| Spring strength | 0.55 | Fixed centering follows the A350's passive sidestick arrangement instead of interpreting load-factor demand as aerodynamic hand force. The baseline spring is 0.55. Low-speed spring blending is off. |
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| Spring deadband | 0.01 | Sets travel around the centre before the baseline spring resists. Smaller values engage it sooner. |
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| Forces · Center starting force | 0.03 | The centre preload is 0.03. It ramps outside the 0.01 deadband across 0.05 travel, shaping the passive centre independently of aircraft autotrim. |
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| Forces · Center starting force transition | 0.05 | Sets the travel used to ramp in centre preload. Wider intervals make its onset more gradual. |
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| Force gain | 0.04 | The stored 0.04 aerodynamic-load gain is inactive under the fixed-centre control law. |
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| Master gain | 0.85 | Scales overall profile strength while preserving effect balance, subject to device and output limits. |
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| Dynamic-pressure blend | False | Allows baseline spring strength to rise with indicated airspeed where the control law permits it. |
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| Minimum spring factor | 0.5 | Sets low-speed spring strength as a fraction of baseline when blending is enabled. One keeps full strength. |
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| 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. |
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| Spring full-strength speed | 90 kt | Sets the IAS where the low-speed blend reaches baseline strength; high-speed stiffening also uses it. |
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| 力回饋調校速度 | 275 kt | Sets the IAS reference for aerodynamic loading. It is an estimate, not published cruise TAS or a flight limit. |
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| Airspeed spring stiffening | 0 | Adds permitted spring resistance above the full-blend speed. Zero removes this high-speed increase. |
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| Airspeed stiffening cap | 5 | Limits the squared airspeed ratio used for high-speed spring stiffening; it is not a device-force cap. |
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| Aileron force scale | 1 | Roll and pitch aerodynamic scales are 1 and 1, respectively. These stored weights do not create directed aerodynamic loading while that term is inactive. The pitch spring-travel curve reaches output 1 at input 1. The roll spring-travel curve reaches output 0.3 at input 1. Spring-travel response contributes separately to axis balance. |
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| Elevator force scale | 1 | Scales pitch aerodynamic loading; pitch spring travel and trim responses are separate settings. |
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| Maximum output force | 0.55 | Caps directed-force output. Native spring effects and device limits remain separate. |
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| SpringResponse · Travel enabled | True | Applies the configured pitch and roll spring travel curves. |
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| SpringResponse · Output | 1 | Sets response at the second pitch-curve point; it is an endpoint only if its input position is full travel. |
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| SpringResponse · Output | 0.3 | Sets response at the second roll-curve point; its input position and other points determine the travel law. |
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| StickFeel · Trim feel enabled | False | Retained for compatibility and group membership. Trim relief, rather than this flag, controls centre movement. |
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| StickFeel · Trim relief enabled | False | Allows trim relief with supported control law and valid telemetry. Axis authorities set its amount. |
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| StickFeel · Elevator authority | 0 | The documented automatic pitch trim belongs to the aircraft's fly-by-wire response and leaves this profile's hardware centre independent. Pitch relief is off, with stored authority 0; roll authority is 0. |
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| StickFeel · Aileron authority | 0 | Scales supported roll-trim relief and permitted centre movement. Zero removes roll response. |
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| StickFeel · Force trim enabled | False | Enables local force trim, separate from aircraft-owned trim and add-on integration qualification. |
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| StickFeel · G load enabled | False | Allows load-factor changes to modify permitted spring laws. Passive fly-by-wire feel can suppress it. |
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| StickFeel · Rate damping enabled | False | Enables rate damping with the configured coefficients and control law. |
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| Autopilot · Follow enabled | False | Autopilot following is off; the configured spring and load retain the hardware feel. Separate neutral hold is on at strength 0.28, when a supported autopilot state admits it. |
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| Autopilot · Follow authority | 0.05 | Sets admitted AP-follow gain, not a percentage of travel. Runtime ownership and input limits still apply. |
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| Autopilot · Neutral hold enabled | True | Permits centering hold during a supported AP state, separate from following a moving target. |
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| Autopilot · Neutral hold strength | 0.28 | Sets admitted AP neutral-hold strength; inactive while neutral hold is disabled. |
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| Aero · Enabled | True | Enables aerodynamic cues; each still needs nonzero strength and its simulator conditions. |
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| Aero · Gain | 0.06 | Sets stall-buffet strength. Zero removes the cue without changing simulator stalls or warnings. |
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| Aero · Gain | 0.06 | Sets high-Mach buffet strength; onset and full-strength thresholds are separate. |
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| Aero · Gain | 0 | Sets flap buffet at the configured position and speed gates. Flap movement texture is separate. |
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| Aero · Max flap index | 4 | Sets the final flap index for detent normalization. UP plus three detents uses maximum index3. |
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| Aero · Min flap index | 2 | Sets the first flap detent that admits buffet; this is a handle index, not degrees. |
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| Aero · Gain | 0 | Sets gear aerodynamic buffet; movement and ground-contact cues are separate. |
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| Aero · Shaker enabled | False | Permits shaker at supported warning conditions; the switch does not establish aircraft equipment. |
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| Aero · Amplitude | 0.5 | Sets triggered shaker strength; inactive while the shaker feature is disabled. |
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| Ground · Enabled | False | Enables ground effects; each still needs its own strength and contact or motion telemetry. |
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| Ground · Gain | 0 | Sets rolling texture strength, modified by speed, surface and undercarriage configuration. |
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| Ground · Gain | 0 | Sets gear-bump texture during ground motion, separate from touchdown impact. |
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| Ground · Gain | 0 | Sets landing-impact strength; landing telemetry and response shape determine the pulse. |
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| Ground · Gain | 0 | Sets reverse-thrust vibration with valid reverser and engine conditions. Zero removes the cue. |
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| Engine · Enabled | False | Enables engine cues with nonzero settings and valid running-engine telemetry. |
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| Engine · Gain | 0 | Sets estimated engine vibration using configured telemetry and response, not measured cockpit vibration. |
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| Mechanical · Enabled | True | Enables accessory cues with configured strengths and observed accessory movement. |
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| Mechanical · Gain | 0 | Sets texture from observed flap movement; a command without movement does not establish the cue. |
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| Mechanical · Gain | 0 | Sets texture from observed gear movement, separate from aerodynamic and touchdown effects. |
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