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Paladin Golden Eagle

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In this page talks about ( Paladin Golden Eagle ) It was sent to us on 25/07/2021 and was presented on 25/07/2021 and the last update on this page on 25/07/2021

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The Paladin Golden Eagle is an American powered parachute, that was designed and produced by Paladin Industries of Pennsauken, New Jersey.Downey, Julia: 2000 Trike and 'Chute Directory, Kitplanes, Volume 17, Number 2, February 2000, page 50. Kitplanes Acquisition Company. ISSN 0891-1851Cliche, Andre: Ultralight Aircraft Shopper's Guide 8th Edition, page D-9. Cybair Limited Publishing, 2001. Bertrand, Noel; Rene Coulon; et al: World Directory of Leisure Aviation 2003-04, page 83. Pagefast Ltd, Lancaster OK, 2003. ISSN 1368-485X
The company's website was removed in 2012, the company seems to have gone out of business and production ended.

Design and development

The Golden Eagle was designed as a US FAR 103 Ultralight Vehicles two-seat trainer. It features a parachute-style high-wing, two-seats-in-tandem accommodation, tricycle landing gear and a single Hirth 2706 engine in pusher configuration. The Rotax 582 engine is a factory option.
The aircraft carriage is constructed from a combination of bolted aluminium and 4130 steel tubing. In flight steering is accomplished via a weight-shift tilt-bar that actuates the canopy brakes, creating roll and yaw. On the ground the aircraft has lever-controlled nosewheel steering. The factory-provided canopy is an Apco Ram Air with an area of . The landing gear incorporates independent hydraulic struts for suspension. The aircraft was factory supplied in the form of an assembly kit that required 50 hours to complete.

Specifications (Golden Eagle)

{{Aircraft specs
prime units?=imp
capacity=one passenger
length m=
length ft=11
length in=0
length note=
span m=
span ft=35
span in=6
span note=
height m=
height ft=6
height in=8
height note=
wing area sqm=
wing area sqft=500
wing area note=
aspect ratio=
empty weight kg=
empty weight lb=340
empty weight note=
gross weight kg=
gross weight lb=850
gross weight note=
fuel capacity=
more general=
eng1 number=1
eng1 name=Hirth 2706
eng1 type=twin cylinder, two-stroke, air-cooled aircraft engine
eng1 kw=
eng1 hp=65
prop blade number=
prop name=
prop dia m=
prop dia ft=
prop dia in=
prop note=
max speed kmh=
max speed mph=
max speed kts=
max speed note=
cruise speed kmh=
cruise speed mph=28
cruise speed kts=
cruise speed note=
stall speed kmh=
stall speed mph=
stall speed kts=
stall speed note=
never exceed speed kmh=
never exceed speed mph=
never exceed speed kts=
never exceed speed note=
range km=
range miles=
range nmi=
range note=
ceiling m=
ceiling ft=10000
ceiling note=
g limits=
roll rate=
glide ratio=3.81:1
climb rate ms=
climb rate ftmin=500
climb rate note=
time to altitude=
sink rate ms=
sink rate ftmin=600
sink rate note=
lift to drag=
wing loading kg/m2=
wing loading lb/sqft=1.7
wing loading note=
more performance=

External links

  • Category:1990s United States ultralight aircraft
    Category:Single-engined pusher aircraft
    Category:Powered parachutes

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