ANF Les Mureaux 160T
{{short description|1932 design French touring monoplane}}
| {{Infobox aircraft begin
| name = ANF Les Mureaux 160T | image = Mureaux 160T L'Aerophile Salon 1932.jpg | caption = }}{{Infobox aircraft type | type = Touring monoplane | national origin = France | manufacturer = ANF Les Mureaux | designer = | first flight = October 1932 | introduced = | retired = | status = | primary user = | number built = 1 | developed from = | variants with their own articles = }} |
The ANF Les Mureaux 160T was a French touring monoplane aircraft developed in the early 1930s and flown for the first time in October 1932, designed by the ANF Les Mureaux. It was a two-seat high-wing monoplane powered by a {{convert|95|hp|kW|0|abbr=on}} Renault 4Pb inline engine, it did not enter production.
Despite its advanced design for such a civilian-adjacent aircraft, the Mureaux 160T was not without its issues. Its engines were known to be underpowered, and it was considered to be somewhat slow and difficult to handle in flight. The flight characteristics of the aircraft turned out to be quite good, but its cost failed - there were no buyers for such a "suburban" aircraft. Only one was produced, and as a result, it was gradually phased out of service in the late 1930s, and it was largely replaced by more advanced aircraft.{{Cite web |title=Displaying Aircraft Type - Aviation Fanatic |url=https://aviationfanatic.com/ent_show.php?ent=4&AT_ID=__LM160 |access-date=2023-05-05 |website=aviationfanatic.com}}{{Cite web |title=ANF Mureaux 160T |url=http://www.airwar.ru/enc/law1/mureaux160.html |access-date=2023-05-05 |website=www.airwar.ru}}{{Cite web |title=Mureaux 160T |url=http://all-aero.com/index.php/contactus/53-planes-l-m-n-o/14963-mureaux-160t |access-date=2023-05-05 |website=all-aero.com}}
Specification
{{Aircraft specs
|prime units?=met
|genhide=
|crew=one
|capacity=one passenger
|length m=8.05
|length note=
|span m=13.60
|span note=
|height m=2.25
|height note=
|wing area sqm=17
|wing area sqft=
|wing area note=
|swept area sqm=
|swept area sqft=
|swept area note=
|aspect ratio=11
|airfoil=
|empty weight kg=480
|empty weight note=
|gross weight kg=820
|gross weight note=
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|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=
|lift kg=
|lift lb=
|lift note=
|more general=
|eng1 number=1
|eng1 name=Renault 4Pb
|eng1 type=4-cylinder inline
|eng1 hp=95
|more power=
|prop blade number=2
|prop name=
|prop dia m=
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|max speed kmh=205
|max speed mph=
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|max speed note=at ground level
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|range km=550
|range note= into {{convert|50|km/h|mph kn|abbr=on}} headwind
|endurance=
|ceiling m=7200
|ceiling note=
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|time to altitude=12 min to {{convert|3000|m|ft|abbr=on}}
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}}