Aero A.46

The Aero A.46 was a Czechoslovakian military trainer biplane that flew in prototype form in 1931. No mass production resulted.

Specifications (A.46)

General characteristics

Crew: two, student and instructor
Length: 8.45 m (27 ft 9 in)
Wingspan: 11.82 m (38 ft 9 in)
Wing area: 32.6 m² (351 sq ft)
Empty weight: 1,134 kg (2,500 lb)
Gross weight: 1,488 kg (3,280 lb)
Powerplant: 1 × Skoda-built Hispano-Suiza 8Fb V-8 water-cooled piston engine, 224 kW (300 hp)

Performance

Maximum speed: 196 km/h (122 mph; 106 kn)
Service ceiling: 4,850 m (15,912 ft)
Rate of climb: 2.783 m/s (547.8 ft/min)
Wing loading: 46 kg/m² (9.4 lb/sq ft)
Power/mass: 0.150 W/kg (0.09 hp/lb)

Aircraft produced by Aero Vodochody

1919-1938	Ae 01 Ae 02 Ae 03 Ae 04 Ae 10 A.11 A.12 A.14 A.15 A.17 A.18 A.19 A.20 A.21 A.22 A.23 A.24 A.25 A.26 A.27 A.29 A.30 A.32 A.34 A.35 A.38 A.42 A.46 A.100 A.101 A.102 A.104 A.125 A.130 A.134 A.200 A.204 A.230 A.300 A.304 A.330 A.430

1945-1992	Ae 45 Ae 50 Ae 145 Ae 245 Ae 345 L-29 L-39 L-59 L-60

1993-present	L-159 Ae 270

Under licence	C-3 C-103 D-44 MB.200

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