Aeromot AMT-100 Ximango
| AMT-100 Ximango | |
|---|---|
.jpg)
| |
| Aeromot AMT-100 Ximango motorglider F-CHXB at Midden-Zeeland Airport (EHMZ), May 19, 1991 | |
| Role | Motor glider |
| National origin | Brazil |
| Manufacturer | Aeromot |
| Designer | René Fournier |
| Introduction | 1986 |
| Number built | 44 (1993) |
| Developed from | Fournier RF-10 |
| Variants | AMT-200 Super Ximango |
The Aeromot AMT-100 Ximango is a Brazilian motor glider developed from the Fournier RF-10.[1]
Design and development
[edit]Built from glassfibre, the Ximango is a low-wing cantilever monoplane with conventional landing gear and a T-tail. Powered by front-mounted 80 hp Limbach L2000 E01, it has an enclosed side-by-side cockpit for two. The wings fold for storage or transportation. The type could also be fitted with an alternate Imaer T2000 M1 engine. The type was developed into the Rotax-powered AMT-200 Super Ximango.
Specification
[edit]Data from Taylor 1996, p. 511
General characteristics
- Crew: 2
- Length: 7.89 m (25 ft 11 in)
- Wingspan: 17.47 m (57 ft 4 in)
- Wing area: 18.7 m2 (201 sq ft)
- Aspect ratio: 16.32
- Empty weight: 600 kg (1,323 lb)
- Max takeoff weight: 800 kg (1,764 lb)
- Powerplant: 1 × Limbach L2000 E01 4-cylinder horizontally opposed 4-stroke piston engine, 60 kW (80 hp)
- Propellers: 2-bladed Hoffmann HO-V62R/L, 1.6 m (5 ft 3 in) diameter
Performance
- Cruise speed: 190 km/h (120 mph, 100 kn)
- Stall speed: 76 km/h (47 mph, 41 kn)
- Never exceed speed: 245 km/h (152 mph, 132 kn)
- Maximum glide ratio: 30
See also
[edit]Related development
Related lists
References
[edit]- ^ Taylor 1996, p. 511.
Bibliography
[edit]- Taylor, Michael JH (1996). Brassey's World Aircraft & Systems Directory 1996/97. London: Brassey's. ISBN 1-85753-198-1.
External links
[edit]
Wikimedia Commons has media related to Aeromot AMT-100 Ximango.
- Certificação [Type Certificate] (PDF) (in Portuguese), BR: Anac, archived from the original (PDF) on 2011-07-06.