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{{One source|date=March 2019}}
__NOTOC__
<!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. -->
<!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. -->
{|{{Infobox Aircraft Begin
{|{{Infobox aircraft begin
|name=Campeiro
|name=Campeiro
|image=
|image=
|caption=
|caption=
}}{{Infobox Aircraft Type
}}{{Infobox aircraft type
|type=Utility monoplane
|type=Utility monoplane
|national origin=Brazil
|national origin=Brazil
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}}
|}
|}
The '''Neiva Campeiro''' is a [[Brazil]]ian two-seat utility monoplane built by [[Indústria Aeronáutica Neiva]] for the [[Brazilian Air Force]]. The Campeiro was based on the earlier [[CAP-4|Neiva Paulistinha 56]] with a re-designed structure and powered by a 150&nbsp;hp (112&nbsp;kW) [[Lycoming O-320|Avco Lycoming O-320-A]] piston engine. The Camperiro was a braced high-wing monoplane with a fixed tailwheel landing gear. Twenty aircraft were built for the Brazilian Air Force as the '''L-7 Campeiro''' and were used for liaison, observation, rescue and training.
The '''Neiva Campeiro''' is a Brazilian two-seat utility monoplane built by [[Indústria Aeronáutica Neiva]] for the [[Brazilian Air Force]]. The Campeiro was based on the earlier [[CAP-4|Neiva Paulistinha 56]] with a re-designed structure and powered by a 150&nbsp;hp (112&nbsp;kW) [[Lycoming O-320|Avco Lycoming O-320-A]] piston engine. The Camperiro was a braced high-wing monoplane with a fixed tailwheel landing gear. Twenty aircraft were built for the Brazilian Air Force as the '''L-7 Campeiro''' and were used for liaison, observation, rescue and training.


==Operators==
==Operators==
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==Specifications==
==Specifications==
{{Aircraft specs
{{aerospecs
|ref=<ref>Orbis 1985, page 2596</ref>
|ref=<ref>Orbis 1985, page 2596</ref>
|prime units? = met
|met or eng?=<!-- eng for US/UK aircraft, met for all others -->met

|crew=2
|crew=2
|capacity=
|length m=6.90
|length m=6.90
|length ft=22
|length ft=22
|length in=3¾
|length in=3.75
|span m=10.70
|span m=10.70
|span ft=35
|span ft=35
|span in=1¼
|span in=1.25
|swept m=<!-- swing-wings -->
|swept ft=<!-- swing-wings -->
|swept in=<!-- swing-wings -->
|rot number=<!-- helicopters -->
|rot dia m=<!-- helicopters -->
|rot dia ft=<!-- helicopters -->
|rot dia in=<!-- helicopters -->
|dia m=<!-- airships etc -->
|dia ft=<!-- airships etc -->
|dia in=<!-- airships etc -->
|width m=<!-- if applicable -->
|width ft=<!-- if applicable -->
|width in=<!-- if applicable -->
|height m=2.65
|height m=2.65
|height ft=8
|height ft=8
|height in=8¼
|height in=8.25
|wing area sqm=16.80
|wing area sqm=16.80
|wing area sqft=18.84
|wing area sqft=18.84
|swept area sqm=<!-- swing-wings -->
|swept area sqft=<!-- swing-wings -->
|rot area sqm=<!-- helicopters -->
|rot area sqft=<!-- helicopters -->
|volume m3=<!-- lighter-than-air -->
|volume ft3=<!-- lighter-than-air -->
|aspect ratio=<!-- sailplanes -->
|empty weight kg=491
|empty weight kg=491
|empty weight lb=1082
|empty weight lb=1082
|gross weight kg=790
|gross weight kg=790
|gross weight lb=1741
|gross weight lb=1741
|lift kg=<!-- lighter-than-air -->
|lift lb=<!-- lighter-than-air -->

