LearAvia Lear Fan

{{Short description|Innovative concept jet}}

{{Infobox aircraft

|name=Lear Fan 2100

|image=Two Learfans at Reno 1982 (6579626527).jpg

|caption=Two Lear Fans during a 1982 display flight

|type =Business aircraft

|national_origin=United States of America

|manufacturer=LearAvia

|designer=Bill Lear

|first_flight=January 1, 1981

|status =

|number_built =3

}}

The LearAvia Lear Fan 2100 was a turboprop business aircraft designed in the 1970s, with an unusual configuration. The Lear Fan never entered production.

Design and development

File:Learfan landing at Reno-Stead (4815953232).jpg

The Lear Fan was designed by Bill Lear, but not completed before his death in 1978. It was planned for production to be carried out in Belfast, Northern Ireland, in a new factory built with money from the British Government in an effort to boost employment.McCellan 2006. The aircraft had a pressurized cabin and was designed for a service ceiling of 41,000 ft (12 500 m). It could accommodate two pilots and seven passengers, or one pilot and eight passengers.

It featured a pusher configuration in which two engines powered a single constant-speed three- or four-bladed propeller at the rear of the aircraft. A purpose-built gearbox allowed two Pratt & Whitney Canada PT6B turboshaft engines to supply power via two independent driveshafts. The intent of the design was to provide the safety of multi-engine reliability, combined with single-engine handling in case of failure of one of the engines.

The aircraft was made of lightweight composite materials instead of the more common aluminum alloy.

Another distinctive feature was the Y-shaped empennage. Two stabilizers pointed upward at an angle, similar to those on a V-tail aircraft, and a short vertical stabilizer pointed downward. However, unlike conventional V-tails, there was no pitch/yaw control mixing on the Lear Fan. The downward-pointing rudder also served to protect the propeller from ground strikes during takeoff and landing.

Operational history

After the cancellation of a planned test flight on December 31, 1980 due to technical issues, the first prototype made its maiden flight on January 1, 1981, a date officially recorded by sympathetic British government officials as "December 32, 1980" in order to secure funding that expired at the end of 1980.[http://www.museumofflight.org/aircraft/lear-fan-2100-futura Lear Fan 2100 (Futura)] {{webarchive|url=https://web.archive.org/web/20090712041304/http://museumofflight.org/aircraft/lear-fan-2100-futura |date=2009-07-12 }}. The Museum of Flight. 2009. Retrieved 27 November 2009.

The Lear Fan, however, did not enter production. Structural problems were discovered during the pressurization of the all-composite fuselage. The US Federal Aviation Administration refused to issue the prototype with an airworthiness certificate because of concerns that, despite having two engines, the combining-gearbox that drove the single propeller was not adequately reliable. Development was abandoned in 1985[http://www.flightglobal.com/pdfarchive/view/1985/1985%20-%201874.html Lear Fan Collapses] {{Webarchive|url=https://web.archive.org/web/20121026070559/http://www.flightglobal.com/pdfarchive/view/1985/1985%20-%201874.html |date=2012-10-26 }}. Flight International 8 June 1985, p.30. after only three aircraft were built.

Surviving aircraft

File:Aircraft on display at the Museum of Flight (6193818405).jpg

File:Frontiers of Flight Museum December 2015 112 (LearAvia Lear Fan 2100).jpg]]

All three Lear Fan aircraft have been preserved. They are on display at the Museum of Flight in Seattle, Washington, the Frontiers of Flight Museum in Dallas, Texas,[http://www.flightmuseum.com/aircraft.htm Aircraft at the Frontiers of Flight Museum – Dallas, Texas] {{webarchive|url=https://web.archive.org/web/20091208071009/http://www.flightmuseum.com/aircraft.htm |date=2009-12-08 }}. Frontiers of Flight Museum. Retrieved 27 November 2009. and on static display in front of the Civil Aerospace Medical Institute in Oklahoma City, Oklahoma.[https://www.google.com/maps/@35.3964909,-97.6191733,48m/data=!3m1!1e3 Lear Fan in front of CAMI] Google Maps satellite view.

Specifications

{{Aircraft specs

|ref=Jane's All The World's Aircraft 1982–83Taylor 1982, pp. 399–400.

|prime units?=imp

|crew=Two (pilot and copilot)

|capacity=Six passengers

|length m=

|length ft=40

|length in=7

|length note=

|span m=

|span ft=39

|span in=4

|span note=

|height m=

|height ft=12

|height in=2

|height note=

|wing area sqm=

|wing area sqft=162.9

|wing area note=

|aspect ratio=9.5

|airfoil=

|empty weight kg=

|empty weight lb=4100

|empty weight note=

|gross weight kg=

|gross weight lb=

|gross weight note=

|max takeoff weight kg=

|max takeoff weight lb=7350

|max takeoff weight note=

|fuel capacity=

|more general=

|eng1 number=2

|eng1 name=Pratt & Whitney (Canada) PT6B-35F

|eng1 type=turboprops

|eng1 kw=

|eng1 shp=650

|eng1 note=

|power original=

|more power=

|prop blade number=

|prop name=

|prop dia m=

|prop dia ft=

|prop dia in=

|prop note=

|max speed kmh=

|max speed mph=450

|max speed kts=

|max speed note=at {{convert|25000|ft}}

|max speed mach=

|cruise speed kmh=

|cruise speed mph=322

|cruise speed kts=

|cruise speed note=at {{convert|40000|ft}} economy cruise

|stall speed kmh=

|stall speed mph=88

|stall speed kts=

|stall speed note=with flaps down and power off

|never exceed speed kmh=

|never exceed speed mph=

|never exceed speed kts=

|never exceed speed note=

|range km=

|range miles=1783

|range nmi=

|range note=

|combat range km=

|combat range miles=

|combat range nmi=

|combat range note=

|ferry range km=

|ferry range miles=

|ferry range nmi=

|ferry range note=

|endurance=

|ceiling m=

|ceiling ft=41000

|ceiling note=

|g limits=

|roll rate=

|glide ratio=

|climb rate ms=

|climb rate ftmin=3450

|climb rate note=

|time to altitude=

|lift to drag=

|wing loading kg/m2=

|wing loading lb/sqft=

|wing loading note=

|disk loading kg/m2=

|disk loading lb/sqft=

|disk loading note=

|fuel consumption kg/km=

|fuel consumption lb/mi=

|power/mass=

|thrust/weight=

|more performance=

|guns=

|bombs=

}}

See also

References

=Citations=

{{reflist}}

=Bibliography=

{{refbegin}}

  • "[http://www.flightglobal.com/pdfarchive/view/1985/1985%20-%201874.html Lear Fan Collapses]". Flight International, 8 June 1985. Sutton, UK:Business Press International. p. 30.
  • McClellan, J. Mac. "[http://www.flyingmag.com/columnists/653/flashback-to-1981.html Flashback to 1981:A Look Back at the Lear Fan]". Flying, June 2006. Retrieved 21 November 2009.
  • Taylor, John W.R. Jane's All The World's Aircraft 1982–83. London:Jane's Yearbooks, 1982. {{ISBN|0-7106-0748-2}}.
  • Whitaker, Richard. "[http://www.flightglobal.com/pdfarchive/view/1981/1981%20-%204020.html Lear Fan: the plastic aeroplane arrives]". Flight International, 26 December 1981, pp. 1896–1901.

{{refend}}