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Research aircraft and systems

Find aircraft background, systems descriptions and manuals for the aircraft you are researching. Each note keeps its source and version context close by.

Simulator manuals describe the developer’s implementation. Aircraft background is research-based; pilot accounts describe an individual’s experience. Coverage here is limited to the selected notes and linked resources, not the full contents of every manual.
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Cirrus SR22 ↗Simulator documentation

Cirrus SR22 · Laminar Research · X-Plane 12

Side controls with conventional trim

The Laminar guide identifies the represented aircraft as an SR22T and describes its side controls, pitch-trim indication and relief of sustained fore-and-aft pressure. The side controls are mechanically connected.

Archived simulator manual; installed package revision not observed · PDF pp.9,18

SourceCirrus SR 22 POH ↗Laminar Research
Cirrus SR22 ↗Simulator documentation

Cirrus SR22 · TorqueSim · TorqueSim · X-Plane 12

Panel generation and simulator version matter

TorqueSim's SR22 history records changes to trim authority and autopilot/control behaviour. Version 2.1 moved the G1000 aircraft to the X-Plane 12.1 X1000 and excludes older simulator versions; 2.1.1 removed the Gizmo dependency. The developer documents G1000 and Entegra products separately, with their release histories.

SR22 G1000 v2.1.1 · v2.0.0, v2.0.2, v2.1.0-2.1.1

Cirrus Vision SF50 ↗Simulator documentation

Cirrus Vision SF50 · Laminar Research · X-Plane 12

The Vision Jet's documented configuration

Laminar's SF50 guide covers flight controls, autopilot and trim/configuration indications. It covers the bundled Vision Jet's equipment; later real-aircraft upgrades and other developers' packages have separate references.

Archived simulator manual; installed package revision not observed · PDF pp.7,46-47

SourceCirrus Vision SF50 POH ↗Laminar Research
Cirrus Vision SF50 ↗Simulator documentation

Cirrus Vision SF50 · Laminar Research · X-Plane 11

The Vision Jet's documented configuration

Laminar's SF50 guide covers flight controls, autopilot and trim/configuration indications. It covers the bundled Vision Jet's equipment; later real-aircraft upgrades and other developers' packages have separate references.

Archived simulator manual; installed package revision not observed · PDF pp.7,46-47

SourceCirrus Vision SF50 POH ↗Laminar Research
Comco Ikarus C42B ↗Research-based aircraft background

Comco Ikarus C42B

The C42B is a light high-wing aircraft with fixed tricycle landing gear and a Rotax powerplant. Comco’s catalogue lists both 80-hp 912 UL and 100-hp 912 ULS configurations, with model and weight approvals kept separate from the later C42 C/CS.

The manufacturer’s handbook identifies aileron pushrods, an elevator pushrod and rudder cables. It also documents an elevator trim tab, mechanical flap control and a brake lever. These linkages give the cockpit a direct mechanical-control arrangement around its light-aircraft structure.

C42B LTF-UL-2019 issue 1, 540 kg configuration.

Couzinet 71 Arc-en-Ciel ↗Research-based aircraft background

Couzinet 71 Arc-en-Ciel

The Couzinet 71 Arc-en-Ciel has three piston engines and fixed tailwheel landing gear. Restauravia describes its flight model as approximate, with historical questions still unresolved. The cockpit checklist includes pitch trim; two flight-controller-labelled instruments display turn and slip.

Couzinet 71 Arc-en-Ciel

Dassault Rafale ↗Research-based aircraft background

Dassault Rafale

The Rafale is a twin-engine canard-delta combat aircraft developed for French air-force and naval use. AzurPoly’s background section dates the Rafale A technology demonstrator’s first flight to 4 July 1986 and the full programme’s launch to 1988. The close-coupled canards and delta wing are part of an airframe built around electronic flight control and several mission roles.

AzurPoly’s Rafale C for MSFS 2024 uses its own fly-by-wire implementation, with load-factor demand and protections that respond to configuration and stores. Automatic pitch and roll trim belong to its normal digital law. Canards, elevons and slats move as part of that control system rather than following a conventional airliner flap schedule.

Manual history · Rafale family · AzurPoly Rafale C

Dauphin AS365 / HH-65 ↗Simulator documentation

AS365 N2 / HH-65A · Taog's Hangar · MSFS 2024

Two helicopters, two automatic flight-control systems

Taog's AS365N2 uses the AP155/CDV85 installation, while the HH-65A has a different four-axis AFCS and flight-director system. Their upper modes can take control of the collective as well as the cyclic. The manual explains collective alignment, trim-release behaviour and the accommodations for spring-centred desktop controls. The control bindings differ by aircraft variant.

MSFS2024; manual V1 contains references to update 1.2 · PDF pp.8,72,76-77,81; chapters 13-15

SourceDownload manual ↗Taog's Hangar
Dauphin AS365 / HH-65 ↗Simulator documentation

AS365 N2 / HH-65A · Taog's Hangar · MSFS 2024

Variant-specific hardware controls

The binding guide publishes separate input events for the Dauphin and HH-65. Axis values use the documented -16384 to 16384 range, and momentary buttons require both press and release actions. Similar display names do not make the two variants' events interchangeable. The guide lists each variant's event identifiers separately.

MSFS2024; keybinding guide V1.0 · PDF pp.1-4 and Trim Release rows

DoubleEnder ↗Simulator documentation

Got Friends DoubleEnder · Got Friends · MSFS 2020 · MSFS 2024

Trim and ground configuration

Pitch trim moves the horizontal stabiliser. Inline Rotax engines, 35-inch tyres and a free-castering tailwheel define the represented configuration, with an optional Type 400A flight director.

PDF2/4/16/20; PDF20 image reviewed