Biblioteca de aeronavesMX Aircraft MXS-R
MX Aircraft MXS-RZLEA · CC BY-SA 4.0 · MX Aircraft MXS-RH (NX530RH, cn MXS-001) (11-9-2024).

MX Aircraft MXS-R

The air-racing development of the carbon-fibre MXS aerobatic monoplane.
Aerobatic1 opções de perfil

Conheça o avião

The single-seat MXS uses a carbon-fibre structure, low wing and compact fuselage for competition aerobatics. The MXS-R developed the aircraft for air racing, with equipment and configuration specific to that role. The simulator represents the racing version.

Aircraft / family

Propulsion
Single piston↗
Configuration
Composite · Aerobatics / racing↗

MX Aircraft MXS · Specifications · real aircraft; source units retained

Length
6.51 m (21.35 ft)↗
Wingspan
7.3 m (24 ft)↗
Height
1.8 m (6 ft)↗
Empty weight
572 kg (1,260 lb)↗
Gross weight
726 kg (1,600 lb)↗
Max takeoff weight
835 kg (1,840 lb)↗
Powerplant
1 × Lycoming AEIO-540EXP MT Propeller MTV9 203 20D blades, 190–280 kW (250–380 hp) Hartzell 3 blade "Claw" counterweighted propeller↗
Maximum speed
426 km/h (265 mph, 230 kn)↗
Cruise speed
330 km/h (210 mph, 180 kn)↗
Stall speed
107 km/h (67 mph, 58 kn)↗

Mais sobre esta aeronave no AirframeDB

From the MX2 to a single-seat competition aircraft

MX Aircraft describes the MXS as a close relative of its two-seat MX2, refocused on agility and unlimited aerobatics. The single-seat carbon-fibre airframe and tailored controls reflect that competition purpose. The family also underlies specialised race and display aircraft, but the manufacturer offers a range of engine and equipment choices. A specification for a standard MXS or a particular race aircraft therefore needs that scope when reading about the simulated MXS-R.

Experience is supported by preparation away from the cockpit

Asked about his age before the Gdynia race, Lamb described experience as something that helped him feel comfortable in the demanding world of pylon racing. He was pleased with the season’s progress, including his Malaysian win, while his team continued working to make the MXS-R faster.

His preparation extended beyond the aircraft. Squash supplied a competitive workout that exercised his reactions, while yoga, Pilates and strength work contributed to his fitness. The interview presents confidence as something maintained through that combination of flying, physical preparation and team effort. Lamb did not regard age itself as an obstacle, but his answer still gave considerable weight to the work required to stay ready for competition.

Returning to the racer means regaining its particular feel

Hall felt comfortable with the physical demands of racing, but that confidence had exposed a different weakness. Back in Australia he flew several other aircraft, and returning to the MXS-R required time to recover its particular feel. Familiarity with flying in general was not giving him the precision he wanted in this aeroplane.

Before the Dallas–Fort Worth race, he planned more practice to rebuild that connection with the controls. He also changed his travel arrangements, flying directly from Britain rather than returning to Australia first. Arriving awake and alert made the coming week feel more promising.

A newcomer reaches the start gate with a mentor behind him

Brageot entered the Master Class with more than an aircraft inherited from Nigel Lamb. A mentoring programme had brought him inside the team, where he learned what each person contributed and practised the MXS on the racecourse. Lamb remained available afterwards, offering advice by telephone and message as his successor began competing.

That preparation did not make the first season effortless. A technical problem at San Diego cost Brageot training and qualifying time, leaving an awkward start to race day. He described solving the problem as part of building experience together. Mental preparation mattered too: a deliberate routine helped him arrive at the start gate ready to concentrate on flying rather than everything happening around the race.

Fontes públicas 8
  1. MX Aircraft MXSResearch background · Wikipedia revision 1325253314 · retrieved 2026-09-12
  2. Microsoft Flight Simulator aircraft manuals
  3. MSFS 2024 FAQ and edition aircraft inventory
  4. Nigel Lamb: nie postrzegam swojego wieku jako przeszkodyPilot interview · 21 July 2014
  5. More training the key for DFW: HallMatt Hall · 4 September 2014
  6. Interview with aerobatic extraordinaire and air race pilot Mika BrageotTelephone interview · 11 July 2017
  7. ICAO Doc 8643 — aircraft type designatorsPublic search data retrieved 2026-09-14; authority update 2026-09-03
  8. MXS development and constructionMX Aircraft account of the MXS development and configurable equipment.

