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词条 Comte AC-4
释义

  1. Design and development

  2. Variants

  3. Operators

  4. Specifications (AC-4)

  5. See also

  6. References

  7. External links

name = AC-4 Gentlemanimage =Flugzeug HB-IKO.jpgcaption =

}}{{Infobox Aircraft Type

type = Two-seat sport/training aircraftnational origin = Switzerlandmanufacturer = Comtedesigner =first flight = 1927introduced =retired =status =primary user = Switzerlandmore users =produced =number built =unit cost =developed from =variants with their own articles =
}}

The Comte AC-4 Gentleman was a 1920s Swiss two-seat sport/training aircraft produced by Flugzeugbau A. Comte.

Design and development

In 1927 the Swiss company Flugzeugbau A. Comte designed and built a prototype two-seat cabin monoplane designated the AC-4 Gentleman. It was a braced high-wing monoplane with fixed tailwheel landing gear. It had staggered seats for two with an option for dual controls.

Variants

AC-4

Production version with a 115 hp (86 kW) Cirrus Hermes inline piston engine.

AC-4B

Second production batch with 140 hp (104 kW) Armstrong Siddeley Genet Major or 110 hp (82 kW) Cirrus Hermes, five built.

Operators

{{SUI}}
  • Swiss Air Force

Specifications (AC-4)

{{aerospecs
|met or eng?=eng
|crew=Two
|capacity=
|length m=8.05
|length ft=26
|length in=5
|span m=12.13
|span ft=39
|span in=9½
|swept m=
|swept ft=
|swept in=
|rot number=
|rot dia m=
|rot dia ft=
|rot dia in=
|dia m=
|dia ft=
|dia in=
|width m=
|width ft=
|width in=
|height m=2.90
|height ft=9
|height in=6
|wing area sqm=20
|wing area sqft=215.29
|swept area sqm=
|swept area sqft=
|rot area sqm=
|rot area sqft=
|volume m3=
|volume ft3=
|aspect ratio=
|empty weight kg=500
|empty weight lb=1,102
|gross weight kg=800
|gross weight lb=1,764
|lift kg=
|lift lb=
|eng1 number=1
|eng1 type=Cirrus Hermes inline piston
|eng1 kw=86
|eng1 hp=115
|eng1 kn=
|eng1 lbf=
|eng1 kn-ab=
|eng1 lbf-ab=
|eng2 number=
|eng2 type=
|eng2 kw=
|eng2 hp=
|eng2 kn=
|eng2 lbf=
|eng2 kn-ab=
|eng2 lbf-ab=
|max speed kmh=175
|max speed mph=109
|max speed mach=
|cruise speed kmh=140
|cruise speed mph=87
|range km=700
|range miles=435
|endurance h=
|endurance min=
|ceiling m=4000
|ceiling ft=13,125
|glide ratio=
|climb rate ms=
|climb rate ftmin=
|sink rate ms=
|sink rate ftmin=
|armament1=
|armament2=
|armament3=
|armament4=
|armament5=
|armament6=
}}

See also

{{aircontent|
|related=
  • Comte AC-8
  • Comte AC-12

|similar aircraft=
|lists=
|see also=
}}

References

  • {{cite book |last= |first= |authorlink= |coauthors= |title= The Illustrated Encyclopedia of Aircraft (Part Work 1982–1985)|year= |publisher= Orbis Publishing|location= |issn=}}

External links

{{commons category|Comte AC-4}}
  • Photos at airliners.net
{{Comte aircraft}}

4 : Swiss civil aircraft|Comte aircraft|Single-engined tractor aircraft|Aircraft first flown in 1927

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