Aero A.22
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| Aero A.22 | |
|---|---|
| Type | Utility aircraft |
| Manufacturer | Aero Vodochody |
| Primary user | Czechoslovakia |
The Aero A.22 was a Czechoslovakian biplane civil utility aircraft based on the Aero A.11 reconnaissance-bomber. The observer's position was replaced by seating for two passengers.
[edit] Specifications (A.22)
General characteristics
- Crew: 1
- Capacity: 2
- Length: 8.2 m (27 ft)
- Wingspan: 12.3 m (40 ft 4 in)
- Height: m (ft in)
- Wing area: 36.9 m² (397 ft²)
- Empty weight: 1,105 kg (2,430 lb)
- Loaded weight: 1,415 kg (3,115 lb)
- Powerplant: 1× Maybach Mb IV, 260 hp (194 kW)
Performance
- Maximum speed: 201 km/h (109 knots, 126 mph)
- Range: km (nm, mi)
- Service ceiling: 7,000 m (23,000 ft)
- Rate of climb: m/s (ft/min)
- Wing loading: 30 kg/m² (6.1 lb/ft²)
- Power/mass: 180 W/kg (0.08 hp/lb)
[edit] Related content
Related development
Designation sequence
Related lists
- List of civil utility aircraft
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