Meet Embraer EMB-121 Xingu
Embraer’s Xingu first flew on 22 October 1976. The manufacturer identifies it as the first pressurized aircraft designed and built in Brazil, with an original executive-transport arrangement accommodating up to eight passengers.
History & design
Embraer enters pressurised executive aviation
The Xingu grew from Embraer's Project 12X studies of a pressurised turboprop family during the 1970s oil crisis. It first flew on 22 October 1976, initially without pressurisation operating; a pressurised test followed in May 1977. The Brazilian Air Force became the first customer.
The prototype appeared at the 1977 Paris Air Show after an Atlantic crossing with a Bandeirante. Civil approval followed in 1979, and France adopted the Xingu for pilot training from 1983. Those roles explain its combination of an executive cabin and a long second career as a twin-engine trainer.
Embraer · EMB 121 Xingu ↗Systems & details
A T-tail above the propeller wake
Embraer describes the high-mounted horizontal tail as a way to keep it away from direct propeller wash and reduce vibration. Pressurisation was another defining step for the programme. These are features of the aircraft architecture; they do not establish the exact feedback produced by a simulator add-on.
Embraer · EMB 121 Xingu ↗In your simulator
No released simulator product is listed for this aircraft in the developers reviewed. Announced products are excluded.
Manuals & resources
Read the original documentation from the people who created it. Manuals open on their publisher’s website.
Developer documentation
Embraer EMB-121 Xingu — product pagesecure.simmarket.com · Aircraft equipment and developer product details.Aircraft background
Embraer EMB-121 Xingu — aircraft background and systemsembraer.com · Aircraft identity, history and configuration. Embraer EMB-121 Xingu — aircraft background and systemsstatus.embraer.com · Embraer historical chronology, original Xingu.Aircraft documentation
EMB 121 XinguEmbraer · Embraer Historical Center; programme narrative. Conflicting dimensional and power figures in the source are excluded.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 · 2 profile choices
BRsim Designs Embraer EMB121A1 Xingu II
BRsim Designs · Free and Pro · Revision 1 · Partial review
MSFS 2020 · MSFS 2024
Embraer’s Xingu first flew on 22 October 1976.
Embraer EMB-121A1 Xingu II
Free and Pro · Revision 1 · Partial review
MSFS 2020 · MSFS 2024 · X-Plane 12
Embraer’s Xingu first flew on 22 October 1976.
BRsim Designs Embraer EMB121A1 Xingu II
Embraer’s Xingu first flew on 22 October 1976.
Aircraft and simulator scope
- BRsim Designs Embraer EMB121A1 Xingu II · BRsim Designs · MSFS 2020 · Add-on starting point
- BRsim Designs Embraer EMB121A1 Xingu II · BRsim Designs · MSFS 2024 · Add-on starting point
msfs2020 official documented scope reviewed2026-10-11 · msfs2024 official documented scope reviewed2026-10-11
The simulator model and controls
BRsim Designs Embraer EMB121A1 Xingu II is the selected BRsim Designs configuration.
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
The developer identifies the upgraded EMB121A1 with PT6A-135 engines.
Requirements cover MSFS 2020 and 2024; EFB fuel and weight loading is recommended.
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
The developer identifies the upgraded EMB121A1 with PT6A-135 engines.
Requirements cover MSFS 2020 and 2024; EFB fuel and weight loading is recommended.
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
ReviewedBRsim Designs Embraer EMB121A1 Xingu II is the selected BRsim Designs configuration.
Flight controls
InheritedEmbraer’s Xingu first flew on 22 October 1976.
Trim
Not yet reviewedThe profile uses the trim behaviour configured below. Pitch relief is off, with stored authority 0.3; roll authority is 0.
Autopilot and stability
ReviewedAutopilot following is off; the configured spring and load retain the hardware feel.
Equipment
InheritedThe developer identifies the upgraded EMB121A1 with PT6A-135 engines.
