Aero A.10
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| Aero A.10 | |
|---|---|
| Type | Airliner |
| Manufacturer | Aero Vodochody |
| Maiden flight | 1921 |
| Retired | 1928 |
| Primary user | Czech Airlines |
The Aero A.10 was a biplane airliner produced in Czechoslovakia shortly after World War I, the first example flying in 1921. Three passengers could be accommodated in an enclosed cabin, and three collapsible tables could also be used to seat another three if desired. The A.10 was important as one of Czech Airlines's first aircraft, with five examples in service with the airline from the time of its inception in 1923 until 1928.
[edit] Specifications (A.10)
This aircraft article is missing some (or all) of its specifications. If you have a source, you can help Wikipedia by adding them.General characteristics
- Crew: 1
- Capacity: 6 passengers
- Length: 10.14 m (33 ft 3 in)
- Wingspan: 14.17 m (46 ft 6 in)
- Height: m (ft in)
- Wing area: 49 m² (527 ft²)
- Empty weight: 1,472 kg (3,245 lb)
- Max takeoff weight: 2,260 kg (4,980 lb)
- Powerplant: 1× Maybach Mb IVa, 190 kW (260 hp)
Performance
- Maximum speed: 160 km/h (90 knots, 100 mph)
- Range: 520 km (280 nm, 330 mi)
- Service ceiling: 5,800 m (19,000 ft)
- Rate of climb: m/s (ft/min)
[edit] Related content
Designation sequence
Related lists
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