Team Tango Tango 2

Team Tango Tango 2
Role	Homebuilt aircraft
National origin	United States of America
Manufacturer	Team Tango
First flight	1996
Number built	17 (Tango 2, Dec 2011) 1 (Tango XR, Dec 2011)[1]

The Team Tango Tango 2 is a low wing composite homebuilt aircraft.^[1][2]

Contents 1 Design and development 2 Variants 3 Specifications (Tango 2) 4 See also 5 References

Design and development

The Tango 2 was developed from the 1983 Aero Mirage TC-2 design.^[3] The Tango 2 is a side by side two seat composite aircraft. Both fuselage and wing spare are molded as single pieces.

Variants

Tango 2

Base model

Tango XR

Extended range aircraft with 90 gallon wet wing fuel tanks.

Specifications (Tango 2)

Data from Team Tango

General characteristics

• Capacity: 2
• Length: 20 ft 7 in (6.27 m)
• Wingspan: 26 ft (7.9 m)
• Height: 6.75 ft (2.06 m)
• Wing area: 78 sq ft (7.2 m²)
• Empty weight: 1,150 lb (522 kg)
• Gross weight: 2,000 lb (907 kg)
• Fuel capacity: 58 gal
• Powerplant: 1 × Lycoming IO-360 , 180 hp (130 kW)

Performance

• Maximum speed: 184 kn; 341 km/h (212 mph)
• Cruise speed: 180 kn; 340 km/h (210 mph)
• Stall speed: 51 kn; 95 km/h (59 mph)
• Never exceed speed: 200 kn; 370 km/h (230 mph)

See also

Aircraft of comparable role, configuration and era

• Glasair I
  

References

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