Sultan, you wrote:
"As to your other post on how a tilt rotor handles a failed interconnect shaft they are call standard inputs to cyclic, pedal, and thrust lever (collective to you)"
Not quite the case OEI, is it?
Thanks,
John Dixson
No its not! Nor was it ever claimed! Nor the case TEI, is it? I completely fail to see the relevence of that post here.
We talk about and basically verify the fact that the ISS does not need to be intact during normal flight/both engines operating. Therefore, the argument has now shifted to the fact that if the ISS fails, AND the V22 goes OEI, there will be trouble.
Gee, ya think so???