Start here
A few places to begin, from the aircraft’s story to the people who fly it.
Aircraft and configuration
Wing42 offers three Blériot XI versions: the 25 hp Anzani, 50 hp Gnome and Anzani R.I.P. realism model. All have fixed wheels and tail contact. Wing warping supplies roll control with limited effectiveness and substantial physical effort described in the manual.
Bleriot XI Anzani
Wing42 · Read more ↗Meet Bleriot XI Anzani
Wing42 offers three Blériot XI versions: the 25 hp Anzani, 50 hp Gnome and Anzani R.I.P. realism model. All have fixed wheels and tail contact. Wing warping supplies roll control with limited effectiveness and substantial physical effort described in the manual.
History & design
A design refined into a Channel crossing
Raymond Saulnier led much of the Type XI design work, with substantial input from Louis Blériot. The aircraft first flew in January 1909; on 25 July, Blériot crossed from Calais to Dover, giving the monoplane international recognition.
National Air and Space Museum · Blériot XI ↗Smithsonian: 1909 design and separate 1914 exhibit
A family of early monoplanes
Orders and licensed production followed the Channel flight. The Smithsonian’s aircraft is a later, 1914 example with a 50 hp Gnôme rotary engine, flown by display pilot John Domenjoz. It should not be confused with the original Anzani-powered Channel-crossing machine.
National Air and Space Museum · Blériot XI ↗Smithsonian: 1909 design and separate 1914 exhibit
Systems & details
Controls and equipment
The aircraft has no wheel brakes. Ignition blipping regulates engine power, while the parking-brake binding operates chocks. The performance table gives speed values without identifying IAS or TAS.
In your simulator
No released simulator product is listed for this aircraft in the developers reviewed. Announced products are excluded.
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
Controls and equipmentBleriot XI Anzani
The aircraft has no wheel brakes. Ignition blipping regulates engine power, while the parking-brake binding operates chocks. The performance table gives speed values without identifying IAS or TAS.
Simulation manual · pages 5–8 and 10–15
Wing42 · Read the source ↗Read the original documentation from the people who created it. Manuals open on their publisher’s website.
Simulator documentation
Bleriot XI Anzani — simulator documentationWing42 · Simulation manual · pages 5–8 and 10–15Aircraft history
Blériot XINational Air and Space Museum · Smithsonian: 1909 design and separate 1914 exhibitBuilt-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 · 5 profile choices
Wing42 Bleriot XI Anzani
Wing42 · Free and Pro · Revision 2 · Inherited starting point
MSFS 2020
The XI with Anzani and Gnome engine versions and wing-warping controls.
Wing42 Bleriot XI Anzani R.I.P.
Wing42 · Free and Pro · Revision 2 · Inherited starting point
MSFS 2020
The XI with Anzani and Gnome engine versions and wing-warping controls.
Wing42 Bleriot XI Gnome
Wing42 · Free and Pro · Revision 2 · Inherited starting point
MSFS 2020
The XI with Anzani and Gnome engine versions and wing-warping controls.
Bleriot XI Anzani
Free and Pro · Revision 1 · Partial review
MSFS 2020 · MSFS 2024 · X-Plane 12
The XI with Anzani and Gnome engine versions and wing-warping controls.
Bleriot XI Gnome
Free and Pro · Revision 1 · Partial review
MSFS 2020 · MSFS 2024 · X-Plane 12
The XI with Anzani and Gnome engine versions and wing-warping controls.
Bleriot XI Anzani
The XI with Anzani and Gnome engine versions and wing-warping controls.
Aircraft and simulator scope
- Bleriot XI Anzani · MSFS 2020 · Variant starting point
- Bleriot XI Anzani · MSFS 2024 · Variant starting point
- Bleriot XI Anzani · X-Plane 12 · Variant starting point
Universal named airframe/configuration; intended MSFS2020/MSFS2024/XP12 starting point, not add-on or edition acceptance. · Physical facts and prior documentary review are reused from their archived dated sources; new market availability is not inferred.