Como o perfil o modela

MX Aircraft MXS-R

Free + Pro
MSFS 2024

The single-seat MXS uses a carbon-fibre structure, low wing and compact fuselage for competition aerobatics. The MXS-R developed the aircraft for air racing, with equipment and configuration specific to that role. The simulator represents the racing version.

This starting point selects MX Aircraft MXS-R. Its aircraft-level settings do not select a particular developer’s custom systems.

The selected response supplies the racer’s pitch/roll balance. Spring resistance builds with the selected airspeed response. A separate aerodynamic term adds speed-dependent control load.

Pitch trim relief accompanies the named racing configuration. Valid trim provides the configured pressure relief. Autopilot following is off.

Controls and trim

The MXS-R is the racing development of a single-seat composite aerobatic aircraft. Its compact fuselage, low wing and piston power serve that competition role. The race fit retains its own equipment rather than being only a livery.

MX Aircraft Examination Report

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%

A escala final de saída aplicada a tudo que o modelo produz, antes do teto do dispositivo.

Mais: tudo (mola, cargas, efeitos) fica mais forte junto.

Menos: tudo amacia junto.

Por que aqui: Scales overall profile strength while preserving effect balance, subject to device and output limits.

Forces

Spring strength74%

A força base de centragem que puxa o manche de volta ao centro. Todas as outras forças se empilham sobre ela. Baixa demais e o manche parece frouxo em voo normal; alta demais e ele briga com sua mão e mascara os sinais menores por cima.

Mais: uma centragem mais firme que resiste mais à mão.

Menos: um manche mais mole que depende só da carga aerodinâmica.

Por que aqui: The selected response supplies the racer’s pitch/roll balance. The baseline spring is 0.74. Its low-speed blend reaches baseline strength at 85 KIAS.

MX Aircraft Examination Report
Spring deadband3%

Uma pequena zona neutra ao redor do centro onde a mola fica quieta, para que movimentos mínimos em repouso não trepidem. Mais larga é mais calma porém mais solta; mais estreita é mais precisa mas pode tremer no centro.

Mais: um centro mais calmo porém mais solto, com mais folga.

Menos: um centro mais apertado que pode tremer em repouso.

Por que aqui: Sets travel around the centre before the baseline spring resists. Smaller values engage it sooner.

Overall aerodynamic load40%

Uma escala mestra sobre as duas cargas sustentadas de eixo, aplicada antes do balanço independente delas. Os perfis normalmente a deixam quieta e ajustam as duas cargas de eixo.

Mais: os dois eixos carregam mais forte.

Menos: os dois eixos aliviam juntos.

Por que aqui: The aerodynamic-load gain is 0.4 with an indicated-speed reference of 170 KIAS. This supplies speed-dependent loading alongside the spring.

Airspeed blendingTrue

Ativa a janela de engate da mola em baixa velocidade (nós de início/pleno acima). Desligado, a mola é constante em todas as velocidades.

Por que aqui: Allows baseline spring strength to rise with indicated airspeed where the control law permits it.

Low-speed spring floor50%

Quanto da mola sobrevive parado, antes que a velocidade possa gerar força aerodinâmica. Um piso alto mantém o manche estacionado firme; um piso baixo dá a sensação solta, de cabos com folga, de um avião leve estacionado.

Mais: um manche mais firme estacionado e no táxi.

Menos: um manche mole estacionado que só desperta com velocidade.

Por que aqui: Sets low-speed spring strength as a fraction of baseline when blending is enabled. One keeps full strength.

Spring engagement start20 kt

A velocidade em que a mola começa a subir do piso de baixa velocidade rumo à força plena: os comandos "ganhando vida" na corrida de decolagem.

Por que aqui: Sets the IAS where the low-speed spring blend starts rising. This is a feel threshold, not a flight limit.

Spring engagement full85.0 kt

A velocidade em que a mola atinge força plena. Entre o início e este ponto, a centragem endurece progressivamente à medida que o fluxo de ar cresce sobre os comandos.

