Meet Embraer Phenom 100
The Phenom 100 is the EMB-500 light business jet. The NTSB’s description of the original model identifies two Pratt & Whitney Canada PW617F-E engines and a Garmin-based automatic-flight installation. Its cockpit includes a stall-warning and protection system with AoA sensors, a warning computer and an actuator connected to the elevator control system.
The protection system provides aural warning, low-speed awareness indications and a stick-pusher action. Its thresholds change with the aircraft’s ice-protection configuration.
History & design
The Phenom 100 gains its original approval
ANAC presented the Embraer 500 type certificate on 9 December 2008. The Phenom 100's review had begun in 2005 under the former Brazilian authority before continuing at ANAC. The regulator describes a programme involving more than 700 documents, inspections and tests. This establishes the original aircraft generation, before the later EV and EX developments and their revised systems.
ANAC · ANAC certifica aeronave Embraer 500 - Phenom 100 ↗A later flight-deck generation
Embraer’s Phenom 100EX page identifies Garmin G3000 Prodigy Touch and runway-overrun awareness equipment. Those details identify the EX development within the family; Cockspur PH100 and Carenado E50P are separately named simulator renditions.
www.embraer.com · Embraer Phenom 100 — aircraft background and systems ↗Embraer current 100EX, later variant scope.
Systems & details
Warning and protection on the original EMB-500
The NTSB report separates the aural warning and airspeed-display cues from the actuator that pushes the column forward. It also explains that ice-protection selection changes the warning/protection schedule. These are configuration-dependent aircraft systems.
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
E50P PHENOM 100 HD SERIES XPLANE 11 – Carenadowww.carenado.com · Aircraft equipment and developer product details. Cockspur PH100 – Cockspurcockspur.eu · Aircraft equipment and developer product details. NTSB AAR-16/01 — Embraer EMB-500, Gaithersburgwww.ntsb.gov · NTSB AAR-16/01, original EMB-500 systems sections 1.3.1–1.3.4.Aircraft background
Embraer Phenom 100 — aircraft background and systemswww.embraer.com · Embraer current 100EX, later variant scope.Aircraft documentation
ANAC certifica aeronave Embraer 500 - Phenom 100ANAC · ANAC notice dated 9 December 2008; original Embraer 500 type approval.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
Carenado E50P Phenom 100
Carenado · Free and Pro · Revision 1 · Partial review
X-Plane 11
The Phenom 100 is the EMB-500 light business jet.
Cockspur PH100 Phenom 100
Cockspur · Free and Pro · Revision 1 · Partial review
MSFS 2020
The Phenom 100 is the EMB-500 light business jet.
Embraer Phenom 100
Free and Pro · Revision 1 · Partial review
MSFS 2020 · MSFS 2024 · X-Plane 12
The Phenom 100 is the EMB-500 light business jet.
Embraer Phenom 100
The Phenom 100 is the EMB-500 light business jet.
Aircraft and simulator scope
- Embraer Phenom 100 · MSFS 2020 · Variant starting point
- Embraer Phenom 100 · MSFS 2024 · Variant starting point
- Embraer Phenom 100 · X-Plane 12 · Variant starting point
Embraer Phenom 100 generic civil family/configuration; physical clauses from the preserved developer description. Exact proprietary equipment, installed package and hardware acceptance are outside this scope. · NTSB AAR-16/01 sections 1.3–1.3.2 describe original EMB-500/Phenom 100 equipment, including a 2009 aircraft. These are physical background facts, not current Cockspur system/telemetry validation, Phenom 100EV/300 applicability or simulator availability evidence.
The simulator model and controls
The Phenom 100 is the EMB-500 light business jet.
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 NTSB describes the original EMB-500/Phenom 100 as a low-wing T-tail aircraft with rear-mounted turbofans and fully retractable tricycle landing gear. Its 2009 example used PW617F-E engines.
For the original EMB-500, the report describes an aural stall warning and a rotary electromechanical stick-pusher actuator connected to the elevator control system.
