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DMRI “Evia” BC II

15.1k Rodrigo110  7.5 years ago

Important Note - only use on High Physics, using on low physics may result in the propellers exploding

The DMRI “Evia” BC II was a long range cargo aircraft designed for the Greek Air Force in 1957. It was powered by Quad “Rolls Royce Griffin” Dual shaft 1700HP Turboprop engines and had a cruising speed of 245mph (394km/h), though the “Evia” reached top speed at high altitude. The “Evia” was armoured, and also carried flares in case of attack from hostiles, but did not carry any weaponry, and instead relied on its armour and escort (usually present) to protect itself.

Controls

  • Pitch for Elevator
  • Roll for Ailerons
  • Trim for Trim
  • VTOL Down to open cargo bay door
  • AG 1 for cargo bay warning lights
  • AG 2 for internal cargo bay overhead lights
  • AG 8 for navigation lights

Control Notes

  • Trim recommended to maintain altitude in-flight (35-55%)
  • Only use on high physics, using on low physics may result in the propellers exploding

Specifications

x4 1700HP “Rolls Royce Griffin” Dual Shaft Turboprop Engines

General Characteristics

  • Created On iOS
  • Wingspan 93.7ft (28.6m)
  • Length 64.8ft (19.8m)
  • Height 15.5ft (4.7m)
  • Empty Weight 16,599lbs (7,529kg)
  • Loaded Weight 26,370lbs (11,961kg)

Performance

  • Horse Power/Weight Ratio 0.257
  • Wing Loading 17.0lbs/ft2 (82.9kg/m2)
  • Wing Area 1,553.4ft2 (144.3m2)
  • Drag Points 23284

Parts

  • Number of Parts 431
  • Control Surfaces 6
  • Performance Cost 1,619