Por que aqui: Sets the IAS where the low-speed blend reaches baseline strength; high-speed stiffening also uses it.

Velocidade de ajuste de força170

A velocidade indicada em que a carga aerodinâmica atinge seu nível pleno de projeto. Ela ancora toda a curva de carga à faixa real de velocidades do avião: um 172 carrega por volta de 110 nós, um jato bem depois.

Mais: as cargas chegam mais tarde; o manche fica leve até mais velocidade.

Menos: as cargas chegam antes e o cruzeiro pesa mais.

Por que aqui: Sets the IAS reference for aerodynamic loading. It is an estimate, not published cruise TAS or a flight limit.

Centre firmness vs speed0%

Quanto a própria centragem endurece com a velocidade, além das cargas de deflexão. Zero mantém a sensação de centro constante; mais faz o manche centrar mais duro em cruzeiro e mais solto no circuito.

Mais: um centro que endurece nitidamente com a velocidade.

Menos: uma sensação de centro constante em qualquer velocidade.

Por que aqui: The high-speed spring-stiffening gain is 0. No additional speed-driven stiffening is added; this does not disable independent aerodynamic loading.

Centre stiffening cap5

O limite superior do endurecimento de centro pela velocidade, para que voos muito rápidos não tensionem a mola sem freio.

Mais: mais endurecimento total permitido em alta velocidade.

Menos: o endurecimento corta antes.

Por que aqui: Limits the squared airspeed ratio used for high-speed spring stiffening; it is not a device-force cap.

Aileron load72%

A carga sustentada de rolagem da deflexão dos ailerons e da velocidade, balanceada independentemente da arfagem. Junto com a carga do profundor define a razão de harmonia de comandos de que falam as resenhas.

Mais: esforços de rolagem mais pesados.

Menos: ailerons mais leves e vivos.

Por que aqui: 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%

A carga sustentada de arfagem da deflexão do profundor e da velocidade, balanceada independentemente da rolagem. É a alavanca principal por trás do peso de arfagem de um tipo. Não toca aileron, mola, compensador nem forças de buffet.

Mais: esforços sustentados de arfagem mais pesados em velocidade.

Menos: um profundor mais leve, com menos músculo para segurar.

Por que aqui: Scales pitch aerodynamic loading; pitch spring travel and trim responses are separate settings.

Max output force55%

Um teto sobre cada força estável de arfagem ou rolagem antes de chegar ao dispositivo, protegendo contra pancadas ou saturação do hardware em manobras fortes.

Mais: picos de força estável mais altos antes do corte.

Menos: um teto mais suave; manobras duras achatam antes.

Por que aqui: Caps directed-force output. Native spring effects and device limits remain separate.

Trim

Trim relief (elevator)30%

Com que força o compensador de profundor alivia o esforço de arfagem mantido e desloca onde o manche assenta. Em 100 %, um avião bem compensado não precisa de pressão mantida: o fluxo de trabalho de compensar-a-carga do voo real.

Mais: o compensador tira mais esforço mantido; em 100 %, todo compensado o anula.

Menos: você segue segurando esforço mesmo compensado.

Por que aqui: Pitch trim relief accompanies the named racing configuration. Pitch authority 0.3 provides load relief and permitted centre movement; roll authority is 0.

MX Aircraft Examination Report
Trim relief (aileron)0%

O mesmo alívio para o compensador de rolagem. A maioria dos tipos de aviação geral não tem compensador de aileron real, então isto fica em zero; tipos com compensador de rolagem recebem um valor correspondente.

Mais: o compensador de rolagem tira mais esforço mantido.

Menos: o compensador de rolagem faz menos.

Por que aqui: Scales supported roll-trim relief and permitted centre movement. Zero removes roll response.

Effect gains · Ground

Runway rumble40%

Vibração de rolagem no solo pela velocidade das rodas e tipo de superfície: asfalto, grama ou cascalho sob o trem.

Mais: uma textura de superfície mais forte no manche.

Menos: um táxi mais liso.

Por que aqui: Sets rolling texture strength, modified by speed, surface and undercarriage configuration.

Gear bumps30%

Solavancos curtos e discretos de juntas de dilatação, sulcos e superfície irregular, pontuando o ronco contínuo.

