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<blockquote data-quote="ramaperez" data-source="post: 2270170" data-attributes="member: 28996"><p>esto es lo que aparece en varios foros y la wiki del avion.</p><p></p><p>"Because the MU-2 offers very high performance at a relatively low cost, some of its operators lack sufficient training and experience for such an advanced aircraft. The MU-2 has performance similar to a small jet, yet early pilot certification required only a simple endorsement from pilot certificates for much slower twin piston-engine aircraft. The fact that numerous MU-2 pilots were inexperienced at high speeds and high altitudes seems to have resulted in the high crash rate. Once a type certification was required for an MU-2 pilot certificate, the accident rate dropped to normal levels.</p><p></p><p>A design feature of the MU-2 is its high cruise speed, while having a low landing speed. This is accomplished by using full-span, double-slotted <a href="https://en.wikipedia.org/wiki/Flap_(aeronautics)">flaps</a> on the <a href="https://en.wikipedia.org/wiki/Trailing_edge">trailing edge</a> of the wing. These flaps give the MU-2 a wing area comparable to a <a href="https://en.wikipedia.org/wiki/Beechcraft_King_Air">Beechcraft King Air</a> in landing configuration, while having a wing area comparable to a light jet while in cruise mode. The full-span flaps meant that over-wing <a href="https://en.wikipedia.org/wiki/Spoiler_(aeronautics)">spoilers</a> were employed, instead of conventional <a href="https://en.wikipedia.org/wiki/Aileron">ailerons</a>."</p><p></p><p></p><p></p><p>El piloto rendio la multi a fines de octubre con Benelli en moron., le tomo examen el mismo inspector que yo rendi la ppa.. Desconozco cuantas horas totales llevaba.</p></blockquote><p></p>
[QUOTE="ramaperez, post: 2270170, member: 28996"] esto es lo que aparece en varios foros y la wiki del avion. "Because the MU-2 offers very high performance at a relatively low cost, some of its operators lack sufficient training and experience for such an advanced aircraft. The MU-2 has performance similar to a small jet, yet early pilot certification required only a simple endorsement from pilot certificates for much slower twin piston-engine aircraft. The fact that numerous MU-2 pilots were inexperienced at high speeds and high altitudes seems to have resulted in the high crash rate. Once a type certification was required for an MU-2 pilot certificate, the accident rate dropped to normal levels. A design feature of the MU-2 is its high cruise speed, while having a low landing speed. This is accomplished by using full-span, double-slotted [URL='https://en.wikipedia.org/wiki/Flap_(aeronautics)']flaps[/URL] on the [URL='https://en.wikipedia.org/wiki/Trailing_edge']trailing edge[/URL] of the wing. These flaps give the MU-2 a wing area comparable to a [URL='https://en.wikipedia.org/wiki/Beechcraft_King_Air']Beechcraft King Air[/URL] in landing configuration, while having a wing area comparable to a light jet while in cruise mode. The full-span flaps meant that over-wing [URL='https://en.wikipedia.org/wiki/Spoiler_(aeronautics)']spoilers[/URL] were employed, instead of conventional [URL='https://en.wikipedia.org/wiki/Aileron']ailerons[/URL]." El piloto rendio la multi a fines de octubre con Benelli en moron., le tomo examen el mismo inspector que yo rendi la ppa.. Desconozco cuantas horas totales llevaba. [/QUOTE]
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