{{short description|1930s 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.6 | logo = | logo_size = | image = | alt = | caption = | long_caption = | other_names = | aircraft_type = Civil transport | aim = | outcome = | related = | national_origin = French | 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 = 20 December 1932 | initiated = | in_service = | last_flight = | expected = | developed_from = | variants = Romano R.16 | developed_into = | preservation = | fate = | predecessors = | successors = | concluded = }}

The '''Romano R.6''' was a transport aircraft built by Romano in France in the early 1930s. It was a three engine, high wing monoplane transport of all-metal construction. A longer wing-span colonial police transport was also built as the '''Romano R.16'''.

==Specifications== {{Aircraft specs |ref=<ref>{{cite web |url=https://www.aviafrance.com/romano-r-6-aviation-france-9409.htm|title=Romano R-6 |author=Bruno Parmenier |date=2 December 2001 |publisher= |accessdate=2 March 2019}}</ref> |prime units?=met <!-- General characteristics --> |genhide=

|crew=Three |capacity=8 passengers |length m=13.90 |length note= |span m=19.64 |span note= |height m=3.27 |height note= |wing area sqm=63.00 |wing area note= |aspect ratio=<!-- sailplanes --> |airfoil= |empty weight kg=3047 |empty weight note= |gross weight kg=4473 |gross weight note= |max takeoff weight kg= |max takeoff weight lb= |max takeoff weight note= |fuel capacity= |more general= <!-- Powerplant --> |eng1 number=3 |eng1 name=Gnome & Rhône 7Kb |eng1 type=7-cylinder radials |eng1 hp=300 |eng1 note= |power original= |more power=

|prop blade number=2 |prop name=Ratier |prop dia m=<!-- propeller aircraft --> |prop dia ft=<!-- propeller aircraft --> |prop dia in=<!-- propeller aircraft --> |prop dia note=

<!-- Performance --> |perfhide=

|max speed kmh=216 |max speed note=at ground level |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=1000 |range note= |endurance=<!-- if range unknown --> |ceiling m=6850 |ceiling ft= |ceiling note= theoretical |g limits=<!-- aerobatic --> |roll rate=<!-- aerobatic --> |glide ratio=<!-- sailplanes --> |climb rate ms= |climb rate ftmin= |climb rate note= |time to altitude= |sink rate ms=<!-- sailplanes --> |sink rate ftmin=<!-- sailplanes --> |sink rate note= |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= }}

==References== {{reflist}}

<!-- ==Further reading== --> <!-- ==External links== -->

{{Romano aircraft}}

Category:1930s French civil aircraft R.6 Category:Trimotors Category:High-wing aircraft Category:Aircraft first flown in 1932