AEROMOT / PISTON

Aeromot AMT200S Super Ximango

A powered glider with retractable main gear, wing airbrakes and a feathering propeller.

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Landing gearRetractable main wheel
Soaring equipmentWing airbrakes · feathering propeller
Simulator ecosystems
YOUR AIRCRAFT COMPANION

Start here

A few places to begin, from the aircraft’s story to the people who fly it.

Introduction

Aircraft and configuration

The AMT200S Super Ximango combines powered flying and soaring with a retractable main wheel, wing airbrakes and feathering propeller. The wings fold only while the aircraft is stationary. Restauravia offers separate MSFS and X-Plane 12 implementations.

Aeromot AMT200S Super Ximango

restauravia.fr · Read more ↗
THE AIRCRAFT

Meet Aeromot AMT200S Super Ximango

The AMT200S Super Ximango combines powered flying and soaring with a retractable main wheel, wing airbrakes and feathering propeller. The wings fold only while the aircraft is stationary. Restauravia offers separate MSFS and X-Plane 12 implementations.

HOW IT CAME TO BE

History & design

A Brazilian branch of the Fournier family

Restauravia identifies the Super Ximango as Aeromot's Brazilian development of the Fournier RF10 motor-glider concept. The represented 1990s aircraft combines side-by-side seating and an engine for self-powered flight with wing airbrakes, a feathering propeller and retractable main wheels for soaring.

The manual describes military training use under the USAF Academy designation TG-14, alongside deliveries in Brazil and the Dominican Republic and private ownership. Its folding wings address storage on the ground rather than changing the aircraft's configuration in flight.

restauravia.fr · Aeromot AMT200S Super Ximango — simulator documentation ↗

Developer English manual, description on page 3; not an independently established production chronology.

UNDER THE SKIN

Systems & details

VIRTUAL VERSIONS

In your simulator

No released simulator product is listed for this aircraft in the developers reviewed. Announced products are excluded.

GO TO THE SOURCE

Manuals & resources

Find your next read

Choose a topic for a short introduction and a link to the original source. Simulator references identify the developer and edition they cover.

Simulator documentation

MSFS cockpitAeromot AMT200S Super Ximango

The MSFS aircraft includes a KAP 140 autopilot, retractable main gear, wing airbrakes and a feathering propeller. Wing folding is ground-only.

MSFS English manual · pages 2–10

restauravia.fr · Read the source ↗
X-Plane cockpitAeromot AMT200S Super Ximango

The X-Plane 12 aircraft uses an STEC 55 autopilot with heading and altitude functions. Winglet and non-winglet versions are included.

X-Plane English manual · pages 2–10

restauravia.fr · Read the source ↗

Read the original documentation from the people who created it. Manuals open on their publisher’s website.

Simulator documentation

↗Aeromot AMT200S Super Ximango — simulator documentationrestauravia.fr · MSFS and X-Plane English manuals · pages 2–10 ↗Aeromot AMT200S Super Ximango — simulator documentationrestauravia.fr · X-Plane English manual · pages 2–10
AIRCRAFT AND FEEL

Built-in force-feedback profiles

Read the documentary basis, editable starting settings and remaining questions for the aircraft you fly. Each explanation refers to the exact profile revision shown.

Catalogue programme-20261011-v3 · 3 profile choices

FFB-BRIDGE BUILT-IN PROFILE

Restauravia Aeromot AMT200S Super Ximango

Free and ProRevision 2Inherited starting point

A powered glider with retractable main gear, wing airbrakes and a feathering propeller.

Aircraft and simulator scope

  • Restauravia Aeromot AMT200S Super Ximango · Restauravia · MSFS 2020 · Add-on starting point
  • Restauravia Aeromot AMT200S Super Ximango · Restauravia · MSFS 2024 · Add-on starting point

The simulator model and controls

Restauravia Aeromot AMT200S Super Ximango is the selected Restauravia configuration.

How this profile feels

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.

Aircraft and configuration

The AMT200S Super Ximango combines powered flying and soaring with a retractable main wheel, wing airbrakes and feathering propeller. The wings fold only while the aircraft is stationary. Restauravia offers separate MSFS and X-Plane 12 implementations.

About the values

Strengths are normalized hardware-feel settings. They set the effect balance; hand force depends on the device and its limits. The IAS reference is a tuning value.

