Aero A.23

The Aero A.23 was a Czechoslovakian biplane airliner of the 1920s. Aero's previous airliner design, the A.10 had been a relatively crude machine drawing heavily on World War I military aircraft. The A.23, designed in 1925 was relatively modern, although it still seated its pilot in an open cockpit above the passenger cabin. Seven A.23s flew CSA's Prague-Marienbad and Prague-Uzhhorod routes between 1926 and 1936.

Specifications (A.23)

General Characteristics

  • Crew: one, pilot
  • Capacity: eight passengers
  • Length: 12.60 m (41 ft 4 in)
  • Wingspan: 16.70 m (54 ft 10 in)
  • Height: m ( ft in)
  • Wing area: 67 m² (721 ft²)
  • Empty: 1,860 kg (4,100 lb)
  • Loaded: kg ( lb)
  • Maximum takeoff: 3,150 kg (6,945 lb)
  • Powerplant: 1x Walter-built Bristol Jupiter IV, 336 kW (450 hp)

Performance

  • Maximum speed: 185 km/h (115 mph)
  • Range: km ( miles)
  • Service ceiling: 5,500 m (18,045 ft)
  • Rate of climb: m/min ( ft/min)
  • Wing loading: kg/m² ( lb/ft²)
  • Power/Mass: kW/kg ( hp/lb)

Related content

Related development: Comparable aircraft: Designation sequence: A.20 - A.21 - A.22 - A.23 - A.24 - A.25 - A.26

 

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