JDT Himax
experimental aircraft pictures, JDT Himax amateur built aircraft
specifications, JDT Himax 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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JDT Himax pictures and
specifications, images of the
JDT Himax amateur built experimental homebuilt aircraft
specifications and data.
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JDT Himax pictures, images
and specifications for the
JDT Himax
amateur built experimental homebuilt aircraft.
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JDT Mini Max Experimental Aircraft
Specifications
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Empty Weight: |
269 lbs. |
| Gross Weight: |
560 lbs. |
| Wing Span: |
25 ft. |
| Wing Area: |
112.5. sq. ft. |
JDT Mini Max Experimental Aircraft Performance
Specifications
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| Engine: |
447 Rotax |
| Cruise Speed: |
65 m.p.h. |
| Stall Speed: |
30 m.p.h. |
| VNE: |
100 m.p.h. |
| Construction: |
wood/fabric |
| Building time: |
400 Hrs. |
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JDT Himax
Experimental Aircraft |
JDT Himax
Experimental Homebuilt Aircraft |
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To view the
pictures, images of the JDT Himax click on the smaller
images and they will enlarge. To return to the index page for the JDT Himax click on JDT Himax Index link, to view
video of the JDT Himax click on the Video link, to
return to the Main Index click on the UltralightNews link. |
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