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Originally posted by RearheatApparently you hit your head the last time you did it.
Originally posted by RearTreat
A pull up would not reduce longitudinal g until after airspeed bleed-off, Einstein. Since you like to quote data where is that in the data prior to the significant longitudinal G reduction? Oh, I see it's not there = EPIC FAIL.
Originally posted by Retreat
How much reduction would that require? Is it in the data? Witnesses testified the aircraft was at full power and based on the excessive and increasing airspeed there is no doubt it was. = EPIC FAIL.
Originally posted by Alfie1
However, the final postion is, I believe, some 200 plus feet north, on the cloverleaf, of where it should be for light poles and impact.
Is this sort of error just something to be accepted from the FDR or is it significant ?
Originally posted by turbofan
That's a good one; almost as funny as 24 knot winds moving aircraft debris,
and not a plume of smoke! :lol
Originally posted by turbofan
John, let's see some data for the smoke trail. Are you ready to suggest
what part of the aircraft system produced this white trail of smoke?
[edit on 18-11-2009 by turbofan]
Originally posted by Alfie1
Sorry to bother you again, but does the fact that the plane was on a heading of 61.5 degrees help ? Is that a product of FDR ?
Originally posted by Reheat
John, If you want to deal with this TF character about acceleration, press on. I don't have the time or patience to deal with his non-sequitur BS, ignorant insults, and lack of understanding of rather simple aeronautical issues.
Originally posted by turbofan
Do YOU understand that 'airspeed bleed-off' has nothing to do with accelerometer reading?
[edit on 18-11-2009 by turbofan]
Originally posted by turbofan
You should also look into the smoke trail origin if you're such the honest
researcher you say you are.
[edit on 18-11-2009 by turbofan]
Originally posted by 911files
Nah, it is all just going over his head.