Thanks. That is a significant difference.
But the F-14A thrust you mention must have been a later engine mod. My 1984 NATOPS lists it as 17,077 pounds in AB.
I recall some losses with engine loss on TO back then, even with the lower thrust. This caused a lot of concern and scrambling for new procedures.
My old NATOPS says the following unusual comment:
That is pretty amazing since the aircraft had by then been operational for almost a decade. I do remember later they established new and radical procedures after that testing.
I stand corrected. And I also should have said, "highly unlikely" rather than "impossible" to spin. And it was...... unless you lost an engine and ended up, "coupled."pretty sure the first flat spin loss was around '75 at pax river. the whole event was filmed. the aircraft appeared to recover after the crew jumped out (c g change).
that particular jet was to have been the first f14 the marines were scheduled to reveive.
http://www.globalsecurity.org/military/systems/aircraft/f-14-test.htm
This link may have it: F-14 Ejection Historyanybody know when the last f14 loss to a flat spin took place?
.....
f14 spin video. this scares me and i'm fearless.
http://www.liveleak.com/view?i=78b_1172623495
off topic... new wheels
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f14 spin video. this scares me and i'm fearless.
http://www.liveleak.com/view?i=78b_1172623495
off topic... new wheels
![]()