AISA I-11
| I-11 | |
|---|---|
| |
| Role | Two-seat general aviation aircraft |
| Manufacturer | AISA
|
| First flight | 16 July 1951 |
| Number built | 208 |
| Variants | AISA I-115 |
The I-11 was a two-seat civil utility aircraft manufactured in
AISA
.
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 a
training
and liaison roles.
The Air Force then requested 200 aircraft built with the seats in tandem, which were designated I-115 by the manufacturers powered by a 112 kW (150 hp) ENMA Tigre inverted air-cooled engine.[1]
Variants
- I-11
- 2 prototypes by Iberavia, tricycle undercarriage
- I-11B
- Production examples by AISA
- AISA I-115
- Tandem-seat version.
Operators
- Spanish Air Force
Specifications (I-11B)
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 × piston 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
Wikimedia Commons has media related to AISA I-11.
- ^ Bridgman 1956, pp. 211
- ^ 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