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.

C.VI.25
General information
Type	Fighter aircraft
Manufacturer	IVL
Status	Destroyed on December 17, 1925
Primary user	Finnish Air Force
Number built	1
History
First flight	June 11, 1925
Developed from	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.

Operators

Finland

• Finnish Air Force

Specifications (C.VI.25)

Data from Thulinista Hornetiin – 75 vuotta Suomen ilmavoimien lentokoneita

General characteristics

• Crew: 1
• Length: 6.9 m (22 ft 8 in)
• Wingspan: 9.5 m (31 ft 2 in)
• Max takeoff weight: 843 kg (1,858 lb)
• Powerplant: 1 × Siemens-Halske Sh.IIIA air-cooled geared rotary piston engine, 119 kW (160 hp)
• Propellers: 4-bladed wooden fixed-pitch propeller

Performance

• Maximum speed: 210 km/h (130 mph, 110 kn)

See also

Related lists

• List of aircraft of the Finnish Air Force
• List of fighter aircraft