SE5A
experimental aircraft pictures, SE5A amateur built aircraft
specifications, SE5A 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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SE5A pictures and
specifications, images of the
SE5A amateur built experimental homebuilt aircraft
specifications and data.
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SE5A pictures, images
and specifications for the
SE5A
amateur built experimental homebuilt aircraft.
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Loehle SE5A
Performance Specifications
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Fuel Capacity: |
10
gal |
38 L |
| Range: |
174 nm |
322 km |
200 mi |
| Cruise: |
57 kts |
106 kmh |
66 mph |
| Stall: |
19 kts |
35 kmh |
22 mph |
| Climb: |
1,000 ft/min |
5.1 m/sec |
| Ceiling: |
12,500 ft |
3,810 m |
| Takeoff
Distance: |
75 ft |
23
m |
| Landing
Distance: |
150 ft |
46
m |
Loehle SE5A
Specifications
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| Gross
Weight: |
525 lbs |
238 kg |
| Empty
Weight: |
265 lbs |
120 kg |
| Useful
Load: |
260 lbs |
118 kg |
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SE5A
Experimental Aircraft |
SE5A
Experimental Homebuilt Aircraft |
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To view the
pictures, images of the SE5A click on the smaller
images and they will enlarge. To return to the index page for the SE5A click on SE5A Index link, to view
video of the SE5A click on the Video link, to
return to the Main Index click on the UltralightNews link. |
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