MSFS 2024 Status:
Investigating Marketplace
Support the site - donate!

Daedalus BS214

Arantis Simulations

GA GENERAL AVIATIONLIGHT TWIN ENGINEHIGH WINGS BUSH STOLANTI ICE FIKIGLASS COCKPIT G3X GTN750

5/5 (3)


The Daedalus BS214 is a prototype experimental twin-engine aircraft. It features a tricycle high-wing design and accommodates two seats, boasting Bush STOL capabilities.

The aircraft was named in honor of Daedalus, the famous ancient Greek architect and engineer who, according to Greek mythology, was the first man who build wings that he and his son Icarus used to escape from Crete. Icarus was the first man flew in the sky.

The aircraft requires just 100 meters of ground roll for takeoff 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 counterclockwise, 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 buildup. 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 meters in width and 1.15 meters 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 prioritizes 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.

For the best experience, it is recommended to fly it in VR, if possible.

KEY FEATURES 3D MODEL

  • 3D model matching the flight model
  • Modern Propeller Model implementing propeller lift and drag
  • Physically Based Rendering (PBR) materials for a perfect visual result
  • Highly detailed textures for special clarity including decals
  • Numerous animations, including:    - Aircraft doors    - Landing gear flex    - All cockpit switches, buttons, knobs and circuit breakers    - Fully animated seats (useful in VR) & armrest    - Sunvisors
  • Realistic backlighting and floodlighting
  • Realistic exterior lighting
  • Detailed checklist (non interactive, no preflight inspection)
  • One livery in 5 colors (blue, red, green, yellow, white)
  • Integration of native MSFS features such as icing and rain effects SYSTEMS
  • G3X Touch Avionics by Working Title (PFD & MFD)
  • Variants with PMS50-GTN750 or TDSSim-GTN750Xi VC integration (replacing the MFD) which require separately purchased and installed third-party software; without it, the GTN750 units will not appear.
  • GMC307 autopilot with Yaw Damper
  • Backup Attitude & Speed instrument
  • Trim & Cabin temperature instrument
  • Anti-Ice System
  • Oxygen System
  • Simulated circuit breakers
  • Automatic A/C system & cabin temperature initialization
  • Full PFD warning system
  • Simulation of engine stress and damage due to exceedances of RPM or temperature limits (CHT, Coolant, and EGT)
  • Airspeed indicator failure under specific conditions EFFECTS
  • Exhaust heat & smoke effect
  • Engine fire smoke effect MANUAL
  • PDF detailed manual
  • PDF hardware key bindings

Note: Please refer to the manual for detailed information on aircraft operation and engine limitations. Manual and changelog are included in the Documentation folder. Manual is also available online on the product page at www.justflight.com

The Daedalus BS214 is a hypothetical 2-seat, twin-engine experimental high-performance STOL (short take-off and landing) aircraft. It was developed in the spirit of Daedalus, a Greek mythological figure who crafted wings of feathers and wax for him and his son Icarus to escape the Island of Crete. As per mythology, the two were the first mortals to fly. The Daedalus BS214, powered by twin piston engines, is optimized for STOL performance. It requires just 328 feet (100 meters) of ground roll to take-off, and a similarly short distance for landing.

The Daedalus BS214 boasts modern composite construction, a STOL-optimized high wing design, a standard empennage, and a fixed tricycle undercarriage. The spacious cockpit features side-by-side seating, a high-visibility canopy, dual controls, and modern avionics with large color flat-panel displays. It is powered by two counterrotating 4-stroke, 4-cylinder Rotax 915iS engines, each of which delivers up to 141 horsepower to a 3-blade composite constant-speed propeller. The Daedalus was built for adventure flying. In addition to its STOL-optimized design, it has an advanced anti-ice protection system allowing it to operate in FIKI (flight into known icing) conditions. This system is powered by a third 70-volt, 70-amp alternator, externally mounted on the right engine. The pitot tube and stall horn are also electrically heated.

Specifications


CRUISE SPEED155 KTAS
ENGINERotax 915iSc3-C24 141HP x2 (CW-CCW)
MAX ALTITUDE23000 FT
RANGE1007 NM
EMPTY WEIGHT1125 LBS
MAX WEIGHT1970 LBS
FUEL CAPACITY76 USG
LENGTH26.4 FT
WINGSPAN36.1 FT

VERSION 1.0.0 RELEASED NOVEMBER 21, 2025

Please refer to the changelog located in the Documentation folder.