Start here
A few places to begin, from the aircraft’s story to the people who fly it.
Aircraft and simulator background
The Moth Minor developed the Moth touring and training role into a low-wing monoplane. Wooden construction and folding wings accompanied the two-seat layout. The prototype flew on 22 June 1937; Coupe versions added enclosed hinged cockpit tops.
de Havilland DH.94 Moth Minor
Developer · Read more ↗Trim, flaps and ground equipment
The manual identifies direct stick controls, a left-side pitch-trim lever and a flap lever. A fixed-pitch Gipsy engine and fixed tailwheel gear complete the configuration; the manual specifies no steerable tailwheel. Wing folding is a ground feature.
de Havilland DH.94 Moth Minor
Developer · Read more ↗Handbook speed and engine limits
The handbook lists 100–105 mph cruise and calls for flap operation below 80 mph. Its 2,600 RPM diving limit concerns engine speed.
de Havilland DH.94 Moth Minor
Developer · Read more ↗Meet de Havilland DH.94 Moth Minor
The Moth Minor developed the Moth touring and training role into a low-wing monoplane. Wooden construction and folding wings accompanied the two-seat layout. The prototype flew on 22 June 1937; Coupe versions added enclosed hinged cockpit tops.
Flight Replicas represents restored open-cockpit and Coupe aircraft with modernised communications and a two-axis autopilot. A stick, pitch-trim lever and flap control remain part of the documented cockpit.
de Havilland DH.94 Moth Minor
de Havilland → · Explore the family →
de Havilland DH.94 Moth Minor
Developer · de Havilland DH.94 Moth Minor — developer reference ↗Aircraft type designators
No type designator selected for this reference.
History & design
Moving from biplanes to a low-wing trainer
De Havilland designed the DH.94 to replace the older biplane Moth line with a wooden low-wing aircraft. Geoffrey de Havilland flew the prototype on 22 June 1937. Open cockpits were standard, with enclosed Coupe versions later offering a different cabin arrangement. Folding wings reduced its hangar footprint.
Developer · de Havilland DH.94 Moth Minor — developer reference ↗DH.94 manual; PDF p.2 History; pp.3–5 controls; pp.11–12 handbook figures
Systems & details
Trim, flaps and ground equipment
The manual identifies direct stick controls, a left-side pitch-trim lever and a flap lever. A fixed-pitch Gipsy engine and fixed tailwheel gear complete the configuration; the manual specifies no steerable tailwheel. Wing folding is a ground feature.
Handbook speed and engine limits
The handbook lists 100–105 mph cruise and calls for flap operation below 80 mph. Its 2,600 RPM diving limit concerns engine speed.
In your simulator
Systems, equipment and documentation for each developer’s aircraft.
MSFS 2020Flight Replicas DH.94 Moth Minor
Flight Replicas · Released
Flight Replicas DH.94 Moth Minor
Flight Replicas · Released
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.
Developer documentation
de Havilland DH.94 Moth Minor — developer referencede Havilland DH.94 Moth Minor
Aircraft features and simulator package description
Developer · Read the source ↗de Havilland DH.94 Moth Minor — developer referencede Havilland DH.94 Moth Minor
MSFS collection, distinct from legacy hangar
Developer · Read the source ↗Developer manual
de Havilland DH.94 Moth Minor — developer referencede Havilland DH.94 Moth Minor
DH.94 manual; PDF p.2 History; pp.3–5 controls; pp.11–12 handbook figures
Developer · Read the source ↗Read the original documentation from the people who created it. Manuals open on their publisher’s website.
Developer documentation
de Havilland DH.94 Moth Minor — developer referenceDeveloper · Aircraft features and simulator package description de Havilland DH.94 Moth Minor — developer referenceDeveloper · MSFS collection, distinct from legacy hangarDeveloper manual
de Havilland DH.94 Moth Minor — developer referenceDeveloper · DH.94 manual; PDF p.2 History; pp.3–5 controls; pp.11–12 handbook figuresBuilt-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
Flight Replicas DH.94 Moth Minor
Flight Replicas · Free and Pro · Revision 2 · Inherited starting point
MSFS 2020
A wooden low-wing two-seater with folding wings, offered with open and enclosed cockpits.
de Havilland DH.94 Moth Minor
Free and Pro · Revision 1 · Partial review
MSFS 2020 · MSFS 2024 · X-Plane 12
A wooden low-wing two-seater with folding wings, offered with open and enclosed cockpits.
Flight Replicas DH.94 Moth Minor
A wooden low-wing two-seater with folding wings, offered with open and enclosed cockpits.
