IVL C.24

C.24
Role	Fighter aircraft
Manufacturer	IVL
Designer	Kurt Berger
First flight	April 16, 1924
Primary user	Finnish Air Force
Number built	1

IVL C.24 was the first aircraft to be designed in Finland and built in an industrial environment. The aircraft was manufactured by IVL, but only in one example.

The designer of the aircraft was engineer Kurt Berger. The aircraft made its maiden flight on April 16, 1924, piloted by Georg Jäderholm.

The aircraft was a one seated, high-wing monoplane. It was designed as a fighter, but its engine was under-powered, the speed moderate and flight characteristics poor. The visibility from the pilot's seat was also very poor. The aircraft was in Finnish Air Force use for a short time.

Operators

Finland

• Finnish Air Force

Specifications (C.24)

Data from AVI

General characteristics

• Crew: 1
• Length: 7.1 m (23 ft 4 in)
• Wingspan: 12.1 m (39 ft 8 in)
• Height: 2.9 m (9 ft 6 in)
• Wing area: 19 m² (200 sq ft)
• Empty weight: 660 kg (1,455 lb)
• Max takeoff weight: 870 kg (1,918 lb)

Performance

• Maximum speed: 200 km/h (120 mph, 110 kn) +
• Wing loading: 44.7 kg/m² (9.2 lb/sq ft)

|crew=One, pilot |capacity= |length main=7.1 m |length alt=23 ft 3 in |span main=12.1 m |span alt= 39 ft 8 in |height main=2.9 m |height alt=9 ft 6 in |area main=19 m² |area alt= 204.4 ft² |airfoil= |empty weight main=660 kg |empty weight alt=1,452 lb |loaded weight main= kg |loaded weight alt= lb |useful load main= kg |useful load alt= kg |max takeoff weight main=870 kg |max takeoff weight alt= 1,740 lb

See also

Related lists

• List of aircraft of the Finnish Air Force