Documentary review and sources

These decisions describe the documentary basis and remaining gaps for this revision. Aircraft documentation and a starting setting describe different kinds of evidence.

Aircraft and variant
Inherited

Restauravia Aeromot AMT200S Super Ximango is the selected Restauravia configuration.

Flight controls
Inherited

A powered glider with retractable main gear, wing airbrakes and a feathering propeller.

Trim
Inherited

The profile uses the trim behaviour configured below. Pitch authority 0.3 provides load relief and permitted centre movement; roll authority is 0.

Autopilot and stability
Inherited

Autopilot following is off; the configured spring and load retain the hardware feel.

Equipment
Inherited

The AMT200S Super Ximango combines powered flying and soaring with a retractable main wheel, wing airbrakes and feathering propeller. The wings fold only while the aircraft is stationary. Restauravia offers separate MSFS and X-Plane 12 implementations.

Speeds and limits
Inherited

The indicated-speed references set the profile response scale; they are separate from aircraft operating limits.

Simulator integration
Inherited

The profile targets msfs2020, msfs2024. Add-on-specific controls use only the supported references configured by this profile.

Force-feedback settings
Inherited

The settings define the profile’s effect balance. Device output limits affect physical hand force.

Starting settings and their rationale

These configured values are starting estimates. The explanations describe what each setting controls; physical validation appears separately below.

Estimated starting settings · revision 2
SettingStarting valueWhat it controls and why
Spring strengthStarting value0.74 What it controls and whyThis profile uses reversible-control loading for Aeromot AMT200S Super Ximango. The baseline spring is 0.74. Its low-speed blend reaches baseline strength at 45 KIAS.
Master force gainStarting value0.85 What it controls and whyScales overall profile strength while preserving effect balance, subject to device and output limits.
Profile force gainStarting value0.8 What it controls and whyThe aerodynamic-load gain is 0.8 with an indicated-speed reference of 95 KIAS. This supplies speed-dependent loading alongside the spring.
Force tuning speed/referenceStarting value95 ktWhat it controls and whySets the IAS reference for aerodynamic loading. It is an estimate, not published cruise TAS or a flight limit.
Spring response reference speedStarting value45 ktWhat it controls and whySets the IAS where the low-speed blend reaches baseline strength; high-speed stiffening also uses it.
Aileron force scaleStarting value0.68 What it controls and whyRoll and pitch aerodynamic scales are 0.68 and 0.86, respectively. They set the aerodynamic axis balance. No custom spring-travel curve is enabled.
Elevator force scaleStarting value0.86 What it controls and whyScales pitch aerodynamic loading; pitch spring travel and trim responses are separate settings.
Trim feelStarting valueDisabled What it controls and whyRetained for compatibility and group membership. Trim relief, rather than this flag, controls centre movement.
Trim reliefStarting valueEnabled What it controls and whyAllows trim relief with supported control law and valid telemetry. Axis authorities set its amount.
Autopilot followStarting valueDisabled What it controls and whyAutopilot following is off; the configured spring and load retain the hardware feel.
Autopilot neutral holdStarting valueDisabled What it controls and whyPermits centering hold during a supported AP state, separate from following a moving target.
Output force limitStarting value0.55 What it controls and whyCaps directed-force output. Native spring effects and device limits remain separate.
All 44 starting settings and their rationale

The settings define the profile’s effect balance. Device output limits affect physical hand force.

