<!-- This article is a part of Wikipedia:WikiProject Aircraft. Please see Wikipedia:WikiProject Aircraft/page content for recommended layout. --> {{Infobox aircraft | name = R.120 | logo = | logo_size = | image = | alt = | caption = | long_caption = | other_names = | aircraft_type = Bomber | aim = | outcome = | related = | national_origin = France | manufacturer = Chantiers aéronavals Étienne Romano | design_group = | designer = Etienne Romano | builder = | issuer = | status = | owners = | primary_user = French Air Force (intended) | 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 = 1938 | initiated = | in_service = | last_flight = | expected = | developed_from = | variants = | developed_into = | preservation = | fate = | predecessors = | successors = | concluded = }}

The '''Romano R.120''' was a twin-engine 4-seat bomber aircraft designed by Etienne Romano in the 1930s.

==Specifications== {{Aircraft specs |ref=Aviafrance: Romano R.120<ref name="avfrr110">{{cite web |last1=Parmentier |first1=Bruno |title=Romano R-120 |url=https://www.aviafrance.com/aviafrance1.php?ID=9402&ID_CONSTRUCTEUR=1116&ANNEE=0&ID_MISSION=0&MOTCLEF= |website=Aviafrance |accessdate=2 March 2019 |location=Paris |language=Fr |date=30 November 2001}}</ref> |prime units?=met <!-- General characteristics --> |crew=4 |capacity= |length m=16.1 |span m=21.1 |upper span m= |mid span m= |lower span m= |width m= |height m=4.25 |wing area sqm=58 |aspect ratio=<!-- sailplanes --> |airfoil= |empty weight kg=4800 |gross weight kg=9100 |max takeoff weight kg= |fuel capacity= |more general= <!-- Powerplant --> |eng1 number=2 |eng1 name=Hispano-Suiza 14AA |eng1 type=14-cylinder two-row air-cooled radial piston engine |eng1 hp=980

|prop blade number=<!-- propeller aircraft --> |prop name= |prop dia m=<!-- propeller aircraft --> |prop dia ft=<!-- propeller aircraft --> |prop dia in=<!-- propeller aircraft --> |prop dia note= <!-- Performance --> |max speed kmh=520 |max speed mach=<!-- supersonic aircraft --> |cruise speed kmh= |stall speed kmh= |never exceed speed kmh= |minimum control speed kmh= |range km=1400 |combat range km= |ferry range km= |endurance=<!-- if range unknown --> |ceiling m=9000 |g limits=<!-- aerobatic --> |roll rate=<!-- aerobatic --> |climb rate ms= |time to altitude= |wing loading kg/m2= |fuel consumption kg/km= |power/mass= |thrust/weight=

|more performance= <!-- Armament --> |guns= **2 x {{cvt|7.5|mm|3}} MAC 1934 in the nose turret **1 x {{cvt|7.5|mm|3}} MAC 1934 in a ventral position **1 x {{cvt|20|mm|3}} Hispano-Suiza HS-404 in a dorsal turret

|bombs= {{cvt|1000|kg}} of bombs }}

==References== {{reflist}}

==External links== *[https://www.aviastar.org/air/france/romano_r-120.php]

{{Romano aircraft}}

Category:1930s French bomber aircraft R.1w0 Category:Twin piston-engined tractor aircraft