Mais: solavancos mais nítidos de juntas e sulcos.

Menos: detalhes de solo mais suaves.

Por que aqui: Sets gear-bump texture during ground motion, separate from touchdown impact.

Effect gains · Airframe

Stall buffet30%

Sacudida da célula ao se aproximar do estol e enquanto o aviso soa: quão alto esta asa anuncia que está infeliz. Tipos de quebra seca recebem buffet modesto e deixam a buzina levar o aviso.

Mais: um tremor pré-estol mais forte.

Menos: uma asa mais discreta; a buzina leva o aviso.

Por que aqui: Sets stall-buffet strength. Zero removes the cue without changing simulator stalls or warnings.

Mach buffet0%

Buffet transônico ao se aproximar do limite de Mach. Significativo para jatos perto de MMO, zero para pistões e turboélices que nunca chegam lá.

Mais: um buffet transônico mais forte perto do limite de Mach.

Menos: um voo mais liso em Mach alto.

Por que aqui: Sets high-Mach buffet strength; onset and full-strength thresholds are separate.

Flap buffet0%

Vibração de baixa frequência da célula com flapes estendidos no fluxo, na janela de velocidade em que eles realmente trabalham o ar.

Mais: um voo mais áspero com flapes trabalhando.

Menos: flapes de aproximação mais suaves.

Por que aqui: Sets flap buffet at the configured position and speed gates. Flap movement texture is separate.

Gear buffet0%

Tamborilar da célula pelo trem retrátil pendurado na corrente de ar. Zero para tipos de trem fixo, onde a célula nunca muda de forma.

Mais: mais tamborilar com o trem embaixo.

Menos: um voo com trem embaixo mais limpo.

Por que aqui: Sets gear aerodynamic buffet; movement and ground-contact cues are separate.

Stick shaker50%

O zumbido dedicado do stick shaker de estol, disparado pelo próprio sistema de aviso do avião. Só tipos com shaker real recebem valor; o resto confia no buffet aerodinâmico e na buzina.

Mais: um shaker mais duro.

Menos: um shaker mais discreto.

Por que aqui: Sets triggered shaker strength; inactive while the shaker feature is disabled.

Effect gains · Engine, mechanical & drag

Touchdown thump60%

O golpe único quando as rodas tocam a pista, escalado pela razão de descida: um pouso macio sussurra, uma chegada firme bate.

Mais: um golpe mais duro no toque.

Menos: chegadas mais suaves.

Por que aqui: Sets landing-impact strength; landing telemetry and response shape determine the pulse.

Reverse rumble0%

Vibração na corrida enquanto o reverso ou as hélices em beta trabalham. Zero para tipos sem reverso.

Mais: uma corrida mais áspera sob reverso.

Menos: um reverso mais discreto.

Por que aqui: Sets reverse-thrust vibration with valid reverser and engine conditions. Zero removes the cue.

Engine rumble12%

Vibração contínua do grupo motopropulsor seguindo a rotação entre marcha lenta e potência máxima, o lembrete sempre presente de que algo queima combustível lá na frente.

Mais: mais motor no manche.

Menos: um motor mais discreto.

Por que aqui: Sets estimated engine vibration using configured telemetry and response, not measured cockpit vibration.

Flap motion0%

Vibração contínua apenas enquanto o simulador informa as superfícies de flape realmente em movimento. Segue o movimento e as falhas reais do atuador, não um cronômetro estimado.

Mais: mais vibração com os flapes em movimento.

Menos: cursos de flape mais discretos.

Por que aqui: Sets texture from observed flap movement; a command without movement does not establish the cue.

Autopilot follow

AP follow authority5%

Quanto os comandos do piloto automático podem mover fisicamente o manche. Mantido minúsculo no MSFS, onde um eixo movido pode ser lido de volta como entrada do piloto; zero desativa o seguimento por completo.

Mais: o piloto automático move seu manche visivelmente mais.

Menos: um seguimento quase imperceptível.

Por que aqui: 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.

Por que aqui: 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.

Por que aqui: 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.

Por que aqui: 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.

Por que aqui: 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.

Por que aqui: Enables rate damping with the configured coefficients and control law.

