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词条 Aero-Service Panda
释义

  1. Design and development

  2. Operational history

  3. Variants

  4. Specifications (Panda Standard)

  5. See also

  6. References

  7. External links

name= Panda image=File:Aero-Service Panda artist's rendering.jpg caption=Artist's rendering of the Panda

}}{{Infobox Aircraft Type

 type=Ultralight aircraft national origin=Poland manufacturer=Aero-Service Jacek Skopiński designer= first flight=28 September 2016 introduced= retired= status=In production (2016) primary user= more users= produced= number built= program cost= unit cost= €49,900 (Panda Standard, 2015) developed from= variants with their own articles=
}}

The Aero-Service Panda is a Polish ultralight, designed and produced by Aero-Service Jacek Skopiński of Warsaw. The aircraft is supplied complete and ready-to-fly.[1][2][3][4]

Design and development

The Panda was designed to comply with the Fédération Aéronautique Internationale microlight rules. It features a cantilever high-wing, a T-tail, a two-seats-in-side-by-side configuration enclosed cabin, fixed tricycle landing gear and a single engine in tractor configuration.[1][2][3][4]

The aircraft is made from sheet aluminum, with some parts, such as the engine cowling and wing tips made from composites. Its {{convert|8.91|m|ft|1|abbr=on}} span wing employs a modified NACA 633-618 airfoil, has an area of {{convert|10.6|m2|sqft|abbr=on}} and flaps. The cabin width is {{convert|120|cm|in|0|abbr=on}}.[1][2][3][4][5]

The Panda prototype was first flown on 28 September 2011.[2][3][4]

Operational history

Reviewer Marino Boric described the design in a 2015 review as possessing visibility that "is good in all directions because of very large glassed surfaces". He also noted that it is "sold at a reasonable price".[1]

Variants

Panda Standard

Base model powered by a {{convert|80|hp|kW|0|abbr=on}} Rotax 912UL four-stroke powerplant.[1]

Panda Sport

Model powered by a {{convert|100|hp|kW|0|abbr=on}} Rotax 912ULS four-stroke powerplant.[1]

Panda Exclusive

Model powered by a {{convert|100|hp|kW|0|abbr=on}} Rotax 912ULS four-stroke powerplant plus with a Dynon glass cockpit and other options as standard.[1]

Specifications (Panda Standard)

{{Aircraft specs
|ref=Tacke and manufacturer[1][5]
|prime units?=met


|genhide=
|crew=one
|capacity=one passenger
|length m=6.62
|length ft=
|length in=
|length note=
|span m=8.91
|span ft=
|span in=
|span note=
|height m=2.32
|height ft=
|height in=
|height note=
|wing area sqm=10.6
|wing area sqft=
|wing area note=
|aspect ratio=
|airfoil=modified NACA 633-618
|empty weight kg=270
|empty weight lb=
|empty weight note=
|gross weight kg=472.5
|gross weight lb=
|gross weight note=
|fuel capacity={{convert|100|l}}
|more general=


|eng1 number=1
|eng1 name=Rotax 912UL
|eng1 type=four cylinder, liquid and air-cooled, four stroke aircraft engine
|eng1 kw=60
|eng1 hp=
|prop blade number=3
|prop name=composite
|prop dia m=
|prop dia ft=
|prop dia in=
|prop note=


|perfhide=
|max speed kmh=220
|max speed mph=
|max speed kts=
|max speed note=
|cruise speed kmh=190
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=62
|stall speed mph=
|stall speed kts=
|stall speed note=flaps down
|never exceed speed kmh=260
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|range km=1200
|range miles=
|range nmi=
|range note=with 45 minutes reserves
|endurance=
|ceiling m=3650
|ceiling ft=
|ceiling note=
|g limits=+4/-2
|roll rate=
|glide ratio=
|climb rate ms=6
|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=44.57
|wing loading lb/sqft=
|wing loading note=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}

See also

  • Aero-Service Puma

References

1. ^1 2 3 4 5 6 7 Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 20. Flying Pages Europe SARL, 2015. {{ISSN|1368-485X}}
2. ^1 2 3 Jackson, Paul (ed): Jane's All The World's Aircraft 2012-2013, pages 500-501. Jane's Information Group, 2012. {{ISBN|978 0 7106 30001}}
3. ^1 2 3 Jackson, Paul (ed): IHS-Jane's All The World's Aircraft 2013-2014, Development and Production, pages 502-504. Jane's Information Group, 2013. {{ISBN|978 0 7106 30407}}
4. ^1 2 3 Jackson, Paul (ed): IHS-Jane's All The World's Aircraft 2014-2015, Development and Production, pages 520-521. Jane's Information Group, 2014. {{ISBN|978-0710631350}}
5. ^1 {{cite web|url = http://www.aero-service.com/airplanes/dane_panda|title = Technical data and performance|accessdate = 17 December 2016|author = Aero-Service Jacek Skopiński |year = 2010}}

External links

{{Commons category|Skopiński Panda}}
  • {{Official website|http://www.aero-service.com/airplanes/dane_panda}}

3 : Aero-Service aircraft|Polish ultralight aircraft 2010–2019|Single-engined tractor aircraft
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