P 40 Flying Tiger
experimental aircraft pictures, P 40 Flying Tiger amateur built aircraft
specifications, P 40 Flying Tiger 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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P 40 Flying Tiger pictures and
specifications, images of the
P 40 Flying Tiger amateur built experimental homebuilt aircraft
specifications and data.
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P 40 Flying Tiger pictures, images
and specifications for the
P 40 Flying Tiger
amateur built experimental homebuilt aircraft.
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Loehle Aircraft P40 Flying Tiger Specifications
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Empty Weight: |
513 lbs. |
| Gross Weight: |
885 lbs. |
| Wing Span: |
28.8 ft. |
| Wing Area: |
130 sq. ft. |
Loehle Aircraft P40 Flying Tiger 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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P 40 Flying Tiger
Experimental Aircraft |
P 40 Flying Tiger
Experimental Homebuilt Aircraft |
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To view the
pictures, images of the P 40 Flying Tiger click on the smaller
images and they will enlarge. To return to the index page for the P 40 Flying Tiger click on P 40 Flying Tiger Index link, to view
video of the P 40 Flying Tiger click on the Video link, to
return to the Main Index click on the UltralightNews link. |
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