IVL C.VI.25 - Misplaced Pages

1920s Finnish fighter aircraft

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.

Operators

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

Heinonen, Timo (1992). Thulinista Hornetiin – 75 vuotta Suomen ilmavoimien lentokoneita (in Finnish). Tikkakoski: Keski-Suomen ilmailumuseo. ISBN 951-95688-2-4.

v t e Valtion lentokonetehdas aircraft
Ilmailuvoimien Lentokonetehdas	IVL A.22 Hansa IVL C.24 IVL C.VI.25 Caudron C.60 IVL Haukka IVL K.1 Kurki
Valtion Lentokonetehdas	NVI F.K.31 VL D.27 Haukka VL Sääski VL Kotka VL Paarma VL Tuisku VL Viima VL Pyry VL Myrsky VL Humu VL Pyörremyrsky
Valmet	Valmet Vihuri Valmet Tuuli Valmet L-70 Vinka Valmet L-80 Turbo-Vinha Valmet PIK-23 Towmaster Valmet L-90TP Redigo