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. 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 value0.74 | What it controls and whyThis profile uses reversible-control loading for Embraer EMB-121 Xingu. The baseline spring is 0.74. Its low-speed blend reaches baseline strength at 85 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 170 KIAS. This supplies speed-dependent loading alongside the spring. |
| Force tuning speed/reference | Starting value170 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 value85.0 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 value0.72 | What it controls and whyRoll 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 scale | Starting value1 | 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 47 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 value0.74 | What it controls and whyThis profile uses reversible-control loading for Embraer EMB-121 Xingu. The baseline spring is 0.74. Its low-speed blend reaches baseline strength at 85 KIAS. |
| Profile force gain | Starting value0.8 | What it controls and whyThe aerodynamic-load gain is 0.8 with an indicated-speed reference of 170 KIAS. This supplies speed-dependent loading alongside the spring. |
| Master force gain | Starting value0.85 | What it controls and whyScales overall profile strength while preserving effect balance, subject to device and output limits. |
| Output force limit | Starting value0.55 | What it controls and whyCaps directed-force output. Native spring effects and device limits remain separate. |
| Elevator force scale | Starting value1 | What it controls and whyScales pitch aerodynamic loading; pitch spring travel and trim responses are separate settings. |
| Aileron force scale | Starting value0.72 | What it controls and whyRoll and pitch aerodynamic scales are 0.72 and 1, respectively. They set the aerodynamic axis balance. No custom spring-travel curve is enabled. |
170 KIAS is a selected control-feel reference for BRsim Designs Embraer EMB121A1 Xingu II, not published cruise TAS, V-speeds or an operating limit. q-blend/deadband/drop thresholds are derived engineering estimates.
| Setting | Starting value | What it controls and why |
|---|---|---|
| Force tuning speed/reference | Starting value170 kt | What it controls and whySets the IAS reference for aerodynamic loading. It is an estimate, not published cruise TAS or a flight limit. |
| QSpring Start Knots | Starting value23.8 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 value85.0 kt | What it controls and whySets the IAS where the low-speed blend reaches baseline strength; high-speed stiffening also uses it. |
| Full Speed Ref Knots | Starting value85.0 kt | What it controls and whyA stored parameter in this profile. Its effect depends on the associated feature and control law; it is not a measured aircraft force. |
| Fade Kts | Starting value51.0 | What it controls and whyA stored parameter in this profile. Its effect depends on the associated feature and control law; it is not a measured aircraft force. |
Accessory motion/ground/engine textures inherit existing current estimates; enablement follows reviewed equipment and qualified standard positions, not new actuator or pressure signals.
| Setting | Starting value | What it controls and why |
|---|---|---|
| Gain | Starting value0 | What it controls and whySets texture from observed flap movement; a command without movement does not establish the cue. |
| Gain | Starting value0.12 | What it controls and whySets texture from observed gear movement, separate from aerodynamic and touchdown effects. |
| Undercarriage | Starting value0 | What it controls and whyA stored parameter in this profile. Its effect depends on the associated feature and control law; it is not a measured aircraft force. |
| Gain | Starting value0.12 | What it controls and whySets estimated engine vibration using configured telemetry and response, not measured cockpit vibration. |
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. |
| 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. |
| 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 85 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. |
| Elevator Authority | Starting value0.3 | What it controls and whyThe profile uses the trim behaviour configured below. Pitch relief is off, with stored authority 0.3; 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. |
| 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 value2 | What it controls and whySets the final flap index for detent normalization. UP plus three detents uses maximum index3. |
| Minimum flap index | Starting value2 | 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. |
| Shaker Enabled | Starting valueDisabled | What it controls and whyPermits shaker at supported warning conditions; the switch does not establish aircraft equipment. |
| 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
- Military paints cosmetic; civil transport feel only. Gear/trim installed implementation requires exact manual/check.
- Physical FFB, installed add-on matching and cross-platform runtime acceptance are deferred. No certification or simulator-vendor endorsement is implied.
- Unqualified physical AP following, neutral hold, force trim, native force additions, hardware failures and input compensation are disabled.
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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