Estimated starting settings · revision 2
SettingStarting valueWhat it controls and why
Spring strengthStarting value0.74 What it controls and whyThis profile uses reversible-control loading for Aeromot AMT200S Super Ximango. The baseline spring is 0.74. Its low-speed blend reaches baseline strength at 45 KIAS.
Spring deadbandStarting value0.04 What it controls and whySets travel around the centre before the baseline spring resists. Smaller values engage it sooner.
Profile force gainStarting value0.8 What it controls and whyThe aerodynamic-load gain is 0.8 with an indicated-speed reference of 95 KIAS. This supplies speed-dependent loading alongside the spring.
Master force gainStarting value0.85 What it controls and whyScales overall profile strength while preserving effect balance, subject to device and output limits.
QBlend EnabledStarting valueEnabled What it controls and whyAllows baseline spring strength to rise with indicated airspeed where the control law permits it.
QSpring Minimum FactorStarting value0.55 What it controls and whySets low-speed spring strength as a fraction of baseline when blending is enabled. One keeps full strength.
QSpring Start KnotsStarting value15 ktWhat it controls and whySets the IAS where the low-speed spring blend starts rising. This is a feel threshold, not a flight limit.
Spring response reference speedStarting value45 ktWhat it controls and whySets the IAS where the low-speed blend reaches baseline strength; high-speed stiffening also uses it.
Force tuning speed/referenceStarting value95 ktWhat it controls and whySets the IAS reference for aerodynamic loading. It is an estimate, not published cruise TAS or a flight limit.
Airspeed spring stiffening gainStarting value0.15 What it controls and whyThe high-speed spring-stiffening gain is 0.15. It strengthens the permitted spring response above 45 KIAS, with the squared-speed ratio capped at 5.
Airspeed spring stiffening limitStarting value5 What it controls and whyLimits the squared airspeed ratio used for high-speed spring stiffening; it is not a device-force cap.
Aileron force scaleStarting value0.68 What it controls and whyRoll and pitch aerodynamic scales are 0.68 and 0.86, respectively. They set the aerodynamic axis balance. No custom spring-travel curve is enabled.
Elevator force scaleStarting value0.86 What it controls and whyScales pitch aerodynamic loading; pitch spring travel and trim responses are separate settings.
Output force limitStarting value0.55 What it controls and whyCaps directed-force output. Native spring effects and device limits remain separate.
Trim feelStarting valueDisabled What it controls and whyRetained for compatibility and group membership. Trim relief, rather than this flag, controls centre movement.
Trim reliefStarting valueEnabled What it controls and whyAllows trim relief with supported control law and valid telemetry. Axis authorities set its amount.
Elevator AuthorityStarting value0.3 What it controls and whyThe profile uses the trim behaviour configured below. Pitch authority 0.3 provides load relief and permitted centre movement; roll authority is 0.
Aileron AuthorityStarting value0 What it controls and whyScales supported roll-trim relief and permitted centre movement. Zero removes roll response.
Force Trim EnabledStarting valueDisabled What it controls and whyEnables local force trim, separate from aircraft-owned trim and add-on integration qualification.
GLoad EnabledStarting valueEnabled What it controls and whyAllows load-factor changes to modify permitted spring laws. Passive fly-by-wire feel can suppress it.
Rate Damping EnabledStarting valueEnabled What it controls and whyEnables rate damping with the configured coefficients and control law.
Autopilot followStarting valueDisabled What it controls and whyAutopilot following is off; the configured spring and load retain the hardware feel.
Autopilot follow authorityStarting value0.1 What it controls and whySets admitted AP-follow gain, not a percentage of travel. Runtime ownership and input limits still apply.
Autopilot neutral holdStarting valueDisabled What it controls and whyPermits centering hold during a supported AP state, separate from following a moving target.
Autopilot neutral hold strengthStarting value0.6 What it controls and whySets admitted AP neutral-hold strength; inactive while neutral hold is disabled.
EnabledStarting valueEnabled What it controls and whyEnables aerodynamic cues; each still needs nonzero strength and its simulator conditions.
GainStarting value0.35 What it controls and whySets stall-buffet strength. Zero removes the cue without changing simulator stalls or warnings.
GainStarting value0 What it controls and whySets high-Mach buffet strength; onset and full-strength thresholds are separate.
GainStarting value0 What it controls and whySets flap buffet at the configured position and speed gates. Flap movement texture is separate.
Maximum flap indexStarting value1 What it controls and whySets the final flap index for detent normalization. UP plus three detents uses maximum index3.
Minimum flap indexStarting value1 What it controls and whySets the first flap detent that admits buffet; this is a handle index, not degrees.
GainStarting value0 What it controls and whySets gear aerodynamic buffet; movement and ground-contact cues are separate.
Shaker EnabledStarting valueDisabled What it controls and whyPermits shaker at supported warning conditions; the switch does not establish aircraft equipment.
Stick shaker amplitudeStarting value0.5 What it controls and whySets triggered shaker strength; inactive while the shaker feature is disabled.
EnabledStarting valueEnabled What it controls and whyEnables ground effects; each still needs its own strength and contact or motion telemetry.
GainStarting value0.4 What it controls and whySets rolling texture strength, modified by speed, surface and undercarriage configuration.
GainStarting value0.25 What it controls and whySets gear-bump texture during ground motion, separate from touchdown impact.
GainStarting value0.65 What it controls and whySets landing-impact strength; landing telemetry and response shape determine the pulse.
GainStarting value0 What it controls and whySets reverse-thrust vibration with valid reverser and engine conditions. Zero removes the cue.
EnabledStarting valueEnabled What it controls and whyEnables engine cues with nonzero settings and valid running-engine telemetry.
GainStarting value0.12 What it controls and whySets estimated engine vibration using configured telemetry and response, not measured cockpit vibration.
EnabledStarting valueEnabled What it controls and whyEnables accessory cues with configured strengths and observed accessory movement.
GainStarting value0 What it controls and whySets texture from observed flap movement; a command without movement does not establish the cue.
GainStarting value0.035 What it controls and whySets texture from observed gear movement, separate from aerodynamic and touchdown effects.
Limits and open questions
  • Force magnitudes and speed references are estimates. Physical and installed acceptance are deferred.
  • 132ktVNE; XP81VNO conflicts with100ktcruise/107KIASglide table. MSFS80hp config conflicts with100hp manual. These are retained and not used as force calibration.
  • Manual motor-glider estimate; developer identifies a real motor-glider pilot among collaborators. This is documentary quality evidence, not independent flight testing.
  • Legacy manual material is used only with separately verified current package scope.

