Loehle P51 Mustang
experimental aircraft pictures, Loehle P51 Mustang amateur built aircraft
specifications, Loehle P51 Mustang 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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Loehle P51 Mustang pictures and
specifications, images of the
Loehle P51 Mustang amateur built experimental homebuilt aircraft
specifications and data.
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Loehle P51 Mustang pictures, images
and specifications for the
Loehle P51 Mustang
amateur built experimental homebuilt aircraft.
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Loehle P51 Mustang Specifications
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Empty Weight: |
513 lbs. |
| Gross Weight: |
885 lbs. |
| Wing Span: |
28.8 ft. |
| Wing Area: |
130 sq. ft. |
Loehle P51 Mustang Performance Specifications
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| Engine: |
582 Rotax |
| Cruise Speed: |
75 m.p.h. |
| Stall Speed: |
30 m.p.h. |
| VNE: |
100 m.p.h. |
| Construction: |
Wood |
| Building time: |
500 Hrs. |
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Loehle P51 Mustang
Experimental Aircraft |
Loehle P51 Mustang
Experimental Homebuilt Aircraft |
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To view the
pictures, images of the Loehle P51 Mustang click on the smaller
images and they will enlarge. To return to the index page for the Loehle P51 Mustang click on Loehle P51 Mustang Index link, to view
video of the Loehle P51 Mustang click on the Video link, to
return to the Main Index click on the UltralightNews link. |
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