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词条 Breda-Pittoni BP.471
释义

  1. Design and development

  2. Operators

  3. Specifications (B.P.471)

  4. References

  5. External links

name = B.P.471image =Breda Pittoni B P 471 I-BIPI.jpgcaption =

}}{{Infobox Aircraft Type

type = Utility transport/airlinermanufacturer = Bredadesigner = Mario Pittonifirst flight = 1950introduced =retired = 1954[1]status =primary user =more users =produced =number built = 1unit cost =developed from =variants with their own articles =
}}

The Breda-Pittoni B.P.471 was an Italian twin-engine airliner/military transport produced by Breda.

Design and development

As part of its efforts to get back into aircraft manufacturing following the war, Breda commissioned Mario Pittoni to develop a twin-engine medium transport designated the Breda-Pittoni B.P.471. The prototype first flew in 1950. It was an all-metal twin-engine monoplane of stressed-skin construction. It had a retractable tricycle undercarriage and wings were of an inverted-gull configuration, this allowed the main landing gear to be short and light. The cabin had room for 18-passengers or freight. The company proposed many uses for the aircraft including a civil airliner and freighter, military navigation trainer or utility freighter. With no interest from buyers the prototype was operated by the Italian Air Ministry as a staff transport.

Operators

{{ITA}}
  • Italian Air Force

Specifications (B.P.471)

{{Aircraft specs
|ref=Jane's All The World's Aircraft 1951–52[2]
|prime units?=met


|genhide=
|crew=2
|capacity=18 passengers
|length m=17.5
|length ft=
|length in=
|span m=23.0
|span ft=
|span in=
|height m=5.75
|height ft=
|height in=
|wing area sqm=
|wing area sqft=
|empty weight kg=
|empty weight lb=
|gross weight kg=10000
|gross weight lb=
|fuel capacity=


|eng1 number=2
|eng1 name=Pratt & Whitney R-1830-92 Twin Wasp
|eng1 type=14-cylinder air-cooled radial engine
|eng1 kw=
|eng1 hp=1200
|eng1 note= (take off power), {{convert|1050|hp|kW|abbr=on|order=flip}} at {{convert|7500|ft|m|abbr=on|order=flip}}


|perfhide=
|max speed kmh=473
|max speed mph=
|max speed kts=
|cruise speed kmh=412
|cruise speed mph=
|cruise speed kts=
|range km=2000
|range miles=
|range nmi=
|range note= at {{convert|395|km/h|mph kn|abbr=on}}
|ceiling m=7500
|ceiling ft=
|climb rate ms=
|climb rate ftmin=
|time to altitude=9 min 39 sec to {{convert|4000|m|ft|-2|abbr=on}}
|more performance=
|avionics=
}}

References

1. ^aeroflight
2. ^Bridgman 1951, p. 154c.
  • {{cite book|last=Bridgman|first=Leonard|title=Jane's All The World's Aircraft 1951–52|year=1951|publisher=Sampson Low, Marston & Company, Ltd.|location=London}}
  • {{cite book |last= |first= |authorlink= |title= The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985)|year= |publisher= Orbis Publishing|location= |issn=}}

External links

{{commons category|Breda-Pittoni BP.471}}
  • BP.471
  • The Breda wind tunnel by Mario Pittoni Technical Memorandum for Naca 1939 - from NASA Technical Reports Server
{{Breda aircraft}}

6 : Italian airliners 1950–1959|Italian military transport aircraft 1950–1959|Breda aircraft|Aircraft first flown in 1950|Mid-wing aircraft|Twin piston-engined tractor aircraft

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