Autopilot

Autopilot · Follow enabledFalse

Whether this feature is active in this profile.

Por que aqui: 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.

Por que aqui: Permits centering hold during a supported AP state, separate from following a moving target.

Autopilot · Neutral hold strength0.6

Por que aqui: Sets admitted AP neutral-hold strength; inactive while neutral hold is disabled.

Aero

Aero · EnabledTrue

Whether this feature is active in this profile.

Por que aqui: Enables aerodynamic cues; each still needs nonzero strength and its simulator conditions.

Aero · Max flap index1

Where this effect reaches full strength (or has fully faded, for washouts).

Mais: a more gradual build to a later peak.

Menos: a quicker build.

Por que aqui: Sets the final flap index for detent normalization. UP plus three detents uses maximum index3.

Aero · Min flap index1

Where this effect begins fading in.

Mais: the effect begins later.

Menos: it begins earlier.

Por que aqui: 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.

Por que aqui: Permits shaker at supported warning conditions; the switch does not establish aircraft equipment.

Ground

Ground · EnabledTrue

Whether this feature is active in this profile.

Por que aqui: 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.

Por que aqui: Enables engine cues with nonzero settings and valid running-engine telemetry.

Mechanical

Mechanical · EnabledTrue

Whether this feature is active in this profile.

Por que aqui: Enables accessory cues with configured strengths and observed accessory movement.

Mechanical · Gain0

The strength of this effect.

Mais: a stronger effect.

Menos: a weaker one.

Por que aqui: Sets texture from observed gear movement, separate from aerodynamic and touchdown effects.

