Wing Ding-II Light Aircraft For Beginners Plans.

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Drawings<br>aircraft<br>Wing Ding-II +<br>manual for<br>building<br>Wing Ding-II<br>light aircraft<br>for beginners plans<br>Attention<br>.<br>I am selling<br>a reference to<br>a resource<br>(website)<br>where<br>you can download<br>absolutely free<br>drawings<br>.<br>For digital download only, the item physically will not be sent!<br>You accept that with the purchase!<br>This item is region free, you do not risk your Steam account (BAN)<br>I'll send<br>you a link<br>to download<br>the drawings<br>after your<br>payment.<br>An excellent and<br>detailed material<br>to build<br>ultralight<br>Whing Ding II<br>.<br>drawings.<br>I leave<br>a comment<br>for each of its<br>customers<br>and<br>hope<br>you<br>do the same.<br>For digital download only, the item physically won't be sent! You accept that with the purchase!<br>This example of the Whing Ding II ultralight aircraft by Aerospace Engineer R.W.Hovey was built around Christmas 1977 by Max Kroone, Graham Percy and Steven Samagalski. A brilliantly conceived microlight design which totally predates the now hugely popular ultralight aircraft category.<br>general characteristics<br>•<br>Crew:<br>one<br>• Length:<br>14 feet<br>(<br>4.3 m)<br>•<br>Wingspan:<br>17 feet<br>(<br>5.2 m)<br>•<br>Height: 5<br>feet 6 inches<br>(1.68<br>m)<br>•<br>Wing area<br>:<br>98<br>square meters (<br>9.1 m<br>2)<br>• Weight:<br>122<br>lbs<br>(55<br>kg)<br>• Gross weight:<br>300 pounds<br>(136<br>kg)<br>•<br>Fuel tank capacity<br>:<br>0.5<br>US gallons<br>(1.9 L<br>;<br>0.42<br>imp<br>gal)<br>•<br>Powerplant<br>:<br>1<br>× McCulloch MAC-<br>101<br>chain saw<br>motor<br>, 12.5<br>hp<br>(9.3<br>kw)<br>•<br>Screws:<br>2-blade<br>hand<br>carved wooden<br>propeller<br>performance<br>•<br>Maximum speed:<br>50<br>miles<br>/ h (<br>80 km / h;<br>43<br>kN)<br>•<br>Cruising Speed<br>:<br>40<br>miles<br>/ h<br>(35<br>kN<br>,<br>64 km / h<br>)<br>•<br>Stall speed<br>:<br>26<br>miles<br>/ h<br>(23<br>kN<br>, 42<br>km / h)<br>•<br>Range:<br>20<br>miles (<br>17<br>NMI;<br>32<br>km)<br>•<br>Ceiling:<br>4,000 m<br>(<br>1,219 m)<br>• G<br>constraints:<br>+ 3 /<br>-3<br>•<br>Rate of climb<br>:<br>100<br>ft /<br>min (<br>0.51<br>m<br>/ s)<br>Общие<br>особенности<br>Экипаж:<br>один<br>Длина:<br>14 футов (4,3 м)<br>Размах крыльев:<br>17 футов (5,2 м)<br>Рост:<br>5 футов 6 дюймов (1,68 м)<br>Площадь крыла:<br>98 кв.м (9,1 м<br>2)<br>Вес:<br>122 фунтов (55 кг)<br>Вес брутто:<br>300 фунтов (136 кг)<br>Емкость топливного ба