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词条 Fisher Boomerang
释义

  1. Development

  2. Specifications (Boomerang)

  3. See also

  4. References

{{about|the 1980s ultralight aircraft|the fighter aircraft| CAC Boomerang}}
name=Fisher Boomerang image= caption=

}}{{Infobox Aircraft Type

 type=Ultralight aircraft national origin=United States manufacturer=Fisher Flying Products designer=Michael E. Fisher first flight= introduced=mid-1982 retired= status=Production completed primary user= number built= developed from= variants with their own articles=
}}

The Fisher Boomerang is a single-seat conventional landing gear, high-winged monoplane ultralight aircraft designed by Michael Fisher and introduced in mid-1982.[1][2]

Development

The Boomerang was intended to meet the requirements of the US FAR 103 Ultralight Vehicles category, including that category's maximum {{convert|254|lb|kg|0|abbr=on}} empty weight. The aircraft has a standard empty weight of {{convert|190|lb|kg|0|abbr=on}}.[2]

The aircraft is a single-seat ultralight with a high wing and a conventional three-axis type with ailerons, elevators and rudder. The airframe structure is of 6061T6 and 2024T3 aluminum tube, covered with Stits Polyfibre aircraft fabric. The landing gear is of a fixed taildragger configuration without suspension on the {{convert|20|in|cm|0|abbr=on}} main wheels. Wings were available in several spans, from {{convert|28|to|32|ft|m|1|abbr=on}}, the longer span being used for the two seat variant.[1][2]

The Boomerang is fitted with a {{convert|30|hp|kW|0|abbr=on}} Kawasaki 340 engine as standard equipment or optionally a {{convert|40|hp|kW|0|abbr=on}} Kawasaki 440A engine, both with a reduction drive system. The aircraft has an empty weight of {{convert|190|lb|kg|0|abbr=on}} and a gross weight of {{convert|470|lb|kg|0|abbr=on}}, giving a useful load of {{convert|280|lb|kg|0|abbr=on}}.[1][2]

The aircraft was discontinued due to poor sales.[2]

Specifications (Boomerang)

{{Aircraft specs
|ref=Janes All the Worlds Aircraft 1983-84[1]
|prime units?=imp


|genhide=
|crew=one
|capacity=no passengers
|length m=
|length ft=
|length in=
|span m=
|span ft=28
|span in=0
|height m=
|height ft=
|height in=
|wing area sqm=
|wing area sqft=156
|aspect ratio=5.03:1
|airfoil=
|empty weight kg=
|empty weight lb=190
|gross weight kg=
|gross weight lb=470
|fuel capacity= 2.5 US gallons (9.5 l) standard, 5 US Gallons (19 l) optional


|eng1 number=1
|eng1 name=Kawasaki 440A
|eng1 type=two-stroke engine
|eng1 kw=
|eng1 hp=40
|prop blade number=2
|prop dia m=
|prop dia ft=4.5
|prop dia in=


|perfhide=Y
|max speed kmh=
|max speed mph=
|max speed kts=
|cruise speed kmh=
|cruise speed mph=
|cruise speed kts=
|range km=
|range miles=
|range nmi=
|ceiling m=
|ceiling ft=
|climb rate ms=
|climb rate ftmin=
|more performance=
|avionics=
}}

See also

{{aircontent
|see also=
|related=
|similar aircraft=
  • Beaujon Enduro
  • Beaujon Mach .07
  • Eipper Quicksilver
  • Fisher Barnstormer
  • Fisher Flyer
  • Jean St-Germain Raz-Mut

|lists=
}}

References

{{commons category|Fisher Flying Products aircraft}}
1. ^1 2 3 Taylor, John WR: Janes All the Worlds Aircraft 1983-84, Janes Publishing Company, 1983, p.660.
2. ^1 2 3 4 Cliche, Andre: Ultralight Aircraft Shopper's Guide 8th Edition, page E-7. Cybair Limited Publishing, 2001. {{ISBN|0-9680628-1-4}}
{{Fisher Flying Products}}

1 : United States ultralight aircraft 1980–1989
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