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Aero A.25The Aero A.25 was a biplane military trainer aircraft developed in Czechoslovakia from the Aero A.11 reconnaissance-bomber and generally similar to the Aero A.21 night trainer. Some A.25s were powered by the less powerful 134 kW (180 hp) Breitfeld & Danek Perun I engines, in which case they were designated Aero A.125 Specifications (A.25) General Characteristics - Crew: two, student and instructor
- Length: 8.10 m (26 ft 8 in)
- Wingspan: 12.80 m (43 ft 0 in)
- Height: 3.10 m (10 ft 2 in)
- Wing area: 36.2 m² (389 ft²)
- Empty: 985 kg (2,167 lb)
- Loaded: 1,270 kg (2,794 lb)
- Maximum takeoff: kg ( lb)
- Powerplant: 1x BMW IIIa, 138 kW (185 hp)
Performance - Maximum speed: 160 km/h (100 mph)
- Range: km ( miles)
- Service ceiling: 6,500 m (21,320 ft)
- Rate of climb: 240 m/min (787 ft/min)
- Wing loading: 35 kg/m² (7.1 lb/ft²)
- Power/Mass: 0.11 kW/kg (0.07 hp/lb)
Related content Related development: A.11 - A.12 - A.21 - A.22 - A.29 Comparable aircraft: Designation sequence: A.22 - A.23 - A.24 - A.25 - A.26 - A.27 - A.29
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