as especially attractive when carrying a small number of passengers and valuing performance over maximum accommodation. He cautioned against treating every nominal seat as equally spacious, suggesting a larger aircraft for a larger family.
Öffentliche Quellen 17
- Beechcraft BaronResearch background · Wikipedia revision 1370279143 · retrieved 2026-09-12
- Microsoft Flight Simulator aircraft manuals
- MSFS 2024 FAQ and edition aircraft inventory
- MSFS 2020 FAQ and edition aircraft inventory
- Beechcraft Baron 58 POH
- X-Plane 12 Desktop Manual
- X-Plane aircraft and avionics manuals
- X-Plane 11 Desktop Manual
- Baron ProfessionalOfficial developer / designated store catalogue · checked 2026-09-12
- Steam Gauge Overhaul - Analog BaronOfficial developer / designated store catalogue · checked 2026-09-12
- Reality Expansion Pack · default Baron B58Official developer / designated store catalogue · checked 2026-09-12
- Hawker-Beechcraft G58 Baron: Noble SteedIan J. Twombly · 1 February 2009
- The Baron of GlassJim Hill, interviewed by Bill Cox · 1 July 2006
- The Beechcraft 58 Baron: Crown Royalty of the Light-Twin WorldTom Lincoln, interviewed by Carly Courtney · 27 March 2017
- Reality Expansion Pack for Carenado B58 Baron-Simcoders-REP-Official developer / designated-store reference · checked 2026-09-14
- ICAO Doc 8643 — aircraft type designatorsPublic search data retrieved 2026-09-14; authority update 2026-09-03
- Beechcraft B58 Enhanced Flight ModelsProduct listing captured 2026-09-24; edition scope from the reviewed catalogue
Wie das Profil es modelliert
Beechcraft Baron 58
Free + ProMSFS 2020MSFS 2024X-Plane 11X-Plane 12
The Baron entered the Beechcraft range in 1961, developing from the earlier Travel Air. Its retractable landing gear and two wing-mounted piston engines provide the familiar outline of a light touring twin. Several fuselage and engine combinations appeared over the family's long history.
This starting point selects Beechcraft Baron 58. Its aircraft-level settings do not select a particular developer’s custom systems.
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 enabled for supported control references.
Controls and trim
Baron products distinguish normally aspirated B58 aircraft, turbocharged B58TCs and pressurized B58Ps. Black Square documents three-axis trim and separate KFC150 autopilot and flight-director cancellation. Carenado's B58 uses its own KFC225 implementation. Engine boost and cabin pressure distinguish equipment and performance; they do not by themselves prescribe a different yoke force.
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: The piston twin's selected aerodynamic yoke loading is independent of whether its engines are normally aspirated or turbocharged and its cabin is pressurized. The baseline spring is 0.74. Its low-speed blend reaches baseline strength at 82.5 KIAS.
Analog Baron manualOperating ManualCarenado B58 Baron for X-Plane 11Spring 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 165 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 start20 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 full82.5 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 Kraftabstimmung165
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 82.5 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: Documented elevator trim supports pitch relief. Aileron and rudder trim serve separate axes, and a trim-tab animation is not a hardware-neutral calibration. Pitch authority 0.3 provides load relief and permitted centre movement; roll authority is 0.
Analog Baron manualOperating ManualCarenado B58 Baron for X-Plane 11Trim 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 buffet10%
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 enabledTrue
Whether this feature is active in this profile.
Warum hier: Following is on at 0.1 authority when a supported, valid autopilot control reference is available.
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 · Gain0.12
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 | The piston twin's selected aerodynamic yoke loading is independent of whether its engines are normally aspirated or turbocharged and its cabin is pressurized. The baseline spring is 0.74. Its low-speed blend reaches baseline strength at 82.5 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 165 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 | 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 | 82.5 kt | Sets the IAS where the low-speed blend reaches baseline strength; high-speed stiffening also uses it. |
| Geschwindigkeit zur Kraftabstimmung | 165.0 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 82.5 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 | Documented elevator trim supports pitch relief. Aileron and rudder trim serve separate axes, and a trim-tab animation is not a hardware-neutral calibration. 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 | True | Following is on at 0.1 authority when a supported, valid autopilot control reference is available. |
| 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 | 0.1 | 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 | 0.12 | Sets texture from observed gear movement, separate from aerodynamic and touchdown effects. |
Öffentliche Quellen 20
- Beechcraft BaronResearch background · Wikipedia revision 1370279143 · retrieved 2026-09-12
- Analog Baron manualBeechcraft Baron 58 / G58
- Operating ManualBaron Professional manual introduction, KFC150 pp.41-42, hardware section and change log
- Carenado B58 Baron for X-Plane 11Beechcraft Baron 58 / G58
- Microsoft Flight Simulator aircraft manuals
- MSFS 2024 FAQ and edition aircraft inventory
- MSFS 2020 FAQ and edition aircraft inventory
- Beechcraft Baron 58 POH
- X-Plane 12 Desktop Manual
- X-Plane aircraft and avionics manuals
- X-Plane 11 Desktop Manual
- Baron ProfessionalOfficial developer / designated store catalogue · checked 2026-09-12
- Steam Gauge Overhaul - Analog BaronOfficial developer / designated store catalogue · checked 2026-09-12
- Reality Expansion Pack · default Baron B58Official developer / designated store catalogue · checked 2026-09-12
- Hawker-Beechcraft G58 Baron: Noble SteedIan J. Twombly · 1 February 2009
- The Baron of GlassJim Hill, interviewed by Bill Cox · 1 July 2006
- The Beechcraft 58 Baron: Crown Royalty of the Light-Twin WorldTom Lincoln, interviewed by Carly Courtney · 27 March 2017
- Reality Expansion Pack for Carenado B58 Baron-Simcoders-REP-Official developer / designated-store reference · checked 2026-09-14
- ICAO Doc 8643 — aircraft type designatorsPublic search data retrieved 2026-09-14; authority update 2026-09-03
- Beechcraft B58 Enhanced Flight ModelsProduct listing captured 2026-09-24; edition scope from the reviewed catalogue
Community & Korrekturen
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Pilotenkorrekturen
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Hangargespräche
Offene Unterhaltung über das Fliegen und Tunen der Beechcraft Baron 58 / G58, im Community-Forum. Korrekturen oben gehen privat an den Maintainer; Hangargespräche sind öffentlich.
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Community
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