Corsair 115
Penultimate Amazing
- Joined
- Apr 18, 2007
- Messages
- 14,519
Assuming the times and altitudes you posted are correct, let's do the math.Can a plane drop in altitude this fast and still stay in control.
8:58 AM 25,000 Feet
9:00 AM 18,500 Feet
9:02 AM 9,000 Feet
But then it hits the south tower at a height of around 1000 feet at 9:02:40 which means the flight descended over 8000 feet in 40 seconds. Would this not send the plane out of control...
In the first two minutes, the aircraft descended 6,500 feet. That works out to a descent rate of 3,250 feet per minute. In the second two minutes, the aircraft descended 9,500 feet. That works out to a descent rate of 4,750 feet per minute. The last 40 seconds saw a descent of 8,000 feet, which works out to 12,000 feet per minute.
For comparison purposes, on a Boeing 757, the normal descent rate from cruising altitude with the engines at idle power is about 1,800 feet per minute. It would be very easy to descend faster by simply adding engine power. At full throttle and with a nose down attitude, I have no doubt a jetliner could achieve the descent rates mentioned. It wouldn't be recommended by the manufacturer, of course, but it could be achieved.
I'm sure if someone wanted to they could dig up the reports on commercial flights incidents or accidents which saw similar large, rapid losses of altitude.
Cruising speed is not maximum attainable speed. Cruising speed just means the speed, for a given altitude, at which the jet flies the farthest distance for a given amount of fuel.This places speed between 668 Mph and 771 Mph Maximum cruising speed for Boeing 767 is 568 MPH and that is at cruising altitude.
What makes you think that?The plane would go much lower speeds at lower altitudes.
Which sources?these speeds are not attainable at the lower altitudes. And a plane going at these speeds would be out of control so badly hitting the tower would have been very hard to do.
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