Start here
A few places to begin, from the aircraft’s story to the people who fly it.
Aircraft and simulator background
The Fox Moth combined components from the Tiger Moth with a purpose-built wooden, plywood-covered fuselage for passenger flying. Designed in late 1931, its prototype flew on 29 January 1932. Gipsy Major power and folding wings accompanied the small transport layout.
de Havilland DH.83 Fox Moth
Developer · Read more ↗Wheel and float configurations
The handbook identifies a Gipsy Major, fixed gear and no flaps. Wheeled aircraft have no steerable tailwheel in this description, while the float fit has its own equipment. The shared manual leaves the Modified model's precise engine and control differences open.
de Havilland DH.83 Fox Moth
Developer · Read more ↗Cockpit and handbook figures
The developer cockpit identifies the stick and elevator-trim lever. The handbook quotes 50 mph takeoff, 66 mph climb, 94 mph cruise and 125 mph dive figures, whose labels and mph units are kept separate.
de Havilland DH.83 Fox Moth
Developer · Read more ↗Meet de Havilland DH.83 Fox Moth
The Fox Moth combined components from the Tiger Moth with a purpose-built wooden, plywood-covered fuselage for passenger flying. Designed in late 1931, its prototype flew on 29 January 1932. Gipsy Major power and folding wings accompanied the small transport layout.
Flight Replicas supplies standard, modified and float versions. Its handbook identifies direct stick controls and an elevator-trim lever; exact engine and control differences in the Modified model are not detailed by that shared handbook.
de Havilland DH.83 Fox Moth
de Havilland → · Explore the family →
de Havilland DH.83 Fox Moth
Developer · de Havilland DH.83 Fox Moth — developer reference ↗Aircraft type designators
No type designator selected for this reference.
History & design
A small passenger aircraft from trainer components
The DH.83 was designed in late 1931 around economical passenger transport. Engine, tail and wing components came from the DH.82, attached to a new wooden fuselage. After its 29 January 1932 first flight, the prototype went to Canada and further examples were assembled in Toronto. British operators used the type for short passenger and feeder flights.
Developer · de Havilland DH.83 Fox Moth — developer reference ↗DH.83 manual; PDF p.2 History; pp.3–4 cockpit and trim; pp.8–9 handbook figures
Systems & details
Wheel and float configurations
The handbook identifies a Gipsy Major, fixed gear and no flaps. Wheeled aircraft have no steerable tailwheel in this description, while the float fit has its own equipment. The shared manual leaves the Modified model's precise engine and control differences open.
Cockpit and handbook figures
The developer cockpit identifies the stick and elevator-trim lever. The handbook quotes 50 mph takeoff, 66 mph climb, 94 mph cruise and 125 mph dive figures, whose labels and mph units are kept separate.
In your simulator
Systems, equipment and documentation for each developer’s aircraft.
Compare simulator versions →MSFS 2020Flight Replicas DH.83 Fox Moth Wheels
Flight Replicas · Released
Flight Replicas DH.83 Fox Moth Wheels
Flight Replicas · Released
MSFS 2020Flight Replicas DH.83 Fox Moth Floats
Flight Replicas · Released
Flight Replicas DH.83 Fox Moth Floats
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 manual
de Havilland DH.83 Fox Moth — developer referencede Havilland DH.83 Fox Moth
DH.83 manual; PDF p.2 History; pp.3–4 cockpit and trim; pp.8–9 handbook figures
Developer · Read the source ↗Developer documentation
de Havilland DH.83 Fox Moth — developer referencede Havilland DH.83 Fox Moth
Original owner post1,June9,2023 package screenshots
Developer · Read the source ↗de Havilland DH.83 Fox Moth — developer referencede Havilland DH.83 Fox Moth
MSFS collection, distinct from legacy hangar
Developer · Read the source ↗de Havilland DH.83 Fox Moth — developer referencede Havilland DH.83 Fox Moth
Aircraft features and simulator package description
Developer · Read the source ↗Read the original documentation from the people who created it. Manuals open on their publisher’s website.
Developer manual
de Havilland DH.83 Fox Moth — developer referenceDeveloper · DH.83 manual; PDF p.2 History; pp.3–4 cockpit and trim; pp.8–9 handbook figuresDeveloper documentation
de Havilland DH.83 Fox Moth — developer referenceDeveloper · Original owner post1,June9,2023 package screenshots de Havilland DH.83 Fox Moth — developer referenceDeveloper · MSFS collection, distinct from legacy hangar de Havilland DH.83 Fox Moth — developer referenceDeveloper · Aircraft features and simulator package descriptionBuilt-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 · 4 profile choices
Flight Replicas DH.83 Fox Moth Wheels
Flight Replicas · Free and Pro · Revision 2 · Inherited starting point
MSFS 2020
A small passenger biplane with a Gipsy Major and a purpose-built wooden cabin.