|eng1 number=1
|eng1 number=1
|eng1 type=[[Lycoming O-320|Avco Lycoming O-320-A]] flat-four piston engine
|eng1 name=[[Lycoming O-320|Avco Lycoming O-320-A]] flat-four piston engine
|eng1 kw=<!-- prop engines -->112
|eng1 kw=<!-- prop engines -->112
|eng1 hp=<!-- prop engines -->150
|eng1 hp=<!-- prop engines -->150
|eng1 kn=<!-- jet/rocket engines -->
|eng1 lbf=<!-- jet/rocket engines -->
|eng1 kn-ab=<!-- afterburners -->
|eng1 lbf-ab=<!-- afterburners -->
|eng2 number=
|eng2 type=
|eng2 kw=<!-- prop engines -->
|eng2 hp=<!-- prop engines -->
|eng2 kn=<!-- jet/rocket engines -->
|eng2 lbf=<!-- jet/rocket engines -->
|eng2 kn-ab=<!-- afterburners -->
|eng2 lbf-ab=<!-- afterburners -->

|max speed kmh=215
|max speed kmh=215
|max speed mph=134
|max speed mph=134
|max speed mach=<!-- supersonic aircraft -->
|cruise speed kmh=<!-- if max speed unknown -->
|cruise speed mph=<!-- if max speed unknown -->
|range km=955
|range km=955
|range miles=535
|range miles=535
|endurance h=<!-- if range unknown -->
|endurance min=<!-- if range unknown -->
|ceiling m=
|ceiling ft=
|glide ratio=<!-- sailplanes -->
|climb rate ms=
|climb rate ftmin=
|sink rate ms=<!-- sailplanes -->
|sink rate ftmin=<!-- sailplanes -->

|armament1=
|armament2=
|armament3=
|armament4=
|armament5=
|armament6=
}}
}}


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{{reflist}}
{{reflist}}
;Bibliography
;Bibliography
* {{cite book |last= Taylor |first= Michael J. H. |title=Jane's Encyclopedia of Aviation |year=1989 |publisher=Studio Editions |location=London |pages= }}
* {{cite book |last= Taylor |first= Michael J. H. |title=Jane's Encyclopedia of Aviation |year=1989 |publisher=Studio Editions |location=London }}
*{{cite book |last= |first= |authorlink= |coauthors= |title= The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985)|year= |publisher= Orbis Publishing|location= |issn=}}
*{{cite book |title= The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985)|publisher= Orbis Publishing}}
<!-- ==External links== -->
<!-- ==External links== -->
{{Indústria Aeronáutica Neiva}}
{{FAB aircraft designations}}


[[Category:Neiva aircraft|Campeiro]]
[[Category:Neiva aircraft|Campeiro]]
[[Category:Brazilian civil utility aircraft 1960–1969]]
[[Category:1960s Brazilian civil utility aircraft]]
[[Category:Single-engined tractor aircraft]]
[[Category:Single-engined tractor aircraft]]
[[Category:High-wing aircraft]]
[[Category:High-wing aircraft]]
[[Category:Single-engined piston aircraft]]
[[Category:Aircraft with fixed conventional landing gear]]




Latest revision as of 17:28, 26 December 2024

Campeiro
Role Utility monoplane
National origin Brazil
Manufacturer Neiva
Primary user Brazilian Air Force
Number built 20
Developed from Neiva Paulistinha 56

The Neiva Campeiro is a Brazilian two-seat utility monoplane built by Indústria Aeronáutica Neiva for the Brazilian Air Force. The Campeiro was based on the earlier Neiva Paulistinha 56 with a re-designed structure and powered by a 150 hp (112 kW) Avco Lycoming O-320-A piston engine. The Camperiro was a braced high-wing monoplane with a fixed tailwheel landing gear. Twenty aircraft were built for the Brazilian Air Force as the L-7 Campeiro and were used for liaison, observation, rescue and training.

Operators

[edit]
 Brazil

Specifications

[edit]

Data from [1]

General characteristics

  • Crew: 2
  • Length: 6.90 m (22 ft 3.75 in)
  • Wingspan: 10.70 m (35 ft 1.25 in)
  • Height: 2.65 m (8 ft 8.25 in)
  • Wing area: 16.80 m2 (18.84 sq ft)
  • Empty weight: 491 kg (1,082 lb)
  • Gross weight: 790 kg (1,741 lb)
  • Powerplant: 1 × Avco Lycoming O-320-A flat-four piston engine , 112 kW (150 hp)

Performance

  • Maximum speed: 215 km/h (134 mph, 116 kn)
  • Range: 955 km (535 mi, 465 nmi)

See also

[edit]

Related development

References

[edit]
Wikimedia Commons has media related to Neiva aircraft.
Notes
  1. ^ Orbis 1985, page 2596
Bibliography
  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions.
  • The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing.


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