Aircraft and simulator scope
- Flight Replicas DH.94 Moth Minor · Flight Replicas · MSFS 2020 · Add-on starting point
The simulator model and controls
Flight Replicas DH.94 Moth Minor is the selected Flight Replicas configuration.
How this profile feels
Spring resistance builds with the selected airspeed response. A separate aerodynamic term adds speed-dependent control load.
Valid trim provides the configured pressure relief. Autopilot following is off.
Aircraft and configuration
The Moth Minor developed the Moth touring and training role into a low-wing monoplane. Wooden construction and folding wings accompanied the two-seat layout. The prototype flew on 22 June 1937; Coupe versions added enclosed hinged cockpit tops.
Trim, flaps and ground equipment
The manual identifies direct stick controls, a left-side pitch-trim lever and a flap lever. A fixed-pitch Gipsy engine and fixed tailwheel gear complete the configuration; the manual specifies no steerable tailwheel. Wing folding is a ground feature.
Handbook speed and engine limits
The handbook lists 100–105 mph cruise and calls for flap operation below 80 mph. Its 2,600 RPM diving limit concerns engine speed.
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.
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
InheritedFlight Replicas DH.94 Moth Minor is the selected Flight Replicas configuration.
Flight controls
InheritedA wooden low-wing two-seater with folding wings, offered with open and enclosed cockpits.
Trim
InheritedThe manual identifies direct stick controls, a left-side pitch-trim lever and a flap lever. Pitch authority 0.3 provides load relief and permitted centre movement; roll authority is 0.
Autopilot and stability
InheritedAutopilot following is off; the configured spring and load retain the hardware feel.
Equipment
InheritedThe Moth Minor developed the Moth touring and training role into a low-wing monoplane. Wooden construction and folding wings accompanied the two-seat layout. The prototype flew on 22 June 1937; Coupe versions added enclosed hinged cockpit tops.
Speeds and limits
InheritedThe indicated-speed references set the profile response scale; they are separate from aircraft operating limits.
Simulator integration
InheritedThe profile targets msfs2020. 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 whyThe manual identifies direct stick controls, a left-side pitch-trim lever and a flap lever. The baseline spring is 0.74. Its low-speed blend reaches baseline strength at 50 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 85 KIAS. This supplies speed-dependent loading alongside the spring. |
| Force tuning speed/reference | Starting value85 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 value50 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 value0.68 | What it controls and whyRoll and pitch aerodynamic scales are 0.68 and 0.82, respectively. They set the aerodynamic axis balance. No custom spring-travel curve is enabled. |
| Elevator force scale | Starting value0.82 | 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 valueEnabled | 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 whyThe manual identifies direct stick controls, a left-side pitch-trim lever and a flap lever. The baseline spring is 0.74. Its low-speed blend reaches baseline strength at 50 KIAS. |
| Spring deadband | Starting value0.04 | What it controls and whySets travel around the centre before the baseline spring resists. Smaller values engage it sooner. |
| Profile force gain | Starting value0.8 | What it controls and whyThe aerodynamic-load gain is 0.8 with an indicated-speed reference of 85 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. |
| 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. |
| QSpring Start Knots | Starting value15 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 value50 kt | What it controls and whySets the IAS where the low-speed blend reaches baseline strength; high-speed stiffening also uses it. |
| Force tuning speed/reference | Starting value85 kt | What it controls and whySets the IAS reference for aerodynamic loading. It is an estimate, not published cruise TAS or a flight limit. |
| 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 50 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. |
| Aileron force scale | Starting value0.68 | What it controls and whyRoll and pitch aerodynamic scales are 0.68 and 0.82, respectively. They set the aerodynamic axis balance. No custom spring-travel curve is enabled. |
| Elevator force scale | Starting value0.82 | What it controls and whyScales pitch aerodynamic loading; pitch spring travel and trim responses are separate settings. |
| Output force limit | Starting value0.55 | What it controls and whyCaps directed-force output. Native spring effects and device limits remain separate. |
| 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 valueEnabled | 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 manual identifies direct stick controls, a left-side pitch-trim lever and a flap lever. Pitch authority 0.3 provides load relief and permitted centre movement; 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 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. |
| 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. |
| Gain | Starting value0.12 | 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 value0.025 | What it controls and whySets texture from observed flap movement; a command without movement does not establish the cue. |
| Gain | Starting value0 | What it controls and whySets texture from observed gear movement, separate from aerodynamic and touchdown effects. |
Limits and open questions
- Force magnitudes and speed references are engineering estimates. Installed telemetry and physical acceptance remain deferred.
- Only documented editions are targeted; a matching definition is not current package acceptance.
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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