The simulator model and controls
The XI with Anzani and Gnome engine versions and wing-warping controls.
How this profile feels
Spring resistance builds with the selected airspeed response. A separate aerodynamic term adds speed-dependent control load.
Pitch-trim relief is off. Autopilot following is off.
Aircraft and configuration
Fixed wheeled undercarriage and tail contact; the selected configuration has no wheel brakes, flaps, spoilers, reversers or stick shaker. Ignition blipping regulates power.
Controls and equipment
The aircraft has no wheel brakes. Ignition blipping regulates engine power, while the parking-brake binding operates chocks. The performance table gives speed values without identifying IAS or TAS.
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.
What the documentation establishes
Bleriot XI Anzani: Fixed wheeled undercarriage and tail contact; the selected configuration has no wheel brakes, flaps, spoilers, reversers or stick shaker. Ignition blipping regulates power.
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
ReviewedThe XI with Anzani and Gnome engine versions and wing-warping controls.
Flight controls
InheritedThe XI with Anzani and Gnome engine versions and wing-warping controls.
Trim
InheritedThe profile uses the trim behaviour configured below. Pitch relief is off, with stored authority 0; roll authority is 0.
Autopilot and stability
ReviewedAutopilot following is off; the configured spring and load retain the hardware feel.
Equipment
InheritedFixed wheeled undercarriage and tail contact; the selected configuration has no wheel brakes, flaps, spoilers, reversers or stick shaker. Ignition blipping regulates power.
Speeds and limits
InheritedThe indicated-speed references set the profile response scale; they are separate from aircraft operating limits.
Simulator integration
ReviewedThe profile targets msfs2020, msfs2024, xplane12. Add-on-specific controls use only the supported references configured by this profile.
Force-feedback settings
InheritedThe 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.
| Setting | Starting value | What it controls and why |
|---|---|---|
| Spring strength | Starting value0.64 | What it controls and whyRoll control: Wing warping. The baseline spring is 0.64. Its low-speed blend reaches baseline strength at 22 KIAS. |
| Master force gain | Starting value0.85 | What it controls and whyScales overall profile strength while preserving effect balance, subject to device and output limits. |
| Profile force gain | Starting value0.8 | What it controls and whyThe aerodynamic-load gain is 0.8 with an indicated-speed reference of 32 KIAS. This supplies speed-dependent loading alongside the spring. |
| Force tuning speed/reference | Starting value32 kt | What 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 speed | Starting value22 kt | What it controls and whySets the IAS where the low-speed blend reaches baseline strength; high-speed stiffening also uses it. |
| Aileron force scale | Starting value1 | What it controls and whyRoll and pitch aerodynamic scales are 1 and 0.78, respectively. They set the aerodynamic axis balance. No custom spring-travel curve is enabled. |
| Elevator force scale | Starting value0.78 | What it controls and whyScales pitch aerodynamic loading; pitch spring travel and trim responses are separate settings. |
| Trim feel | Starting valueDisabled | What it controls and whyRetained for compatibility and group membership. Trim relief, rather than this flag, controls centre movement. |
| Trim relief | Starting valueDisabled | What it controls and whyAllows trim relief with supported control law and valid telemetry. Axis authorities set its amount. |
| Autopilot follow | Starting valueDisabled | What it controls and whyAutopilot following is off; the configured spring and load retain the hardware feel. |
| Autopilot neutral hold | Starting valueDisabled | What it controls and whyPermits centering hold during a supported AP state, separate from following a moving target. |
| Output force limit | Starting 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.