Flight Replicas DH.83 Fox Moth Floats
Flight Replicas · Free and Pro · Revision 2 · Inherited starting point
MSFS 2020
A small passenger biplane with a Gipsy Major and a purpose-built wooden cabin.
de Havilland DH.83 Fox Moth
Free and Pro · Revision 1 · Partial review
MSFS 2020 · MSFS 2024 · X-Plane 12
A small passenger biplane with a Gipsy Major and a purpose-built wooden cabin.
de Havilland DH.83 Fox Moth Straight Floats
Free and Pro · Revision 1 · Partial review
MSFS 2020 · MSFS 2024 · X-Plane 12
A small passenger biplane with a Gipsy Major and a purpose-built wooden cabin.
de Havilland DH.83 Fox Moth Straight Floats
A small passenger biplane with a Gipsy Major and a purpose-built wooden cabin.
Aircraft and simulator scope
- de Havilland DH.83 Fox Moth Straight Floats · MSFS 2020 · Variant starting point
- de Havilland DH.83 Fox Moth Straight Floats · MSFS 2024 · Variant starting point
- de Havilland DH.83 Fox Moth Straight Floats · 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
A small passenger biplane with a Gipsy Major and a purpose-built wooden cabin.
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
Gipsy Major engine, fixed straight floats and no flaps.
Wheel and float configurations
The handbook identifies a Gipsy Major, fixed gear and no flaps. Wheeled aircraft have no steerable tailwheel in this description, while the float fit has its own equipment. The shared manual leaves the Modified model's precise engine and control differences open.
Cockpit and handbook figures
The developer cockpit identifies the stick and elevator-trim lever. The handbook quotes 50 mph takeoff, 66 mph climb, 94 mph cruise and 125 mph dive figures, whose labels and mph units are kept separate.
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
de Havilland DH.83 Fox Moth Straight Floats: Gipsy Major engine, fixed straight floats and no flaps.
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
ReviewedA small passenger biplane with a Gipsy Major and a purpose-built wooden cabin.
Flight controls
InheritedA small passenger biplane with a Gipsy Major and a purpose-built wooden cabin.
Trim
InheritedThe developer cockpit identifies the stick and elevator-trim lever. Pitch authority 0.3 provides load relief and permitted centre movement; roll authority is 0.
Autopilot and stability
ReviewedAutopilot following is off; the configured spring and load retain the hardware feel.
Equipment
InheritedGipsy Major engine, fixed straight floats and no flaps.
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 value0.74 | What it controls and whyThe handbook identifies a Gipsy Major, fixed gear and no flaps. 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 80 KIAS. This supplies speed-dependent loading alongside the spring. |
| Force tuning speed/reference | Starting value80 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 value0.7 | What it controls and whyRoll and pitch aerodynamic scales are 0.7 and 0.85, respectively. They set the aerodynamic axis balance. No custom spring-travel curve is enabled. |
| Elevator force scale | Starting value0.85 | 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 handbook identifies a Gipsy Major, fixed gear and no flaps. The baseline spring is 0.74. Its low-speed blend reaches baseline strength at 50 KIAS. |
| Profile force gain | Starting value0.8 | What it controls and whyThe aerodynamic-load gain is 0.8 with an indicated-speed reference of 80 KIAS. This supplies speed-dependent loading alongside the spring. |
| Elevator force scale | Starting value0.85 | What it controls and whyScales pitch aerodynamic loading; pitch spring travel and trim responses are separate settings. |
| Aileron force scale | Starting value0.7 | What it controls and whyRoll and pitch aerodynamic scales are 0.7 and 0.85, 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. |
de Havilland DH.83 Fox Moth Straight Floats: No documented in-flight aileron trim. One normalized pitch-relief channel only; roll authority and duplicate TrimFeel centre are zero. Rudder trim does not become lateral stick trim. Estimated pitch/roll trim authorities 0.3/0; 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 value0.3 | What it controls and whyThe developer cockpit identifies the stick and elevator-trim 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. |
de Havilland DH.83 Fox Moth Straight Floats: 80 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 value80 kt | What it controls and whySets the IAS reference for aerodynamic loading. It is an estimate, not published cruise TAS or a flight limit. |
The selected float fit disables wheel-braking, tire-thump and retracting-gear cues; no amphibious wheels are inferred.
| Setting | Starting value | What it controls and why |
|---|---|---|
| Gain | Starting value0.08 | What it controls and whyThe selected float fit disables wheel-braking, tire-thump and retracting-gear cues; no amphibious wheels are inferred. |
| Gain | Starting value0 | What it controls and whyThe selected float fit disables wheel-braking, tire-thump and retracting-gear cues; no amphibious wheels are inferred. |
| Gain | Starting value0 | What it controls and whyThe selected float fit disables wheel-braking, tire-thump and retracting-gear cues; no amphibious wheels are inferred. |
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. |
| 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. |
| 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. |
| 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. |
| 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 value0.06 | What it controls and whySets gear-bump texture during ground motion, separate from touchdown impact. |
| Gain | Starting value0.16 | 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. |
Limits and open questions
- de Havilland DH.83 Fox Moth Straight Floats 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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