IRI T250A

T250A
General information
TypeHelicopter
National origin
Italy
ManufacturerItalian Rotors Industries
StatusProduction completed (2016)
History
Introduction date
2015
Developed from
IRI T22B

The IRI T250A is an Italian helicopter that was designed and produced by Italian Rotors Industries of Aprilia, Lazio and introduced in 2015. Now out of production, when it was available the aircraft was supplied complete and ready-to-fly.

The company seems to have been founded about 2013 and gone out of business in June 2016, ending production.

Design and development

The T250A features a single main rotor and tail rotor, a two-seats-in side-by-side configuration enclosed cockpit with a windshield, skid landing gear and a 250 hp (186 kW) PBS TS 100 turboshaft engine made by PBS Velká Bíteš.

The aircraft fuselage is made from composites. Its two-bladed rotor has a diameter of 7.6 m (24.9 ft). The aircraft has a typical empty weight of 295 kg (650 lb) and a gross weight of 650 kg (1,433 lb), giving a useful load of 355 kg (783 lb). With full fuel of 130 litres (29 imp gal; 34 US gal) the payload for the crew, passenger and baggage is 261 kg (575 lb).

The aircraft was built to ISO 9001 and EN 9100 standards.

Specifications (T250A)

Data from Tacke

General characteristics

Performance

See also

References

  1. 1 2 3 4 5 Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 209. Flying Pages Europe SARL, 2015. ISSN 1368-485X
  2. ↑ "IRI Helicopters". Internet Archive Wayback Machine. Retrieved 30 December 2017.
  3. ↑ Italian Rotors Industries (28 June 2016). "Italian Rotors Industries". Facebook. Retrieved 30 December 2017.