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Aero A.21The Aero A.21 was a biplane military trainer aircraft developed in Czechoslovakia from the Aero A.11 reconnaissance-bomber. The aircraft was developed specifically as a night-trainer, to teach Czechoslovakian Air Force pilots instrument flying techniques. Specifications (A.21) General Characteristics - Crew: two, student and instructor
- Length: 8.20 m (26 ft 11 in)
- Wingspan: 12.80 m (43 ft 0 in)
- Height: 3.10 m (10 ft 2 in)
- Wing area: 36.5 m² (393 ft²)
- Empty: 1,080 kg (2,376 lb)
- Loaded: 1,328 kg (2,922 lb)
- Maximum takeoff: kg ( lb)
- Powerplant: 1x Breitfeld & Danek Perun I, 134 kW (180 hp)
Performance - Maximum speed: 170 km/h (106 mph)
- Range: km ( miles)
- Service ceiling: 6,500 m (21,320 ft)
- Rate of climb: 141 m/min (461 ft/min)
- Wing loading: 36 kg/m² (7.4 lb/ft²)
- Power/Mass: 0.10 kW/kg (0.06 hp/lb)
Related content Related development: A.11 - A.12 - A.22 - A.25 - A.29 Comparable aircraft: Designation sequence: A.18 - A.19 - A.20 - A.21 - A.22 - A.23 - A.24
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