Aero A.22
 |
| Aero A.22 | |
|---|---|
| Role | 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.
Specifications (A.22)
General characteristics
- Crew: 1
- Capacity: 2 pax
- Length: 8.2 m (26 ft 11 in)
- Wingspan: 12.3 m (40 ft 4 in)
- Wing area: 36.9 m2 (397 sq ft)
- Empty weight: 1,105 kg (2,436 lb)
- Gross weight: 1,415 kg (3,120 lb)
- Powerplant: 1 × Maybach Mb.IV 6-cyl. water-cooled in-line piston engine, 190 kW (260 hp)
Performance
- Maximum speed: 201 km/h (125 mph, 109 kn)
- Service ceiling: 7,000 m (23,000 ft)
- Wing loading: 30 kg/m2 (6.1 lb/sq ft)
- Power/mass: 0.180 kW/kg (0.08 hp/lb)
See also
Wikimedia Commons has media related to Aero Vodochody aircraft.
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