Aero A.22

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
Role Utility aircraft
Manufacturer Aero Vodochody
Primary user Czechoslovakia

Specifications (A.22)

Data 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

Related development

References

  1. Stroud 1966, pp. 32–33

Stroud, John (1966). European Transport Aircraft since 1910. London: Putnam.CS1 maint: ref=harv (link)

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