Hispano HS-42

From Wikipedia, the free encyclopedia
Jump to: navigation, search
HS-42 and HA-43
Role Military trainer
National origin Spain
Manufacturer Hispano-Suiza/Hispano Aviación
First flight 1947
Primary user Spanish Air Force

The Hispano HS-42 and its derivative, the HA-43, were advanced military trainer aircraft produced in Spain in the 1940s. The basic design was that of a conventional, low-wing, cantilever monoplane with seating for the pilot and instructor in tandem. The HS-42 had fixed, tailwheel undercarriage with spatted mainwheels, while the HA-43 had retractable main units. Produced on the assembly line that had been used to build Fokker D.XXI fighters, the HS-42 shared some components with this aircraft.


Original production version with fixed undercarriage and Piaggio Stella P.VII C.16 engine
Improved variant with retractable undercarriage and Armstrong Siddeley Cheetah 27 engine



Specifications (HA-43)[edit]

Data from Jane's All The World's Aircraft 1953-54 [1]

General characteristics

  • Crew: Two, pilot and instructor
  • Length: 7.95 m (26 ft 2 in)
  • Wingspan: 10.00 m (32 ft 10 in)
  • Height: 2.6 m (8 ft 6 in)
  • Empty weight: 1,504 kg (2,309 lb)
  • Gross weight: 2,050 kg (4,510 lb)
  • Powerplant: 1 × Armstrong Siddeley Cheetah 27, 290 kW (390 hp)


  • Maximum speed: 335 km/h (209 mph)
  • Range: 1,200 km (750 miles)
  • Service ceiling: 6,000 m (19,680 ft)
  • Rate of climb: 8.0 m/s (1,410 ft/min)



  1. ^ Bridgman 1953, pp.186-187.
  • Bridgman, Leonard (ed.) (1953). Jane's All The World's Aircraft 1953-54. London: Jan's. 
  • The Illustrated Encyclopedia of Aircraft. London: Aerospace Publishing. p. 2174. 
  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. pp. 510–11.