Physical validation

No physical force validation is recorded in this public catalogue for this revision. Documentary review and software checks do not establish how a particular device feels.

FFB-Bridge maintains this profile’s revisions and tuning discussion.

Revision 2 and download availability in FFB-Bridge ↗
Exact profile identity
Profile
addon-restauravia-ximango
Artifact SHA-256
b6152e940d46a0b2f2c6c587c8cbca3c10e32831b0374fb138c450349d46445f
Bytes
13077
Spring strength
Forces.SpringStrength
Spring deadband
Forces.SpringDeadband
Profile force gain
Forces.ForceGain
Master force gain
Forces.MasterGain
QBlend Enabled
Forces.QBlendEnabled
QSpring Minimum Factor
Forces.QSpringMinimumFactor
QSpring Start Knots
Forces.QSpringStartKnots
Spring response reference speed
Forces.QSpringFullKnots
Force tuning speed/reference
Forces.CruiseSpeedRefKnots
Airspeed spring stiffening gain
Forces.SpringAirspeedStiffenGain
Airspeed spring stiffening limit
Forces.SpringAirspeedStiffenCap
Aileron force scale
Forces.AileronForceScale
Elevator force scale
Forces.ElevatorForceScale
Output force limit
Forces.MaxOutputForce
Trim feel
StickFeel.TrimFeelEnabled
Trim relief
StickFeel.TrimReliefEnabled
Elevator Authority
StickFeel.TrimRelief.ElevatorAuthority
Aileron Authority
StickFeel.TrimRelief.AileronAuthority
Force Trim Enabled
StickFeel.ForceTrimEnabled
GLoad Enabled
StickFeel.GLoadEnabled
Rate Damping Enabled
StickFeel.RateDampingEnabled
Autopilot follow
Autopilot.FollowEnabled
Autopilot follow authority
Autopilot.FollowAuthority
Autopilot neutral hold
Autopilot.NeutralHoldEnabled
Autopilot neutral hold strength
Autopilot.NeutralHoldStrength
Enabled
Aero.Enabled
Gain
Aero.Stall.Gain
Gain
Aero.Mach.Gain
Gain
Aero.Flap.Gain
Maximum flap index
Aero.Flap.MaxFlapIndex
Minimum flap index
Aero.Flap.MinFlapIndex
Gain
Aero.Gear.Gain
Shaker Enabled
Aero.ShakerEnabled
Stick shaker amplitude
Aero.Shaker.Amplitude
Enabled
Ground.Enabled
Gain
Ground.Rumble.Gain
Gain
Ground.Bumps.Gain
Gain
Ground.Thump.Gain
Gain
Ground.Reverse.Gain
Enabled
Engine.Enabled
Gain
Engine.Rumble.Gain
Enabled
Mechanical.Enabled
Gain
Mechanical.FlapMotion.Gain
Gain
Mechanical.GearMotion.Gain
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