Aero A.46

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

[edit] 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)
• Height: ()
• Wing area: 32.6 m² (351 ft²)
• Empty weight: 1,134 kg (2,495 lb)
• Loaded weight: 1,488 kg (3,274 lb)
• Powerplant: 1× Skoda-built Hispano-Suiza 8Fb, 224 kW (300 hp)

Performance

• Maximum speed: 196 km/h (123 mph)
• Service ceiling 4,850 m (15,908 ft)
• Rate of climb: 167 m/min (547 ft/min)
• Wing loading: 46 kg/m² (9.3 lb/ft²)
• Power/mass: 150 W/kg (0.09 hp/lb)

[edit] See also

v • d • e Aircraft produced by Aero 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.125 • A.26 • A.27 • A.29 • A.30/A.130/A.230/A.330/A.430 • A.32 • A.34/A.134 • A.35 • A.38 • A.42 • A.46 A.100 • A.101 • A.102 • A.104 A.200 • A.204 A.300 • A.304 Ae 45/145 • Ae 50 • Ae 270 L-29 • L-39 • L-59/L-159 • L-60 Under licence: C-3/C-103  • MB.200

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