{{Short description|American ultralight aircraft}} {{Use mdy dates|date=January 2022}} {{Use American English|date=January 2022}} <!-- This article is a part of Wikipedia:WikiProject Aircraft. Please see Wikipedia:WikiProject Aircraft/page content for recommended layout. --> {{Infobox aircraft | name = P-Craft | logo = | logo_size = | image = | alt = | caption = | long_caption = | other_names = | aircraft_type = Ultralight aircraft | aim = | outcome = | related = | national_origin = United States | manufacturer = Paup Aircraft | design_group = | designer = D. Paup | builder = | issuer = | status = Production completed | owners = | primary_user = | more_users = | service = | major_applications = | proposals = | prototypes = | number_built = | construction_number = | civil_registration = | military_serial = | radio_code = | requirement = | aircraft_carried = | flights = | total_hours = | total_distance = | construction_date = | introduction = 1982 | retired = | first_flight = | initiated = | in_service = | last_flight = | expected = | developed_from = | variants = | developed_into = | preservation = | fate = | predecessors = | successors = | concluded = }} The '''Paup P-Craft''' is an American ultralight aircraft that was designed by D. Paup and produced by Paup Aircraft, introduced in 1982. The aircraft was supplied as a kit for amateur construction.<ref name="Cliche">Cliche, Andre: ''Ultralight Aircraft Shopper's Guide'' 8th Edition, page E-2. Cybair Limited Publishing, 2001. {{ISBN|0-9680628-1-4}}</ref><ref name="VUM">{{Cite web|url = http://virtualultralightmuseum.com/op.htm#pcraft|title = P-Craft|accessdate = 7 December 2011|last = Virtual Ultralight Museum|date = n.d.}}</ref>
==Design and development== The P-Craft was designed to comply with the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of {{convert|254|lb|kg|0|abbr=on}}. The aircraft has a standard empty weight of {{convert|165|lb|kg|0|abbr=on}}. It features a strut-braced high-wing, a single-seat, open cockpit, conventional landing gear and a single engine in pusher configuration.<ref name="Cliche" /><ref name="VUM" />
The aircraft is made from aluminum tubing, with the aft fuselage welded steel tubing. Its tapered {{convert|32.5|ft|m|1|abbr=on}} span wing has no wing-mounted control surfaces. The wing is covered in doped aircraft fabric. Pitch is controlled conventionally, while yaw is controlled by the rudder, actuated by sideways movement of the control stick. The high degree of wing dihedral produces rolling motion from yaw coupling. The landing gear is bungee-suspended and the tailwheel is steerable. The single cylinder, two-stroke Cuyuna 215 {{convert|20|hp|kW|0|abbr=on}} engine is mounted behind the open pilot's seat, with the propeller rotating in between the top and bottom tail structural members.<ref name="Cliche" /> <!-- ==Operational history== --> <!-- ==Variants== --> <!-- ==Aircraft on display== -->
==Specifications (P-Craft) == {{Aircraft specs |ref=Cliche and the Virtual Ultralight Museum<ref name="Cliche" /><ref name="VUM" /> |prime units?=imp<!-- 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=one |capacity= |length m= |length ft= |length in= |length note= |span m= |span ft=32 |span in=6 |span note= |height m= |height ft= |height in= |height note= |wing area sqm= |wing area sqft=132 |wing area note= |aspect ratio= |airfoil= |empty weight kg= |empty weight lb=165 |empty weight note= |gross weight kg= |gross weight lb=402 |gross weight note= |fuel capacity=<!-- {{convert|XX|u.s.gal}} --> |more general= <!-- Powerplant --> |eng1 number=1 |eng1 name=Cuyuna 215 |eng1 type=single cylinder two-stroke engine |eng1 kw=<!-- prop engines --> |eng1 hp=20<!-- prop engines -->
|prop blade number=<!-- propeller aircraft --> |prop name= |prop dia m=<!-- propeller aircraft --> |prop dia ft=<!-- propeller aircraft --> |prop dia in=<!-- propeller aircraft --> |prop note=
<!-- Performance --> |perfhide=
|max speed kmh= |max speed mph= |max speed kts= |max speed note= |cruise speed kmh= |cruise speed mph=40 |cruise speed kts= |cruise speed note= |stall speed kmh= |stall speed mph=22 |stall speed kts= |stall 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=<!-- if range unknown --> |ceiling m= |ceiling ft= |ceiling note= |g limits= |roll rate=<!-- aerobatic --> |glide ratio=<!-- sailplanes --> |climb rate ms= |climb rate ftmin=300 |climb rate note= |time to altitude= |sink rate ms= |sink rate ftmin= |sink rate note= |lift to drag= |wing loading kg/m2= |wing loading lb/sqft=3.05 |wing loading note= |power/mass= |thrust/weight= |more performance= |avionics= }}
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==References== {{reflist}}
Category:Ultralight aircraft