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Originally posted by TiffanyInLA
With that said, when you use correct math based on the distance/sweeps of each radar point, you'll get the same as the NTSB reports, 430 knots for the North tower aircraft and 510 knots for the south tower aircraft.
Originally posted by TiffanyInLA
(Interviewer asks -) "So there's no way the aircraft could be going 500 mph at [700 ft] altitude then?"
Boeing Spokesperson - (Laughs) "Not a chance..."
(Interviewer asks -) "So there's no way the aircraft could be going 500 mph at [700 ft] altitude then?"
Boeing Spokesperson - (Laughs) "why yes it easily can..."
Originally posted by Xtrozero
Originally posted by TiffanyInLA
(Interviewer asks -) "So there's no way the aircraft could be going 500 mph at [700 ft] altitude then?"
Boeing Spokesperson - (Laughs) "Not a chance..."
Actually it was...
(Interviewer asks -) "So there's no way the aircraft could be going 500 mph at [700 ft] altitude then?"
Boeing Spokesperson - (Laughs) "why yes it easily can..."
What these two statements do not have is neither say Official Boeing spokesperson, exec etc followed by a full name, as my prior posts did.
1). Posting: You will not post any material that is knowingly false, misleading, or inaccurate.
Originally posted by Xtrozero
Originally posted by TiffanyInLA
With that said, when you use correct math based on the distance/sweeps of each radar point, you'll get the same as the NTSB reports, 430 knots for the North tower aircraft and 510 knots for the south tower aircraft.
So are these two speeds the ones you are officially endorsing?
Originally posted by hooper
"I believe the.....
or
"I believe that.....
Originally posted by TiffanyInLA
Originally posted by Xtrozero
Originally posted by TiffanyInLA
Please let us know when you will find one verified pilot who will endorse your claims that it is "easy" to control an aircraft at Vmo+150, Va+220, while pulling G's leveling from a 10,000 ft dive in less than a minute, while cranking in 38 degrees of bank to hit a target with less than a 25' margin for error.
edit on 10-9-2010 by TiffanyInLA because: typo - clarity
One correction and one addition. Va is irrelevant. It is simply the maximum speed at which full elevator input can be applied without stuff breaking or bending and not springing back. Slower than Va and the wing stalls, releasing the g-loading. Faster than Va, something's going to give with full elevator input.
One thing that has not been addressed by those who think it's a piece of cake to fly something at Vmo+150 while pulling gs is the rolling g load. Your V-g diagram is for non rolling symetrical loading. Introducing a rolling moment into the equation reduced maximum allowable g-loading to about 2/3 of the certified design load limit. It varies for every airframe type ad I remember the F-4 Phantom II Flight Manual had several pages on it depending on weight, ordinance configuration, whether they had the mickey mouse jury-rigged machine gun pod on it, the model (B, D or E), etc. Some other good information on the effect of rolling on gs is in the Bellanca 8KCAB flight manual and the one for each of the Avions Mudry CAP aircraft (10, 20 230, 231, 232.)
Originally posted by TiffanyInLA
.
Your source says it is "way off the charts".
You falsely misrepresented both of them and intentionally changed their words in order to not disrupt your blind support of the OS.
Originally posted by TiffanyInLA
Those are the two speeds officially endorsed by the NTSB based on their analysis.
Do you claim they are wrong?
Originally posted by Xtrozero
But then these are quick picks off the net, Boeing has about 30,000 engineers and pilots working for them and there is no 911 rumblings anywhere in the company, sorry.
I was demonstrating that anything can be written as you did and as I did.
I’ll send her an email since we work for the same company.. ;P
Originally posted by Xtrozero
Once again, do you see those speeds as correct or as closely correct as we most likely can determined? Can we get a yes or no?
Originally posted by TiffanyInLA
I see those speeds as thoroughly analyzed by the NTSB, a govt agency tasked to ensure the safety of the traveling public, using RADES and ASR radar. It cross-checks with the radar data (when you apply the correct math) being provided through the FOIA by the 84th Radar Evaluation Squadron in located at Hill AFB in Utah.
Originally posted by Xtrozero
So do I take that as a YES you agree with their findings?
I never suggested any speed other to say a "high rate" high enough to do what they did.
Originally posted by TiffanyInLA
Scroll forward to 2:57
Originally posted by TiffanyInLA
Considering you have expressed that MIT, NIST and FEMA might be more accurate because their analysis shows a lower speed, you may want to get them to guide your next approach, that is if you really fly aircraft.
Originally posted by Xtrozero
Originally posted by TiffanyInLA
Scroll forward to 2:57
Lol, thank you so much for providing this video. I posted it again for all to watch since it would be hard for me to find something better so show how crackpot so many of you guys are...
The engineer on the video said the "plane would shake itself apart at 220 MPH at that altitude"
Do you agree with his statement that the plane would do that?
And the lady on the phone…lol good god! hehe
Her first words were ‘oh boy..hehe” AND her final “official statement” for Boeing… “well ya whatever that other guy said” Geez, if this is your damning proof…I just do not know what to say, or how you can even back it up..I do give you some credit, but hell how can I now after watching this that you have pushed and endorsed a number of times…
You actually made me choke on my beer in laughter as I watched it…next time warn me will ya…
Once again, LOL you got me on that one…
Originally posted by zerbot565
how do they measure the speed ?
is it some sort of theoretical equation based on flight alt and engien output that gives you the correct flight speed ?
Originally posted by Xtrozero
I expressed many times that it is hard to put a true number to their speeds....
so now what do YOU think...so are those the speeds you endorse? Come on, are you going to ever actually put your own opinion on anything, or just cut and paste others over and over.