Phantom
experimental aircraft pictures, Phantom amateur built aircraft
specifications, Phantom homebuilt aircraft specifications and photographs,
Ultralight News newsmagazine.
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Single place Part 103 ultralights in the United States are defined as single
place ultralight aircraft that weigh 254 lbs or less, have a stall speed
not more than 24 knots, a top
speed of 55 knots, and carry no more than 5 gallons of fuel. To fly a
legal Part 103
ultralight aircraft in the United States the pilot does not require a
pilot license.
Single place aircraft weighing more than 254 lbs. in the U.S. require a
pilots license and must be built as experimental, amateur built,
homebuilt aircraft. These include weight shift aircraft, more commonly
known as trikes, powered parachutes, and powered para-gliders.
Single place ultralights in Canada can weigh up to 1200 lbs. and an
ultralight pilots license is required to fly them.
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Phantom pictures and
specifications, images of the
Phantom amateur built experimental homebuilt aircraft
specifications and data.
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Phantom pictures, images
and specifications for the
Phantom
amateur built experimental homebuilt aircraft.
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Phantom experimental amateur built aircraft
specifications
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Empty Weight: |
250 lbs. |
| Gross Weight: |
510 lbs. |
| Wing Span: |
28.6" ft. |
| Wing Area: |
142 sq. ft. |
Phantom experimental amateur built aircraft
performance specifications
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| Engine: |
447 Rotax |
| Cruise Speed: |
55 m.p.h. |
| Stall Speed: |
27 m.p.h. |
| VNE: |
100 m.p.h. |
| Construction: |
aluminum
tube/Dacron fabric |
| Building time: |
150 Hrs. |
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Phantom
Experimental Aircraft |
Phantom
Experimental Homebuilt Aircraft |
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To view the
pictures, images of the Phantom click on the smaller
images and they will enlarge. To return to the index page for the Phantom click on Phantom Index link, to view
video of the Phantom click on the Video link, to
return to the Main Index click on the UltralightNews link. |
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