IRI T250A
{{Short description|Italian helicopter}}
{{Use dmy dates|date=January 2022}}
{{Use British English|date=January 2022}}
{{Infobox aircraft begin
| name=T250A | image= | caption= }}{{Infobox aircraft type | type=Helicopter | national origin=Italy | manufacturer=Italian Rotors Industries | designer= | first flight= | introduced=2015 | retired= | status=Production completed (2016) | primary user= | more users= | produced= | number built= | developed from= IRI T22B | variants with their own articles= }} |
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.Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 209. Flying Pages Europe SARL, 2015. {{ISSN|1368-485X}}
The company seems to have been founded about 2013 and gone out of business in June 2016, ending production.{{cite web|url= https://web.archive.org/web/*/http://www.irihelicopters.eu/ |title=IRI Helicopters |website=Internet Archive Wayback Machine |access-date=30 December 2017}}{{cbignore}}{{cite web|url = https://www.facebook.com/irihelicopters|title = Italian Rotors Industries |access-date = 30 December 2017|author=Italian Rotors Industries |work = Facebook|date = 28 June 2016}}
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 {{convert|250|hp|kW|0|abbr=on}} 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 {{convert|7.6|m|ft|1|abbr=on}}. The aircraft has a typical empty weight of {{convert|295|kg|lb|0|abbr=on}} and a gross weight of {{convert|650|kg|lb|0|abbr=on}}, giving a useful load of {{convert|355|kg|lb|0|abbr=on}}. With full fuel of {{convert|130|L}} the payload for the crew, passenger and baggage is {{convert|261|kg|lb|0|abbr=on}}.
Specifications (T250A)
{{Aircraft specs
|prime units?=met
|genhide=
|crew=one
|capacity=one passenger
|length m=
|length ft=
|length in=
|length note=
|width m=
|width ft=
|width in=
|width note=
|height m=
|height ft=
|height in=
|height note=
|airfoil=
|empty weight kg=295
|empty weight lb=
|empty weight note=
|gross weight kg=650
|gross weight lb=
|gross weight note=
|fuel capacity={{convert|130|L}}
|more general=
|eng1 number=1
|eng1 name=PBS TS 100
|eng1 type=turboshaft engine
|eng1 kw=
|eng1 hp=250
|rot number=1
|rot dia m=7.6
|rot dia ft=
|rot dia in=
|rot area sqm=45
|rot area sqft=
|rot area note=
|perfhide=
|max speed kmh=195
|max speed mph=
|max speed kts=
|max speed note=
|cruise speed kmh=175
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|range km=
|range miles=
|range nmi=
|range note=
|endurance=
|ceiling m=
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=11
|climb rate ftmin=
|climb rate note=
|time to altitude=
|disk loading kg/m2=14.4
|disk loading lb/sqft=
|disk loading note=
|fuel consumption kg/km=
|fuel consumption lb/mi=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}
See also
References
{{reflist}}
External links
- [https://web.archive.org/web/*/http://www.irihelicopters.eu/ Official website archives] on Archive.org
{{Portal bar|Italy|Companies|Aviation}}
Category:2010s Italian sport aircraft