Todas as configurações do perfil
Configurações estimadas do perfil
ParâmetroValorO que controla e por quê
Spring strength0.74 The selected response supplies the racer’s pitch/roll balance. The baseline spring is 0.74. Its low-speed blend reaches baseline strength at 85 KIAS.
Spring deadband0.03 Sets travel around the centre before the baseline spring resists. Smaller values engage it sooner.
Force gain0.4 The aerodynamic-load gain is 0.4 with an indicated-speed reference of 170 KIAS. This supplies speed-dependent loading alongside the spring.
Master gain0.85 Scales overall profile strength while preserving effect balance, subject to device and output limits.
Dynamic-pressure blendTrue Allows baseline spring strength to rise with indicated airspeed where the control law permits it.
Minimum spring factor0.5 Sets low-speed spring strength as a fraction of baseline when blending is enabled. One keeps full strength.
Spring wake-up speed20 ktSets the IAS where the low-speed spring blend starts rising. This is a feel threshold, not a flight limit.
Spring full-strength speed85.0 ktSets the IAS where the low-speed blend reaches baseline strength; high-speed stiffening also uses it.
Velocidade de ajuste de força170.0 ktSets the IAS reference for aerodynamic loading. It is an estimate, not published cruise TAS or a flight limit.
Airspeed spring stiffening0 The high-speed spring-stiffening gain is 0. No additional speed-driven stiffening is added; this does not disable independent aerodynamic loading.
Airspeed stiffening cap5 Limits the squared airspeed ratio used for high-speed spring stiffening; it is not a device-force cap.
Aileron force scale0.72 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 scale1.0 Scales pitch aerodynamic loading; pitch spring travel and trim responses are separate settings.
Maximum output force0.55 Caps directed-force output. Native spring effects and device limits remain separate.
StickFeel · Trim feel enabledTrue Retained for compatibility and group membership. Trim relief, rather than this flag, controls centre movement.
StickFeel · Trim relief enabledTrue Allows trim relief with supported control law and valid telemetry. Axis authorities set its amount.
StickFeel · Elevator authority0.3 Pitch trim relief accompanies the named racing configuration. Pitch authority 0.3 provides load relief and permitted centre movement; roll authority is 0.
StickFeel · Aileron authority0 Scales supported roll-trim relief and permitted centre movement. Zero removes roll response.
StickFeel · Force trim enabledFalse Enables local force trim, separate from aircraft-owned trim and add-on integration qualification.
StickFeel · G load enabledTrue Allows load-factor changes to modify permitted spring laws. Passive fly-by-wire feel can suppress it.
StickFeel · Rate damping enabledTrue Enables rate damping with the configured coefficients and control law.
Autopilot · Follow enabledFalse Autopilot following is off; the configured spring and load retain the hardware feel.
Autopilot · Follow authority0.05 Sets admitted AP-follow gain, not a percentage of travel. Runtime ownership and input limits still apply.
Autopilot · Neutral hold enabledFalse Permits centering hold during a supported AP state, separate from following a moving target.
Autopilot · Neutral hold strength0.6 Sets admitted AP neutral-hold strength; inactive while neutral hold is disabled.
Aero · EnabledTrue Enables aerodynamic cues; each still needs nonzero strength and its simulator conditions.
Aero · Gain0.3 Sets stall-buffet strength. Zero removes the cue without changing simulator stalls or warnings.
Aero · Gain0 Sets high-Mach buffet strength; onset and full-strength thresholds are separate.
Aero · Gain0 Sets flap buffet at the configured position and speed gates. Flap movement texture is separate.
Aero · Max flap index1 Sets the final flap index for detent normalization. UP plus three detents uses maximum index3.
Aero · Min flap index1 Sets the first flap detent that admits buffet; this is a handle index, not degrees.
Aero · Gain0 Sets gear aerodynamic buffet; movement and ground-contact cues are separate.
Aero · Shaker enabledFalse Permits shaker at supported warning conditions; the switch does not establish aircraft equipment.
Aero · Amplitude0.5 Sets triggered shaker strength; inactive while the shaker feature is disabled.
Ground · EnabledTrue Enables ground effects; each still needs its own strength and contact or motion telemetry.
Ground · Gain0.4 Sets rolling texture strength, modified by speed, surface and undercarriage configuration.
Ground · Gain0.3 Sets gear-bump texture during ground motion, separate from touchdown impact.
Ground · Gain0.6 Sets landing-impact strength; landing telemetry and response shape determine the pulse.
Ground · Gain0 Sets reverse-thrust vibration with valid reverser and engine conditions. Zero removes the cue.
Engine · EnabledTrue Enables engine cues with nonzero settings and valid running-engine telemetry.
Engine · Gain0.12 Sets estimated engine vibration using configured telemetry and response, not measured cockpit vibration.
Mechanical · EnabledTrue Enables accessory cues with configured strengths and observed accessory movement.
Mechanical · Gain0 Sets texture from observed flap movement; a command without movement does not establish the cue.
Mechanical · Gain0 Sets texture from observed gear movement, separate from aerodynamic and touchdown effects.
Fontes públicas 9
  1. MX Aircraft MXSResearch background · Wikipedia revision 1325253314 · retrieved 2026-09-12
  2. MX Aircraft Examination ReportMX Aircraft MXS-R
  3. Microsoft Flight Simulator aircraft manuals
  4. MSFS 2024 FAQ and edition aircraft inventory
  5. Nigel Lamb: nie postrzegam swojego wieku jako przeszkodyPilot interview · 21 July 2014
  6. More training the key for DFW: HallMatt Hall · 4 September 2014
  7. Interview with aerobatic extraordinaire and air race pilot Mika BrageotTelephone interview · 11 July 2017
  8. ICAO Doc 8643 — aircraft type designatorsPublic search data retrieved 2026-09-14; authority update 2026-09-03
  9. MXS development and constructionMX Aircraft account of the MXS development and configurable equipment.

Comunidade e correções

Se a sua experiência no tipo diz que esta página errou, corrija aqui.

Correções de pilotos

Voa esta aeronave? Corrija esta página.

Esta página é construída com referências citadas, e experiência real no tipo vale mais que citação. Cite a afirmação errada e conte o que a aeronave real faz. As correções vão ao mantenedor para revisão e alimentam a próxima revisão desta pesquisa.

Papo de hangar

Conversa aberta sobre voar e ajustar o MX Aircraft MXS-R, no fórum da comunidade. As correções acima vão em particular ao mantenedor; o papo de hangar é público.

Ainda não há papo de hangar sobre o MX Aircraft MXS-R. Seja quem começa.

Comunidade

Perfis da comunidade para esta aeronave

Ainda não há perfis da comunidade para esta aeronave. Ajustou do seu jeito? Compartilhe um perfil e ele aparecerá aqui.