| Spring strength | 0.74 | An elevator-trim lever adjusts pitch trim. The baseline spring is 0.74. Its low-speed blend reaches baseline strength at 45 KIAS. |
|---|
| Force gain | 0.8 | The aerodynamic-load gain is 0.8 with an indicated-speed reference of 75 KIAS. This supplies speed-dependent loading alongside the spring. |
|---|
| Elevator force scale | 1 | Scales pitch aerodynamic loading; pitch spring travel and trim responses are separate settings. |
|---|
| Aileron force scale | 0.74 | Roll and pitch aerodynamic scales are 0.74 and 1, respectively. They set the aerodynamic axis balance. No custom spring-travel curve is enabled. |
|---|
| Maximum output force | 0.55 | Caps directed-force output. Native spring effects and device limits remain separate. |
|---|
| StickFeel · Elevator authority | 0.3 | An elevator-trim lever adjusts pitch trim. 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. |
|---|
| Velocidade de ajuste de força | 75 kt | Sets the IAS reference for aerodynamic loading. It is an estimate, not published cruise TAS or a flight limit. |
|---|
| Ground · Gain | 0.14 | Wheel-brake cues are disabled for the selected ski starting point. Persistence and cabin options do not supply force calibration. |
|---|
| Mechanical · Gain | 0 | Wheel-brake cues are disabled for the selected ski starting point. Persistence and cabin options do not supply force calibration. |
|---|
| Mechanical · Gain | 0 | Wheel-brake cues are disabled for the selected ski starting point. Persistence and cabin options do not supply force calibration. |
|---|
| Spring deadband | 0.04 | Sets travel around the centre before the baseline spring resists. Smaller values engage it sooner. |
|---|
| 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 | 0.55 | Sets low-speed spring strength as a fraction of baseline when blending is enabled. One keeps full strength. |
|---|
| Spring wake-up speed | 15 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 | 45 kt | Sets the IAS where the low-speed blend reaches baseline strength; high-speed stiffening also uses it. |
|---|
| Airspeed spring stiffening | 0.15 | The 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 stiffening cap | 5 | Limits the squared airspeed ratio used for high-speed spring stiffening; it is not a device-force cap. |
|---|
| StickFeel · Trim feel enabled | False | 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 · 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 | Sets flap buffet at the configured position and speed gates. Flap movement texture is separate. |
|---|
| Aero · Max flap index | 3 | 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 | 0.1 | Sets gear-bump texture during ground motion, separate from touchdown impact. |
|---|
| Ground · Gain | 0.32 | 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. |
|---|
