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Aero A.22

From Wikipedia, the free encyclopedia
Aero A.22
Role Utility aircraft
Manufacturer Aero Vodochody
Primary user Czechoslovakia

TheAero A.22was aCzechoslovakianbiplanecivil utility aircraft based on theAero A.12reconnaissance-bomber. The observer's position was replaced by seating for two passengers.

Specifications (A.22)

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Data fromEuropean 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

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Related development

References

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  1. ^Stroud 1966,pp. 32–33

Stroud, John (1966).European Transport Aircraft since 1910.London: Putnam.