The Daedalus BS214 comes with two versions (as of 1 June 2026): a native MSFS 2020 version and a native MSFS 2024 version, one for each simulator.
The native MSFS 2024 version includes:
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Pre-flight inspection, including checklist
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Chocks and covers
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Wear and tear simulation for supported systems
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CFD simulation
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MSFS 2024 avatars for pilot, co-pilot and passengers
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EFB in the 3D cockpit
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Baggage loader displaying different baggage objects according to the selected load
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Wwise sounds converted for MSFS 2024
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Presets for different avionics configurations
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Two-stage Enter/Exit Aircraft functionality, allowing doors to remain open while in interior, exterior, or preflight states
The Daedalus BS214 is a prototype experimental twin-engine aircraft. It features a tricycle high-wing design and accommodates two seats, boasting STOL bush flying capabilities.
The aircraft was named in honour of Daedalus (Δαίδαλος), the famous ancient Greek architect and engineer who, according to Greek mythology, was the first man who built wings that he and his son Icarus used to escape from Crete. Icarus (Ίκαρος) was the first man to fly in the sky.
The aircraft requires just 100 metres of ground roll for take-off and landing. It is powered by two Rotax 915iS engines, each producing 141 hp. These engines deliver excellent performance during cruising and particularly in climb rates. The right engine rotates anticlockwise, meaning the aircraft has no critical engine. Controlling the aircraft in the event of an engine failure (whether left or right) is straightforward.
The aircraft is capable of flying in FIKI (Flight Into Known Icing) conditions, thanks to its anti-ice protection system. The windshield, propellers and leading edges of the wings and the tail are electrically heated to prevent ice build-up. A third external 70V 70A alternator, installed on the right engine, powers the (LPED) heated leading edges. The Pitot tube and stall horn are also electrically heated.
The cockpit is designed for comfort, measuring 1.35 metres in width and 1.15 metres in height, making it spacious for both the pilot and co-pilot.
An automatic A/C climate control system, installed on the left engine, ensures a comfortable and pleasant environment in all weather conditions. The large windshield, along with side and rear windows, provides excellent visibility. The design of the aircraft prioritises safety, performance, comfort and ergonomics.
The Daedalus BS214 was designed and built using NASA's OpenVSP software (airfoils, fuselage, tail, empennage, dimensions, CFD, lift polar, drag polar etc.). Real-world data and formulas were employed to calculate all necessary specifications, such as weight, surface areas, dimensions etc. The 3D model aligns precisely with the flight model in MSFS.
For the best experience, it is recommended to fly it in VR, if possible.
See the Detailed Description below for all the aircraft features!