Airdrome Aeroplanes Fokker D-V111
experimental aircraft pictures, Airdrome Aeroplanes Fokker D-V111 amateur built aircraft
images, Airdrome Aeroplanes Fokker D-V111 homebuilt plane 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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Airdrome Aeroplanes Fokker D-V111 pictures, images of the
Airdrome Aeroplanes Fokker D-V111 ultralight, experimental, lightsport aircraft.
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Airdrome Aeroplanes Fokker D-V111 pictures, images of the
Airdrome Aeroplanes
Fokker D-V111 ultralight, experimental, lightsport aircraft.
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Airdrome
Aeroplanes Fokker D-VIII Performance
Specifications
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| Horsepower: |
52
hp |
| Fuel
Capacity: |
5 gal |
19
L |
| Range: |
105 nm |
194 km |
121 mi |
| Cruise: |
70 kts |
130 kmh |
81 mph |
| Stall: |
28 kts |
52 kmh |
32 mph |
| Climb: |
1,120 ft/min |
5.7 m/sec |
| Ceiling: |
10,000 ft |
3,048 m |
| Takeoff
Distance: |
115 ft |
35
m |
| Landing
Distance: |
300 ft |
91
m |
Airdrome
Aeroplanes Fokker D-VIII Specifications
|
| Gross
Weight: |
517 lbs |
235 kg |
| Empty
Weight: |
275 lbs |
125 kg |
| Useful
Load: |
242 lbs |
110 kg |
|
Wingspan: |
24
ft |
7.32 m |
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| Length: |
15.2 ft |
4.63 m |
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Airdrome Aeroplanes Fokker D-V111
Ultralight Aircraft |
Airdrome Aeroplanes Fokker D-V111
Experimental Aircraft |
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