| Setting | Starting value | What it controls and why |
|---|---|---|
| Spring strength | Starting value0.64 | What it controls and whyRoll control: Wing warping. The baseline spring is 0.64. Its low-speed blend reaches baseline strength at 22 KIAS. |
| Profile force gain | Starting value0.8 | What it controls and whyThe aerodynamic-load gain is 0.8 with an indicated-speed reference of 32 KIAS. This supplies speed-dependent loading alongside the spring. |
| Elevator force scale | Starting value0.78 | What it controls and whyScales pitch aerodynamic loading; pitch spring travel and trim responses are separate settings. |
| Aileron force scale | Starting value1 | What it controls and whyRoll and pitch aerodynamic scales are 1 and 0.78, respectively. They set the aerodynamic axis balance. No custom spring-travel curve is enabled. |
| Output force limit | Starting value0.55 | What it controls and whyCaps directed-force output. Native spring effects and device limits remain separate. |
Bleriot XI Anzani: The reviewed cockpit/procedures provide no pilot-operated pitch/roll trim. Both trim-centre and trim-relief effects are disabled; no modern-aircraft trim mechanism is inherited. Estimated pitch/roll trim authorities 0/0; exact add-on sign, travel, units and build-specific neutral remain unqualified. Rudder trim never substitutes for roll trim.
| Setting | Starting value | What it controls and why |
|---|---|---|
| Elevator Authority | Starting value0 | What it controls and whyThe profile uses the trim behaviour configured below. Pitch relief is off, with stored authority 0; roll authority is 0. |
| Aileron Authority | Starting value0 | What it controls and whyScales supported roll-trim relief and permitted centre movement. Zero removes roll response. |
Bleriot XI Anzani: 32 KIAS is the retained estimated tuning reference. It is not published cruise TAS, VNE, a new flight limit or a measured force threshold. Source-specific operating quantities remain attached to their original configuration and conditions.
| Setting | Starting value | What it controls and why |
|---|---|---|
| Force tuning speed/reference | Starting value32 kt | What it controls and whySets the IAS reference for aerodynamic loading. It is an estimate, not published cruise TAS or a flight limit. |
Unfitted-equipment effects and nosewheel shimmy are excluded. Piston and propwash texture remain estimates from standard engine/airflow channels.
| Setting | Starting value | What it controls and why |
|---|---|---|
| Gain | Starting value0 | What it controls and whyUnfitted-equipment effects and nosewheel shimmy are excluded. Piston and propwash texture remain estimates from standard engine/airflow channels. |
| Gain | Starting value0 | What it controls and whyUnfitted-equipment effects and nosewheel shimmy are excluded. Piston and propwash texture remain estimates from standard engine/airflow channels. |
| Gain | Starting value0.12 | What it controls and whyUnfitted-equipment effects and nosewheel shimmy are excluded. Piston and propwash texture remain estimates from standard engine/airflow channels. |
| Shaker Enabled | Starting valueDisabled | What it controls and whyUnfitted-equipment effects and nosewheel shimmy are excluded. Piston and propwash texture remain estimates from standard engine/airflow channels. |
Exact configured values with software explanations. Force magnitudes remain editable estimates; disabled features retain inactive values.
