{{short description|1920s French aircraft}} <!-- This article is a part of Wikipedia:WikiProject Aircraft. Please see Wikipedia:WikiProject Aircraft/page content for recommended layout. --> {{Infobox aircraft | name = Romano R.3 | logo = | logo_size = | image = | alt = | caption = | long_caption = | other_names = | aircraft_type = Experimental seaplane | aim = | outcome = | related = | national_origin = France | manufacturer = Chantiers aéronavals Étienne Romano | design_group = | designer = | builder = | issuer = | status = | owners = | primary_user = | more_users = | service = | major_applications = | proposals = | prototypes = | number_built = 1 | construction_number = | civil_registration = | military_serial = | radio_code = | requirement = | aircraft_carried = | flights = | total_hours = | total_distance = | construction_date = | introduction = | retired = | first_flight = 1924 | initiated = | in_service = | last_flight = | expected = | developed_from = | variants = | developed_into = | preservation = | fate = | predecessors = | successors = | concluded = }}
The '''Romano R.3''' was a French experimental seaplane built by Romano in the 1920s. It featured a biplane layout.
==Specifications== {{Aircraft specs |ref=<ref>{{cite web|url=https://www.aviafrance.com/romano-r-3-aviation-france-9406.htm |title=Romano R.3 - Hydravion expérimental - Un siècle d'aviation française |publisher=Aviafrance.com |date=2003-08-27 |accessdate=2019-02-26}}</ref> |prime units?=met <!-- General characteristics --> |genhide=
|crew=Two |length m=7.80 |length note= |span m=11.00 |span note= |height m=3.70 |height note= |wing area sqm=30.00 |wing area note= |aspect ratio= |airfoil= |gross weight kg=1020 |gross weight note= |max takeoff weight kg= |max takeoff weight lb= |max takeoff weight note= |fuel capacity= |lift note= |more general= <!-- Powerplant --> |eng1 number=1 |eng1 name=Hispano-Suiza 8Ab |eng1 type=V-8 water-cooled piston engine |eng1 hp=180 |more power=
|prop blade number= |prop name= |prop dia m=<!-- propeller aircraft --> |prop dia ft=<!-- propeller aircraft --> |prop dia in=<!-- propeller aircraft --> |prop dia note=
<!-- Performance --> |perfhide=
|max speed kmh=160 |max speed note= |cruise speed kmh= |cruise speed mph= |cruise speed kts= |cruise speed note= |stall speed kmh= |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= |minimum control speed kmh= |minimum control speed mph= |minimum control speed kts= |minimum control speed note= |range km= |range miles= |range nmi= |range note= |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=2000 |ceiling note=in 14 minutes |g limits=<!-- aerobatic --> |roll rate=<!-- aerobatic --> |glide ratio=<!-- sailplanes --> |climb rate ms= |climb rate ftmin= |climb rate note= |time to altitude= |lift to drag= |wing loading kg/m2= |wing loading lb/sqft= |wing loading note= |fuel consumption kg/km= |fuel consumption lb/mi= |power/mass= |thrust/weight=
|more performance= <!-- Armament --> |armament=<!-- add bulletted list here or if you want to use the following specific parameters, remove this parameter--> |guns= |bombs= |avionics= }}
==References== {{reflist}}
{{Romano aircraft}}
Category:1920s French experimental aircraft R.3 Category:Aircraft first flown in 1924 Category:Biplanes Category:Single-engined tractor aircraft Category:Floatplanes