- Design and development
- Specifications (Qualt 201)
- References
- External links
| name=FMP Qualt 201 | image=Qualt 200L AN1599893.jpg | caption=Qualt 200 }}{{Infobox Aircraft Type | type=Ultralight aircraft and Light-sport aircraft | national origin=Czech Republic | manufacturer=FMP s.r.o. | designer= | first flight= | introduced= | retired= | status=In production | primary user= | more users= | produced= | number built= | program cost= | unit cost= €48,000 (assembled, 2015) | developed from= FMP Qualt 200 | variants with their own articles=
}} |
The FMP Qualt 201 is a Czech ultralight and light-sport aircraft, designed and produced by FMP s.r.o. of Prague. The aircraft is supplied as a complete ready-to-fly-aircraft.[1][2] Design and developmentThe Qualt 201 was derived from the earlier FMP Qualt 200, which it replaced in production. The 201 was designed to comply with the Fédération Aéronautique Internationale microlight rules and US light-sport aircraft rules. It features a cantilever low-wing, a two-seats-in-side-by-side configuration enclosed open cockpit under a bubble canopy, fixed conventional landing gear, a T-tail and a single engine in tractor configuration.[1][2] The aircraft is made from composites. Its {{convert|9.2|m|ft|1|abbr=on}} span wing has an area of {{convert|10.5|m2|sqft|abbr=on}} and mounts split-style flaps. Standard engines available are the {{convert|64|hp|kW|0|abbr=on}} Rotax 582 two-stroke, the {{convert|80|hp|kW|0|abbr=on}} Rotax 912UL, the {{convert|100|hp|kW|0|abbr=on}} Rotax 912ULS and the {{convert|85|hp|kW|0|abbr=on}} Jabiru 2200 four-stroke powerplants.[1][2] Specifications (Qualt 201) {{Aircraft specs
|ref=Bayerl[1]
|prime units?=met
|genhide=
|crew=one
|capacity=one passenger
|length m=
|length ft=
|length in=
|length note=
|span m=9.2
|span ft=
|span in=
|span note=
|height m=1.7
|height ft=
|height in=
|height note=
|wing area sqm=10.5
|wing area sqft=
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=280
|empty weight lb=
|empty weight note=
|gross weight kg=472.5
|gross weight lb=
|gross weight note=
|fuel capacity={{convert|48|l}}
|more general=
|eng1 number=1
|eng1 name=Jabiru 2200
|eng1 type=four cylinder, air-cooled, four stroke aircraft engine
|eng1 kw=
|eng1 hp=85
|prop blade number=
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=
|prop note=
|perfhide=
|max speed kmh=230
|max speed mph=
|max speed kts=
|max speed note=
|cruise speed kmh=170
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=60
|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=
|range km=
|range miles=
|range nmi=
|range note=
|endurance=
|ceiling m=
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=6
|climb rate ftmin=
|climb rate note=
|time to altitude=
|sink rate ms=
|sink rate ftmin=
|sink rate note=
|lift to drag=
|wing loading kg/m2=45.0
|wing loading lb/sqft=
|wing loading note=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}
References1. ^1 2 3 Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 55. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
2. ^1 2 Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 56. Flying Pages Europe SARL, 2015. {{ISSN|1368-485X}}
External links{{commons category|FMP Qualt}}- {{Official website|http://www.fmp.cz/}}
3 : Czech ultralight aircraft 2000–2009|Light-sport aircraft|Single-engined tractor aircraft |