IVL C.VI.25

IVL C.VI.25 was a Finnish fighter aircraft designed by IVL. It was a further development of the IVL C.24.

The aircraft made its maiden flight on June 11, 1925. The aircraft was wrecked after a forced landing, due to engine trouble, on December 17, 1925.

The aircraft was under-powered, like its predecessor, and it was not considered possible to further develop the aircraft.

IVL C.VI.25
Class Aircraft
Type Fighter
Manufacturer IVL
Origin Finland
Country Name Origin Year
Finland 1925
Country Name Operational Year Retirement Year
Finland View
ManufacturerName Production From Production To Quantity
IVL 1 View

Role Fighter aircraft
Manufacturer IVL
First flight June 11, 1925
Status Destroyed on December 17, 1925
Primary user Finnish Air Force
Number built 1
Developed from IVL C.24


General characteristics

  • Crew: 1
  • Length: 6.9 m (22 ft 6 in)
  • Wingspan: 9.5 m (31 ft 2 in)
  • Height: ()
  • Max. takeoff weight: 843 kg (1,854 lb)
  • Powerplant: 1 × Siemens-Halske Sh.IIIA radial engine, 119 kW (160 hp)

Performance

  • Maximum speed: 210 km/h (113 knots, 130 mph)

End notes