ktesibios
Worthless Aging Hippie
- Joined
- Feb 23, 2002
- Messages
- 1,493
Funny- last night I happened to catch a little bit of the History Channel's Modern Marvels program "Enginerring Disasters 20", about the crash of American Airlines flight 587 in Queens on November 12, 2001. Curiosity tweaked, I looked around online for more information, which led to the NTSB accident report at http://www.ntsb.gov/publictn/2004/AAR0404.pdf .
This contains some interesting information about flight 587's FDR. From page 48:
Footnotes 18 & 20 on page 5 are also of interest (bolding mine):
and on page 55:
But-but- that's impossible! An FDR can't fail to record everything right up to the instant of impact- it's CERTIFIED! And all the data has to be recorded within half a second of its measurement!
COVER-UP! TAMPERING!
WAKE UP BUSH LOYALIST SHEEPLE!
Right, turbofan?
This contains some interesting information about flight 587's FDR. From page 48:
1.11.2 Flight Data Recorder
The accident airplane was equipped with a Fairchild model FA2100 FDR, [NOTE:the same type used in flight 77]
S/N 1186, that was manufactured by L-3 Communications. The FDR used solid-state flash memory, stored in a crash-survivable memory unit, as the recording medium. The FDR was sent to the Safety Board’s laboratory for readout and evaluation.
The FDR showed extensive fire and impact damage. The memory module inside the memory unit did not show any damage, but the memory cable needed to be replaced before the data could be read out.
The FDR contained more than 81 hours of recorded data, and American Airlines provided conversion formulas for the data.84 The FDR recorded about 1 minute 33 seconds of flight data for the accident airplane, beginning at 0914:28.45 (the time that the right main landing gear squat switch changed from ground to air) and ending at 0916:01.23 (before airplane impact).
Footnotes 18 & 20 on page 5 are also of interest (bolding mine):
18 After 0915:58.5, the rudder pedals moved briefly to 0.7 inch right and then to 3.9 inches right, where they remained for the remainder of the FDR recording. (The FDR stopped recording 13.6 seconds before impact.)
20 The rudder angle data detected by the rudder position sensor at the vertical stabilizer were filtered before they were recorded on the FDR. As a result, the rudder angles during the second set of load factor
excursions had to be reconstructed using the recorded FDR data, the characteristics of the filter (as determined from a test performed during this investigation), and constraints imposed by the rudder control system and the recorded motion of the airplane. See section 1.11.2 for information about the data filter and section 1.16.2 for information about the reconstruction of rudder angles.
and on page 55:
However, because of uncertainties in the FDR
data—including data latencies (that is, delays), data filtering, and sampling rate effects— the rudder and sideslip angles at the time that the vertical stabilizer separated from the airplane were determined within a narrow range[/b]—10° to 11° for the rudder angle and 10° to 12.5° for the sideslip angle
But-but- that's impossible! An FDR can't fail to record everything right up to the instant of impact- it's CERTIFIED! And all the data has to be recorded within half a second of its measurement!
COVER-UP! TAMPERING!
WAKE UP BUSH LOYALIST SHEEPLE!
Right, turbofan?





