{{Short description|Two-seat monoplane aircraft}} <!-- This article is a part of Wikipedia:WikiProject Aircraft. Please see Wikipedia:WikiProject Aircraft/page content for recommended layout. --> {{Infobox aircraft |name = Lancair 360 |image = Lancair360-cruise.jpg |caption = |type = Kit Plane |manufacturer = Lancair |designer = Lance A. Neibauer |first_flight = |introduction = |retired = |status = Operational |primary_user = Civilian |more_users = |produced = |number_built = |unit cost = |developed_from = Lancair 320 }}
The '''Lancair 360''' is a two-seat aircraft marketed in kit form. It is a low-wing monoplane of conventional configuration with retractable tricycle undercarriage. The Lancair Legacy was chosen to replace the Lancair 360 in 1999.<ref>{{cite journal|title=Flying Magazine|date=November 1999|page=36}}</ref> thumb|right|Lancair 360 MKII thumb|right|A Lancair 360 at Peachtree-Dekalb Regional Airport.
==Variants== *Lancair 360TC - Carbon Fiber Turbocharged <ref>{{cite journal|journal=Flying Magazine|date=July 1998|page=39}}</ref>
==Specifications (Lancair 360) == {{Aircraft specs |ref=''Lancair''<ref>{{cite web|url=http://www.lancair.com/media/builderupdates/235-320-360/320-360SPEC/320-360specs.pdf|website=Lancair.com|title=Lancair|url-status=dead|archive-url=https://web.archive.org/web/20141223101952/http://www.lancair.com/media/builderupdates/235-320-360/320-360SPEC/320-360specs.pdf|archive-date=2014-12-23}}</ref><!-- for givingthe reference for the data --> |prime units?=kts<!-- imp or kts first for US aircraft, and UK aircraft pre-metrification, met(ric) first for all others. You MUST choose a format, or no specifications will show -->
<!-- General characteristics --> |genhide= |crew=1 |capacity=2 |length m= |length ft= 21 |length in= |length note= |span m=7.162 |span ft= 23 |span in=6 |span note= |upper span m= |upper span ft= |upper span in= |upper span note= |mid span m= |mid span ft= |mid span in= |mid span note= |lower span m= |lower span ft= |lower span in= |lower span note= |swept m=<!-- swing-wings --> |swept ft=<!-- swing-wings --> |swept in=<!-- swing-wings --> |swept note= |dia m=<!-- airships etc --> |dia ft=<!-- airships etc --> |dia in=<!-- airships etc --> |dia note= |width m=<!-- if applicable --> |width ft=<!-- if applicable --> |width in=<!-- if applicable --> |width note= |height m= |height ft= |height in= |height note= |wing area sqm= |wing area sqft= 76 |wing area note= |swept area sqm=<!-- swing-wings --> |swept area sqft=<!-- swing-wings --> |swept area note= |volume m3=<!-- lighter-than-air --> |volume ft3=<!-- lighter-than-air --> |volume note= |aspect ratio=7.266 |airfoil=NASA NLF(1)-0215F |empty weight kg=495 |empty weight lb= 1090 |empty weight note=Varies, based on Engine and Options |gross weight kg=765 |gross weight lb= 1685 |gross weight note= |max takeoff weight kg= |max takeoff weight lb= |max takeoff weight note= |fuel capacity=40-44 gal |lift kg=<!-- lighter-than-air --> |lift lb=<!-- lighter-than-air --> |lift note= |more general= <!-- Powerplant --> |eng1 number=1 |eng1 name= IO-320/IO360 |eng1 type= Lycoming |eng1 kw=<!-- prop engines --> |eng1 hp=160-180 |eng1 kn=<!-- jet/rocket engines --> |eng1 lbf=<!-- jet/rocket engines --> |eng1 note= |power original= |thrust original= |eng1 kn-ab=<!-- afterburners --> |eng1 lbf-ab=<!-- afterburners --> |eng2 number= |eng2 name= |eng2 type= |eng2 kw=<!-- prop engines --> |eng2 hp=<!-- prop engines --> |eng2 kn=<!-- jet/rocket engines --> |eng2 lbf=<!-- jet/rocket engines --> |eng2 note= |eng2 kn-ab=<!-- afterburners --> |eng2 lbf-ab=<!-- afterburners --> |eng3 number= |eng3 name= |eng3 type= |eng3 kw=<!-- prop engines --> |eng3 hp=<!-- prop engines --> |eng3 kn=<!-- jet/rocket engines --> |eng3 lbf=<!-- jet/rocket engines --> |eng3 note= |eng3 kn-ab=<!-- afterburners --> |eng3 lbf-ab=<!-- afterburners --> |more power= |prop blade number=2 or 3<!-- propeller aircraft --> |prop name= |prop dia m=<!-- propeller aircraft --> |prop dia ft=<!-- propeller aircraft --> |prop dia in=<!-- propeller aircraft --> |prop dia note= |rot number=<!-- helicopters --> |rot dia m=<!-- helicopters --> |rot dia ft=<!-- helicopters --> |rot dia in=<!-- helicopters --> |rot area sqm=<!-- helicopters --> |rot area sqft=<!-- helicopters --> |rot area note= <!-- Performance --> |perfhide= |max speed kmh= |max speed mph= 255-260 |max speed kts= |max speed note= |max speed mach=<!-- supersonic aircraft --> |cruise speed kmh= |cruise speed mph= 235 |cruise speed kts=205 |cruise speed note= |stall speed kmh=<!-- aerobatic --> |stall speed mph=68 |stall speed kts=59 |stall speed note=Landing Configuration |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=940-1180 |range miles= |range nmi= |range note=(75%, std/opt fuel) |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=<!-- if range unknown --> |ceiling m= |ceiling ft= |ceiling note= |g limits=+9.0 -4.5 |roll rate=<!-- aerobatic --> |glide ratio=<!-- sailplanes --> |climb rate ms= |climb rate ftmin= |climb rate note= |time to altitude= |sink rate ms=<!-- sailplanes --> |sink rate ftmin=<!-- sailplanes --> |sink rate note= |lift to drag= |wing loading kg/m2= |wing loading lb/sqft=22.17 |wing loading note= |disk loading kg/m2= |disk loading lb/sqft= |disk loading note= |power/mass=0.107 |thrust/weight= |more performance= |avionics= }}
==References== {{Commons category}} {{reflist}}
{{Lancair aircraft}}
360 Category:1980s United States civil utility aircraft Category:Homebuilt aircraft Category:Single-engined tractor aircraft Category:Low-wing aircraft Category:Single-engined piston aircraft Category:Aircraft with retractable tricycle landing gear