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 NTSB describes the original EMB-500/Phenom 100 as a low-wing T-tail aircraft with rear-mounted turbofans and fully retractable tricycle landing gear. Its 2009 example used PW617F-E engines.
For the original EMB-500, the report describes an aural stall warning and a rotary electromechanical stick-pusher actuator connected to the elevator control system.
The original EMB-500 Garmin integrated autopilot is designed to disengage when it receives a stall-warning signal from the stall-warning/protection computer.
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 Phenom 100 is the EMB-500 light business jet.
Flight controls
Not yet reviewedThe Phenom 100 is the EMB-500 light business jet.
Trim
Not yet reviewedThe 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
ReviewedThe NTSB describes the original EMB-500/Phenom 100 as a low-wing T-tail aircraft with rear-mounted turbofans and fully retractable tricycle landing gear. Its 2009 example used PW617F-E engines.
Speeds and limits
InheritedThe indicated-speed references set the profile response scale; they are separate from aircraft operating limits.
Simulator integration
Not yet 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 value0.74 | What it controls and whyThis profile uses reversible-control loading for Embraer Phenom 100. The baseline spring is 0.74. Its low-speed blend reaches baseline strength at 105 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 210 KIAS. This supplies speed-dependent loading alongside the spring. |
| Force tuning speed/reference | Starting value210 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 value105 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 value0.75 | What it controls and whyRoll and pitch aerodynamic scales are 0.75 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 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 value0.74 | What it controls and whyThis profile uses reversible-control loading for Embraer Phenom 100. The baseline spring is 0.74. Its low-speed blend reaches baseline strength at 105 KIAS. |
| Profile force gain | Starting value0.8 | What it controls and whyThe aerodynamic-load gain is 0.8 with an indicated-speed reference of 210 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 value0.75 | What it controls and whyRoll and pitch aerodynamic scales are 0.75 and 1, respectively. They set the aerodynamic axis balance. No custom spring-travel curve is enabled. |
Embraer Phenom 100: 210 indicated knots is the inherited control-feel reference; it is not cruise TAS, a flight limit or a measured load threshold. Speed scheduling remains an editable estimate.
| Setting | Starting value | What it controls and why |
|---|---|---|
| Force tuning speed/reference | Starting value210 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 value29.4 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 value105 kt | What it controls and whySets the IAS where the low-speed blend reaches baseline strength; high-speed stiffening also uses it. |
Embraer Phenom 100: exact trim axes, mechanism and portable telemetry contract are unresolved in the inspected source. Trim feel, trim relief, force trim and hydraulic centering are disabled for this generic choice.
| Setting | Starting value | What it controls and why |
|---|---|---|
| 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. |
| Autopilot follow | Starting valueDisabled | What it controls and whyAutopilot following is off; the configured spring and load retain the hardware feel. |
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 value0.04 | 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 value0.55 | 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 105 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. |
| 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. |
| 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 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 value3 | 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 valueDisabled | What it controls and whyEnables engine cues with nonzero settings and valid running-engine telemetry. |
| Gain | Starting value0 | What it controls and whySets estimated engine vibration using configured telemetry and response, not measured cockpit vibration. |
| Enabled | Starting valueEnabled | What it controls and whyEnables accessory cues with configured strengths and observed accessory movement. |
| Gain | Starting value0 | What it controls and whySets texture from observed flap movement; a command without movement does not establish the cue. |
| Gain | Starting value0.025 | What it controls and whySets texture from observed gear movement, separate from aerodynamic and touchdown effects. |
Limits and open questions
- The physical control and accessory configuration needs an aircraft manual; the source product cold-and-dark requirement is not transferred to a universal profile.
- Generic airframe starting scope; exact installed add-on matching, custom signals and device operation remain unqualified.
- Force magnitudes and scheduling are inherited estimates. No physical calibration or certification is claimed.
- The NTSB report supplies original-aircraft equipment background only. Pusher force/activation thresholds are not copied into this profile; trim geometry, normal primary-control-force transmission and current simulator servo signals remain unresolved.
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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