Trainersmilitary training aircraft
A.25
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.
Summary from Wikipedia licensed under CC BY-SA.
- Manufacturer
- AERO Vodochody Aerospace
- Category
- Trainers
- First flight
- 1920-01-01
Specifications
- Cruise speed
- 86 kt
- Max speed
- 86 kt
- Service ceiling
- 21,300 ft
- Rate of climb
- 790 ft/min
- Max takeoff weight
- 2,800 lb
- Empty weight
- 2,172 lb
- Powerplant
- 1 × BMW IIIa 6-cylinder water-cooled in-line piston engine
- Engines
- 1
- Seats
- 2
- Length
- 26.6 ft
- Wingspan
- 42 ft
- Height
- 10.2 ft
Specifications are approximate and may vary by variant. Compiled from Wikipedia (CC BY-SA).
Reference and training only. Specifications vary by variant — consult the manufacturer and the official documents.