Likewise.
white streak at 09:16:06
5 seconds after FDR stopped
Not 09:16:08
FDR stopped at 3 seconds AFTER tail seperation with NEW noises of loud bangs and roaring noises due to engine speration. lateral accel pinned.
Page 133 of the PDF, NTSB states: "FDR and CVR data showed that engine
separation occurred during the out-of-control airplane motion that followed
the separation of the vertical stabilizer."
That's exactly what I said. The FDR stopped after tail separation, which does not affect the FDR -- we know this to be true because it records screwy results from the rudder servo, and logs the horizontal acceleration. The FDR also stops before engine separation. There are no other signs of gross breakup, since there is but a single, confined debris field, apart from engines and stabilizer.
So, once again, the stab failure didn't stop the FDR. The engine separation didn't stop the FDR. Gross structural failure didn't stop the FDR. What did?
I wish I could agree with you, but the NTSB reconstruction and videos
tell otherwise:
http://www.ntsb.gov/Events/2001/AA587/board_mtg_anim.htm
This animation is not sufficiently accurate for this purpose, as you well know, having been told literally hundreds of times.
The FDR data, which is what this thread is about, is consistent with pole impacts. As long as we understand the last few seconds are missing, for which there are a number of possible explanations, and precedent. That's what this thread is about. Stop trying to derail. Stick to the subject or concede the point.
You may want to retract that statement after re-reading the study and
watching the video reconstruction of the flight including text highlights of
the events. You may want to read the Flight Path Study, specifically Time
Correlation done by the NTSB
I've read it, seen it, and I've already explained to you that it isn't accurate enough for you to make your claims. The NTSB was off by nearly ten seconds in the AA 11 and UA 175 impacts. The most accurate data we have is from the FDR itself. That is the focus of discussion.
Please re-read the study and watch the flight study. It's all there.
God of the gaps fallacy noted, and ignored.
No, it is NOT. It is the time the sensor creates the signal, converts it and
transmits to DFDAU in ARINC 429 format. IE: Sensor to input side of DFDAU.
Here is MY conversation with Rockwell in it's entirety:
Ah, now that I know what you're talking about, this is something yet again. I was referring to the earlier e-mail that actually involved the DFDAU. This one does not. This is the time between radar signal reception and measurement. Another result that has absolutely nothing to do with latency to the FDR. Rockwell has no way of knowing how AA is going to packetize the result, how it's queued, whether it gets averaged or combined with other measurements in the flight computer, who applies a timestamp and when, and so on. This is totally meaningless for this discussion.
We are debating those points with MacGyver now to credit, or discredit them
You are in no position to credit or discredit refereed journal articles. If you even understand how a debate works, you must accept them as valid until proving they are false. And that, just to save you some time, will never happen.