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The Aero A.22 was a Czechoslovakian biplane civil utility aircraft based on the Aero A.12 reconnaissance-bomber. The observer's position was replaced by seating for two passengers.
| Aero A.22 | |
|---|---|
| General information | |
| Type | Utility aircraft |
| Manufacturer | Aero Vodochody |
| Primary user | Czechoslovakia |
Specifications (A.22)
editData from European Transport Aircraft since 1910[1]
General characteristics
- Crew: 1
- Capacity: 2 passengers
- Length: 8.3 m (27 ft 3 in)
- Wingspan: 12.8 m (42 ft 0 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 × Walter 6-cylinder water-cooled in-line piston engine, 160 kW (220 hp)
Performance
- Maximum speed: 200 km/h (120 mph, 110 kn)
- Cruise speed: 175 km/h (109 mph, 94 kn)
- Range: 750 km (470 mi, 400 nmi)
- Service ceiling: 7,650 m (25,100 ft)
See also
editRelated development
References
edit- ^ Stroud 1966, pp. 32–33
Stroud, John (1966). European Transport Aircraft since 1910. London: Putnam.