Bombersprototype light bomber and reconnaissance aircraft
Aero A.104
The Aero A.104 was a parasol monoplane light bomber and reconnaissance aircraft built in Czechoslovakia during the 1930s. It was the final derivative of the Aero A.100, and was essentially an Aero Ab.101 with an enclosed cockpit and without the lower wing. Although two different prototypes flew in 1937, it was not mass-produced.
Summary from Wikipedia licensed under CC BY-SA.
- Manufacturer
- AERO Vodochody Aerospace
- Category
- Bombers
- First flight
- 1937-01-01
Specifications
- Cruise speed
- 180 kt
- Max speed
- 180 kt
- Range
- 540 nm
- Service ceiling
- 30,000 ft
- Rate of climb
- 1,340 ft/min
- Max takeoff weight
- 6,834 lb
- Empty weight
- 6,834 lb
- Powerplant
- ČKD-built Hispano-Suiza 12Ydrs V-12 Liquid-cooled piston engine
- Engines
- 1
- Length
- 35.5 ft
- Wingspan
- 50.8 ft
- Number built
- 2
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.