{{Short description|1920s German seaplane airliner}} __NOTOC__ <!-- This article is a part of Wikipedia:WikiProject Aircraft. Please see Wikipedia:WikiProject Aircraft/page content for recommended layout. --> {{Infobox aircraft | name = V 101 Jasmund | logo = | logo_size = | image = | alt = | caption = | long_caption = | other_names = | aircraft_type = Floatplane airliner | aim = | outcome = | related = | national_origin = Germany | manufacturer = LFG | design_group = | designer = | builder = | issuer = | status = | 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 = | retired = | first_flight = ca. 1926 | initiated = | in_service = | last_flight = | expected = | developed_from = | variants = | developed_into = | preservation = | fate = | predecessors = | successors = | concluded = }}

The '''LFG V 101 Jasmund''' (named for Jasmund on Rügen) was a seaplane airliner produced in small quantities in Germany in the 1920s. It was a conventional, strut-braced, low-wing monoplane with an enclosed cabin for five passengers, an enlarged, metal development of the V 20 Arkona<ref name="Jane's">Taylor 1989, 577</ref> (of which a metal version had already been flown).

The V 101 was produced to operate alongside the V 13s and V 20s in service with Luft-Fahrzeug and Luftverkehr Pommern on seaplane routes in North Germany from 1926, possibly in favour of the V 59 that had been considered for this role.<ref name="Jane's" />

==Specifications== {{Aircraft specs |prime units? = met |crew=One pilot |capacity=5 passengers |length m=9.85 |length ft=32 |length in=4 |span m=15.65 |span ft=51 |span in=4 |height m=3.60 |height ft=11 |height in=10 |wing area sqm=40.0 |wing area sqft=430 |empty weight kg=1,300 |empty weight lb=2,860 |gross weight kg=1,950 |gross weight lb=4,290 |eng1 number=1 |eng1 name=Armstrong Siddeley Puma |eng1 kw=<!-- prop engines -->180 |eng1 hp=<!-- prop engines -->240 |max speed kmh=170 |max speed mph=110 |stall speed kmh=<!-- aerobatic and STOL aircraft -->150 |stall speed mph=<!-- aerobatic and STOL aircraft -->94 |range km=680 |range miles=425 |ceiling m=3,500 |ceiling ft=11,500 |climb rate ms=2.1 |climb rate ftmin=410 }} <!-- ==See also== --> {{aircontent <!-- include as many lines are appropriate. additional lines/entries with carriage return. --> |see also= |related=<!-- related developments --> |similar aircraft=<!-- similar or comparable aircraft --> |lists=<!-- related lists --> }}

==Notes== {{reflist}}

==References== * {{cite book |last= Taylor |first= Michael J. H. |title=Jane's Encyclopedia of Aviation |year=1989 |publisher=Studio Editions |location=London }} * [http://www.histaviation.com/LFG_V_101.html German aviation between 1939-1945] {{Webarchive|url=https://web.archive.org/web/20080601121810/http://www.histaviation.com/LFG_V_101.html |date=2008-06-01 }} <!-- ==External links== -->

{{LFG aircraft}}

Category:1920s German airliners Category:Floatplanes Category:LFG aircraft Category:Single-engined tractor aircraft Category:Low-wing aircraft