Breda A.2

{{short description|Early 20th century aircraft}}

{{Infobox aircraft

|name=A.2

|image=File:Breda_A.2_3-view_L'Air_April_15,1927.png

|caption=

|type=Sports plane

|manufacturer=Breda

|designer=

|first_flight= 1921

|introduction=

|retired=

|status=

|primary_user=

|more_users=

|produced=

|number_built=

|variants=

}}

The Breda A.2 was a small sport and touring aircraft developed in Italy in 1921.

Design and development

An advanced design for its time, the A.2 was a low-wing cantilever monoplane with fixed tailskid undercarriage. The pilot and passenger sat in tandem, open cockpits. Originally powered by an inverted inline engine of 97 kW (130 hp), a more powerful version was developed with a 187 kW (250 hp) engine as a reconnaissance aircraft.

Operators

;{{flag|Kingdom of Italy}}

Specifications (variant)

{{Aircraft specs

|ref=

|prime units?=met

|crew=2

|capacity={{convert|340|kg|lb|abbr=on}}

|length m=

|length ft=

|length in=

|length note=

|span m=

|span ft=

|span in=

|span note=

|height m=

|height ft=

|height in=

|height note=

|wing area sqm=34

|aspect ratio=

|airfoil=

|empty weight kg=950

|gross weight kg=1400

|fuel capacity=

|more general=

|eng1 number=1

|eng1 name=inverted in-line engine

|eng1 type=

|eng1 kw=

|eng1 hp=130

|eng1 shp=

|eng1 kn=

|eng1 lbf=

|eng1 note= - {{convert|250|hp|kW|abbr=on|disp=flip}}

|power original=

|thrust original=

|eng1 kn-ab=

|eng1 lbf-ab=

|prop blade number=

|prop name=

|prop dia m=

|prop dia ft=

|prop dia in=

|prop dia note=

|perfhide=

|max speed kmh=

|max speed mph=

|max speed kts=

|max speed note=

|max speed mach=

|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=

|ceiling m=6000

|ceiling ft=

|ceiling note=

|g limits=

|roll rate=

|glide ratio=

|climb rate ms=

|climb rate ftmin=

|climb rate note=

|time to altitude=

|sink rate ms=

|sink rate ftmin=

|sink rate note=

|lift to drag=

|wing loading kg/m2=

|wing loading lb/sqft=

|wing loading note=

|disk loading kg/m2=

|disk loading lb/sqft=

|disk loading note=

|fuel consumption kg/km=

|fuel consumption lb/mi=

|power/mass=

|thrust/weight=

|more performance=

}}

References

{{commons category}}

{{Reflist}}

  • {{cite book |last= Taylor |first= Michael J. H. |title=Jane's Encyclopedia of Aviation |year=1989 |publisher=Studio Editions |location=London |pages=195 }}
  • {{cite book |last= Gunston |first= Bill |title=World Encyclopedia of Aircraft Manufacturers |year=1993 |publisher=Naval Institute Press |location= Annapolis |pages=56 }}

{{Breda aircraft}}

{{Portal bar|Italy|Companies|Aviation}}

A.2

Category:1920s Italian sport aircraft

Category:Single-engined tractor aircraft

Category:Low-wing aircraft

Category:Aircraft first flown in 1921