Terzi T-9 Stiletto

Terzi T-9 Stiletto
Role	Two-seat light sport monoplane
National origin	Italy
Manufacturer	Terzi Aerodyne
Designer	Pietro Terzi
First flight	December 1990[1]

The Terzi T-9 Stiletto is an Italian two-seat light aircraft designed and built by Terzi Aerodyne of Milan, Italy.^[2]

Design and development

The Stiletto is a two-seat low-wing monoplane designed to meet the JAR-VLA regulations.^[2] It is mainly metal construction but has a glassfibre cabin enclosure.^[2] It has a fixed nosewheel landing gear and is powered by a nose mounted Rotax 912A piston engine.^[2] The cantilever wings can be detached for transport and storage.^[2]

Specifications

Data from ^[2]

General characteristics

• Crew: 1
• Capacity: 1
• Length: 6.85 m (22 ft 6 in)
• Wingspan: 10.26 m (33 ft 8 in)
• Height: 2.3 m (7 ft 7 in)
• Wing area: 12.3 m² (132 sq ft)
• Aspect ratio: 8.558
• Empty weight: 380 kg (838 lb)
• Max takeoff weight: 650 kg (1,433 lb)
• Powerplant: 1 × Rotax 912A piston, 58 kW (78 hp)
• Propellers: 2-bladed

Performance

• Maximum speed: 200 km/h; 124 mph (108 kn)
• Cruise speed: 163 km/h; 101 mph (88 kn) 60% power
• Stall speed: 74 km/h; 46 mph (40 kn) with flaps

References

Notes

1. Lambert 1993, pp. 202–203.
2. Taylor 1996, p. 408

Bibliography

• Lambert, Mark (editor) (1993). Jane's All The World's Aircraft 1993-94. Coulsdon, UK: Jane's Data Division. ISBN 0-7106-1066-1.
• Taylor, Michael J. H. (1996). Brassey's World Aircraft & Systems Directory. London, England: Brassey's. ISBN 1-85753-198-1.