Scepter
experimental aircraft pictures, Scepter amateur built aircraft
specifications, Scepter 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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Scepter pictures and
specifications, images of the
Scepter amateur built experimental homebuilt aircraft
specifications and data.
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Scepter pictures, images
and specifications for the
Scepter
amateur built experimental homebuilt aircraft.
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Slipstream
Sceptre ultralight aircraft specifications |
Empty weight: |
425 lbs |
Useful load: |
475 lbs |
Gross weight: |
900 lbs |
Overall height: |
6’-3 1/2” |
Wing span: |
30’-8” |
Chord: |
6’-1” |
Wing area: |
179 sq ft |
Engine horsepower: |
40 hp |
TYPICAL
PERFORMANCE |
Cruise speed: |
55 mph |
VNE (never exceed): |
120 mph |
Glide ratio: |
12 to 1 |
Slipstream Sceptre ultralight aircraft performance
specifications |
Stall Speed: |
27 mph |
Rate of climb: |
750 fpm |
Take off roll: |
100 ft |
Service ceiling: |
9,000 ft |
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Scepter
Experimental Aircraft |
Scepter
Experimental Homebuilt Aircraft |
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To view the
pictures, images of the Scepter click on the smaller
images and they will enlarge. To return to the index page for the Scepter click on Scepter Index link, to view
video of the Scepter click on the Video link, to
return to the Main Index click on the UltralightNews link. |
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