VSKYLABS 510X-ER VLJ
VSKYLABS 510X-ER VLJ: Mechanical/tab-assisted controls motivate aerodynamic yoke loading.
X-Plane 12 · Revision 3
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Catalogue programme-20261022-v1
The full catalogue contains 1641 profile choices; 1564 declare an MSFS 2020, MSFS 2024 or X-Plane 12 target. Profile choices may cover multiple editions of one aircraft.
VSKYLABS 510X-ER VLJ: Mechanical/tab-assisted controls motivate aerodynamic yoke loading.
X-Plane 12 · Revision 3
Aircraft and full profile explanation →VSKYLABS 902eX-NTR: The spring and damping supply supported testbed-cyclic resistance.
X-Plane 12 · Revision 2
Aircraft and full profile explanation →VSKYLABS 902X-NTR: The spring and damping supply supported testbed-cyclic resistance.
X-Plane 12 · Revision 3
Aircraft and full profile explanation →VSKYLABS Aeroprakt A22-LS: The A22-LS's light manual controls motivate an airspeed-dependent stick response while retaining the profile's own centering balance.
X-Plane 12 · Revision 3
Aircraft and full profile explanation →VSKYLABS Aeropro EuroFOX A220: The flaperon mixer connects lateral control and flap function; the profile approximates the resulting reversible stick resistance.
X-Plane 12 · Revision 3
Aircraft and full profile explanation →VSKYLABS Aeropro EuroFOX A220 STOL: The flaperon mixer connects lateral control and flap function; the profile approximates the resulting reversible stick resistance.
X-Plane 12 · Revision 3
Aircraft and full profile explanation →VSKYLABS Aeropro EuroFOX A240: The flaperon mixer connects lateral control and flap function; the profile approximates the resulting reversible stick resistance.
X-Plane 12 · Revision 3
Aircraft and full profile explanation →VSKYLABS Aeros-2 Trike: Symmetric centering and damping provide nominal bar resistance without claiming that the flex-wing bar behaves like a conventional elevator control.
X-Plane 12 · Revision 3
Aircraft and full profile explanation →VSKYLABS B-8M Gyrocopter: Nominal centering and damping approximate rotor-head control; this revision also retains a selected speed-dependent directed load.
X-Plane 12 · Revision 3
Aircraft and full profile explanation →VSKYLABS C-47 Skytrain NXG: Manual primary controls motivate airspeed-dependent yoke resistance.
X-Plane 12 · Revision 5
Aircraft and full profile explanation →VSKYLABS C-47 Skytrain NXG Skis: Manual primary controls motivate airspeed-dependent yoke resistance.
X-Plane 12 · Revision 3
Aircraft and full profile explanation →VSKYLABS Cicare-8: The selected light cyclic response is nominal; cockpit friction does not establish hydraulic boost or an automatic centre-position command.
X-Plane 12 · Revision 2
Aircraft and full profile explanation →VSKYLABS Contraventus: The selected resistance accompanies an unconventional rudder-controlled roll interface.
X-Plane 12 · X-Plane 11 · Revision 1
Aircraft and full profile explanation →VSKYLABS Contraventus XP12: The selected resistance accompanies an unconventional rudder-controlled roll interface.
X-Plane 12 · Revision 3
Aircraft and full profile explanation →VSKYLABS DC-3 Airliner NXG: Reversible yoke loading follows the manually operated transport controls.
X-Plane 12 · Revision 4
Aircraft and full profile explanation →VSKYLABS DC-3 Airliner NXG Skis: Reversible yoke loading follows the manually operated transport controls.
X-Plane 12 · Revision 3
Aircraft and full profile explanation →VSKYLABS Dorand D.20: Nominal cyclic centering accompanies a simulator interpretation of an unflown prototype.
X-Plane 12 · Revision 3
Aircraft and full profile explanation →VSKYLABS Dynali H3 EasyFlyer: The cyclic spring and damping approximate mechanical push-pull controls.
X-Plane 12 · Revision 2
Aircraft and full profile explanation →VSKYLABS F-19: The spring supplies the selected hypothetical electronic-control response.
X-Plane 12 · Revision 3
Aircraft and full profile explanation →VSKYLABS F-19 concept: The spring supplies the selected hypothetical electronic-control response.
X-Plane 12 · Revision 1
Aircraft and full profile explanation →VSKYLABS FA Tensor 600X: The spring supplies gyroplane control resistance independently of wing-based speed loading.
X-Plane 12 · Revision 3
Aircraft and full profile explanation →VSKYLABS Flight Design CTLS: The stabilator/flaperon arrangement motivates reversible stick resistance.
X-Plane 12 · Revision 4
Aircraft and full profile explanation →VSKYLABS Guimbal Cabri G2: The cyclic response approximates unboosted mechanical controls.
X-Plane 12 · Revision 4
Aircraft and full profile explanation →VSKYLABS Heinkel He-162: Mechanical linkage motivates airspeed-sensitive stick resistance.
X-Plane 12 · Revision 3
Aircraft and full profile explanation →New aircraft, useful sources and improvements to AirframeDB. Occasional updates, when there’s something to share.