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Aero Tovarna Letadel Dr Kabes Aero 2
Ikarus Aero 2

Aero2-01
 
The Ikarus Aero 2 was designed in response to a Yugoslav Air Force requirement for a modern, monoplane trainer to replace the Fizir FN biplanes then in service. Although the design pre-dated the war, the Aero 2 was a piston-engined military trainer aircraft built in Yugoslavia in the years following World War II.
 
Designed by Ing. Petkov and Ing. Boris Cijan, the prototype was built by the Ikarus factory at Zemun and flew for the first time on 19 October 1946.
 
Aero2-02
Aero 2H

 

Variants:
 
Aero 2B
Open cockpit version: 145hp (108kW) de Havilland Gipsy Major
 
Aero 2BE
Enclosed cockpit version: 145hp (108kW) de Havilland Gipsy Major
 
Aero 2C
Open cockpit version: 160hp (119kW) Walter Minor 6-III
 
Aero 2D
Enclosed cockpit version: 160hp (119kW) Walter Minor 6-III
 
Aero 2E
Enclosed cockpot version: 160hp (119kW) Walter Minor 6-III
 

 

Aero 2F
Open cockpit version
Engine: 160hp (119kW) Walter Minor 6-III
Span: 34 ft 5.25 in
Length: 27 ft 0 in
Loaded weight: 2156 lb
Max speed: 139 mph at SL

Seats: 2

 
Aero 2H
Twin-float version: 160hp (119kW) Walter Minor 6-III
 
General characteristics:
Engine: 1 × de Havilland Gipsy Major, 108 kW (145 hp)
Wingspan: 10.5 m (34 ft 5¼ in)
Wing area: 17.4 sq.m (187 sq.ft)
Length: 8.45 m (27 ft 8¾ in)
Height: 2.80 m (8 ft 10¼ in)
Empty weight: 564 kg (1241 lb)
Gross weight: 996 kg (2196 lb)
Maximum speed: 208 km/h (129 mph)
Range: 680 km (423 miles)
Service ceiling: 4500 m (14,765 ft)
Seats: 2
 
Aero2-03
Aero 2F

 

 
 
 
 
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