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AISA I-11

From Wikipedia, the free encyclopedia
I-11
General information
TypeTwo-seat general aviation aircraft
ManufacturerIberavia/AISA
Number built208
History
First flight16 July 1951
VariantAISA I-115

TheI-11 was a two-seat civil utility aircraft manufactured inSpain in the 1950s. Originally designed by the Spanish aircraft companyIberavia, its first (of two) prototype flew on 16 July1951. It was a low-wingmonoplane of conventional configuration with fixed, tricycleundercarriage and a large,bubble canopy over the two side-by-side seats. Flight characteristics were found to be pleasing, but before plans could be made for mass production, Iberavia was acquired byAISA.

The new management decided to continue with development, but made a few changes to the design, reducing the size of the canopy, and replacing the undercarriage with ataildragger arrangement. This configuration entered production in1952 with an order from the Director General for Civil Aviation for 70 aircraft for use in Spain's aeroclubs. TheSpanish Air Force then ordered 125 for use intraining and liaison roles.

The Air Force then requested 200 aircraft built with the seats in tandem, which were designatedI-115 by the manufacturers powered by a 112 kW (150 hp) ENMA Tigre inverted air-cooled engine.[1]

Variants

[edit]
I-11
2 prototypes by Iberavia, tricycle undercarriage
I-11B
Production examples by AISA
AISA I-115
Tandem-seat version.

Operators

[edit]
 Spain

Specifications (I-11B)

[edit]

Data from Jane's All The World's Aircraft 1969–70[2]

General characteristics

  • Crew: 1
  • Capacity: 1 passenger or trainee
  • Length: 6.48 m (21 ft 3 in)
  • Wingspan: 9.32 m (30 ft 7 in)
  • Height: 1.91 m (6 ft 3 in)
  • Wing area: 13.4 m2 (144 sq ft)
  • Empty weight: 420 kg (926 lb)
  • Gross weight: 669 kg (1,474 lb)
  • Powerplant: 1 ×Continental C90-12F Four-cylinder air-cooled horiztonally opposedpiston engine, 67 kW (90 hp)

Performance

  • Maximum speed: 201 km/h (125 mph, 109 kn)
  • Cruise speed: 180 km/h (110 mph, 96 kn)
  • Range: 640 km (400 mi, 350 nmi)
  • Service ceiling: 4,700 m (15,400 ft)
  • Rate of climb: 3.69 m/s (726 ft/min)

References

[edit]
Wikimedia Commons has media related toAISA I-11.
  1. ^Bridgman 1956, pp. 211
  2. ^Taylor 1969, pp. 166–167
  • Bridgman, Leonard (1956).Jane's All the World's Aircraft 1956–57. London: Jane's All the World's Aircraft Publishing Co. Ltd.
  • Taylor, John W.R., ed. (1969).Jane's All The World's Aircraft 1969-70. London: Jane's Yearbooks.
  • Taylor, Michael J. H. (1989).Jane's Encyclopedia of Aviation. London: Studio Editions. p. 50.
  • Simpson, R. W. (1995).Airlife's General Aviation. Shrewsbury: Airlife Publishing. pp. 403–404.
  • Fundació Aeronàutica Mallorquina website
Spanish Armed Forces liaison/utility aircraft designations
Enlace (L)
Liaison
First series
Second series
Utilitario (U)
Utility
  • 1 Not assigned
  • 2 No details known
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