Aero A.25
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| Aero A.25 | |
|---|---|
| Role | Trainer aircraft |
| Manufacturer | Aero Vodochody |
| First flight | 1920s |
| Primary user | Czechoslovakia |
The 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 (Aero A.25)
General characteristics
- Crew: 2 (instructor and student)
- 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 weight: 985 kg (2,167 lb)
- Loaded weight: 1,270 kg (2,794 lb)
- Powerplant: 1 × BMW IIIa, 138 kW (185 hp)
Performance
- Maximum speed: 160 km/h (86 knots, 100 mph)
- Range: km (nm, mi)
- Service ceiling: 6,500 m (21,320 ft)
- Rate of climb: 4 m/s (787 ft/min)
- Wing loading: 35 kg/m² (7.1 lb/ft²)
- Power/mass: 110 W/kg (0.07 hp/lb)
Operators
See also
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Wikimedia Commons has media related to Aero Vodochody aircraft. |
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