page_title: Aero A.23
section_title: Specifications
hierarchical_section_title: Aero A.23 / Specifications
caption_attribution_description: English: Aero A.23 as designed with a Lorraine-Dietrich 12C motor. 3-view drawing from Les Ailes May 17,1928
context_page_description: The Aero A.23 was a Czechoslovakian airliner of the 1920s. Aero Vodochody had produced the first Czech airliner, the A.10, four of which had served with ČSA, the national airline. The A.23, another biplane, was bigger, more powerful and could carry more passengers.
context_section_description: Data from Les Ailes May 1928, Jane's Encyclopedia of Aircraft
  General characteristics
  Crew: Two
  Capacity: Six or seven passengers
  Length: 12.20 m (40 ft 0 in)
  Wingspan: 16.60 m (54 ft 6 in)
  Height: 4.50 m (14 ft 9 in)
  Wing area: 67 m² (720 sq ft)
  Empty weight: 1,790 kg (3,946 lb)
  Gross weight: 3,100 kg (6,834 lb)
  Powerplant: 1 × Walter Jupiter IV 9-cylinder radial, 310 kW (420 hp)
  Propellers: 2-bladed
  Performance
  Maximum speed: 185 km/h (115 mph; 100 kn)
  Cruise speed: 155 km/h (96 mph; 84 kn)
  Stall speed: 90 km/h (56 mph; 49 kn) minimum speed
  Range: 620 km (385 mi; 335 nmi) no reserves
  Service ceiling: 5,500 m (18,000 ft)
  Time to altitude: 39 min 15 s to 5,000 m (16,000 ft)
  Take-off distance: 80 m (260 ft)
  Landing distance: 60 m (200 ft)
caption: Aero A.23 as designed with a Lorraine-Dietrich 12C motor. 3-view drawing from Les Ailes May 17,1928
exif: {}