| Setting | Starting value | What it controls and why |
|---|---|---|
| Spring deadband | Starting value0.045 | What it controls and whySets travel around the centre before the baseline spring resists. Smaller values engage it sooner. |
| Master force gain | Starting value0.85 | What it controls and whyScales overall profile strength while preserving effect balance, subject to device and output limits. |
| QBlend Enabled | Starting valueEnabled | What it controls and whyAllows baseline spring strength to rise with indicated airspeed where the control law permits it. |
| QSpring Minimum Factor | Starting value0.5 | What it controls and whySets low-speed spring strength as a fraction of baseline when blending is enabled. One keeps full strength. |
| QSpring Start Knots | Starting value5 kt | What 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 speed | Starting value22 kt | What it controls and whySets the IAS where the low-speed blend reaches baseline strength; high-speed stiffening also uses it. |
| Airspeed spring stiffening gain | Starting value0.15 | What it controls and whyThe high-speed spring-stiffening gain is 0.15. It strengthens the permitted spring response above 22 KIAS, with the squared-speed ratio capped at 5. |
| Airspeed spring stiffening limit | Starting value5 | What it controls and whyLimits the squared airspeed ratio used for high-speed spring stiffening; it is not a device-force cap. |
| Trim feel | Starting valueDisabled | What it controls and whyRetained for compatibility and group membership. Trim relief, rather than this flag, controls centre movement. |
| Trim relief | Starting valueDisabled | What it controls and whyAllows trim relief with supported control law and valid telemetry. Axis authorities set its amount. |
| Force Trim Enabled | Starting valueDisabled | What it controls and whyEnables local force trim, separate from aircraft-owned trim and add-on integration qualification. |
| GLoad Enabled | Starting valueEnabled | What it controls and whyAllows load-factor changes to modify permitted spring laws. Passive fly-by-wire feel can suppress it. |
| Rate Damping Enabled | Starting valueEnabled | What it controls and whyEnables rate damping with the configured coefficients and control law. |
| Autopilot follow | Starting valueDisabled | What it controls and whyAutopilot following is off; the configured spring and load retain the hardware feel. |
| Autopilot follow authority | Starting 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 hold | Starting valueDisabled | What it controls and whyPermits centering hold during a supported AP state, separate from following a moving target. |
| Autopilot neutral hold strength | Starting value0.6 | What it controls and whySets admitted AP neutral-hold strength; inactive while neutral hold is disabled. |
| Enabled | Starting valueEnabled | What it controls and whyEnables aerodynamic cues; each still needs nonzero strength and its simulator conditions. |
| Gain | Starting value0.35 | What it controls and whySets stall-buffet strength. Zero removes the cue without changing simulator stalls or warnings. |
| Gain | Starting value0 | What it controls and whySets high-Mach buffet strength; onset and full-strength thresholds are separate. |
| Gain | Starting value0 | What it controls and whySets flap buffet at the configured position and speed gates. Flap movement texture is separate. |
| Maximum flap index | Starting value1 | What it controls and whySets the final flap index for detent normalization. UP plus three detents uses maximum index3. |
| Minimum flap index | Starting value1 | What it controls and whySets the first flap detent that admits buffet; this is a handle index, not degrees. |
| Gain | Starting value0 | What it controls and whySets gear aerodynamic buffet; movement and ground-contact cues are separate. |
| Stick shaker amplitude | Starting value0.5 | What it controls and whySets triggered shaker strength; inactive while the shaker feature is disabled. |
| Enabled | Starting valueEnabled | What it controls and whyEnables ground effects; each still needs its own strength and contact or motion telemetry. |
| Gain | Starting value0.4 | What it controls and whySets rolling texture strength, modified by speed, surface and undercarriage configuration. |
| Gain | Starting value0.25 | What it controls and whySets gear-bump texture during ground motion, separate from touchdown impact. |
| Gain | Starting value0.65 | What it controls and whySets landing-impact strength; landing telemetry and response shape determine the pulse. |
| Gain | Starting value0 | What it controls and whySets reverse-thrust vibration with valid reverser and engine conditions. Zero removes the cue. |
| Enabled | Starting valueEnabled | What it controls and whyEnables engine cues with nonzero settings and valid running-engine telemetry. |
| Enabled | Starting valueEnabled | What it controls and whyEnables accessory cues with configured strengths and observed accessory movement. |
Limits and open questions
- Bleriot XI Anzani is a universal starting point; exact add-on matching, edition operation and physical hand-force calibration remain unqualified.
- Autopilot movement and unknown custom trim, failure or force-input signals are disabled. Confirm the selected equipment fit and trim direction for the implementation in use.
- Force magnitudes and speed tuning are editable inherited estimates. Owner physical and installed-aircraft acceptance remain pending.
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.
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