- Design and development
- Specifications
- References Notes
name=Delt-Air 250 | image= | caption= }}{{Infobox Aircraft Type | type=Delta-wing homebuilt aircraft | national origin=United States | manufacturer= | designer=Herbert Dean | first flight=8 November 1961 | introduced= | retired= | status=Destroyed | produced= | primary user= | number built=1 | developed from= | variants with their own articles= | developed into= }} |
The Dean Delt-Air 250 was an American twin-seat amateur-built, delta wing light aircraft. Designed and built by Herbert Dean of Flint, Michigan, the aircraft was destroyed on its first flight and Dean was killed. Design and developmentThe Delt-Air was a single-engined all-metal light aircraft powered by a {{convert|180|hp|kW|0|abbr=on}} Lycoming O-360 engine mounted at the rear driving a pusher propeller. It had a tricycle landing gear and rear-hinged canopy for access to the tandem cockpit. Registered N6379T it was destroyed during its first fatal flight on 8 November 1961.[3] Specifications{{Aircraft specs |ref=Flight International January 1962 |prime units?=imp |genhide= |crew= |capacity= |length m= |length ft=25 |length in=3 |length note= |span m= |span ft=16 |span in=3 |span note= |swept m= |swept ft= |swept in= |swept note= |height m= |height ft= |height in= |height note= |wing area sqm= |wing area sqft= |wing area note= |airfoil= |empty weight kg= |empty weight lb= |empty weight note= |gross weight kg= |gross weight lb=1460 |gross weight note= |max takeoff weight kg= |max takeoff weight lb= |max takeoff weight note= |more general=
|eng1 number=1 |eng1 name=Lycoming O-360 |eng1 type=four-cylinder, direct-drive, horizontally opposed, air-cooled, piston aircraft engine. |eng1 kw= |eng1 hp=180 |eng1 note= |power original= |thrust original= |eng1 kn-ab= |eng1 lbf-ab= |prop blade number=2 |prop name= |prop dia m= |prop dia ft= |prop dia in= |prop note=
|perfhide= |max speed kmh= |max speed mph=240 |max speed kts= |max speed note=estimated |cruise speed kmh= |cruise speed mph= |cruise speed kts= |cruise speed note= |stall speed kmh= |stall speed mph= |stall speed kts= |stall speed note= |never exceed speed kmh= |never exceed speed mph= |never exceed speed kts= |never exceed speed note= |minimum control speed kmh= |minimum control speed mph= |minimum control speed kts= |minimum control speed note= |range km= |range miles= |range nmi= |range note= |endurance= |ceiling m= |ceiling ft= |ceiling note= |climb rate ms= |climb rate ftmin= |climb rate note= |more performance= |avionics= }}{{aircontent |see also= |related= |similar aircraft= |lists= }}
ReferencesNotes1. ^1 {{cite web | title=American airplanes - Da - Dy | url=http://aerofiles.com/_d.html| publisher=www.aerofiles.com |date=11 March 2009|accessdate=24 December 2014}}
[1] }}{{refbegin}}{{refend}} 4 : United States civil utility aircraft 1960–1969|Homebuilt aircraft|Delta-wing aircraft|Aircraft first flown in 1961 |