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Printed page 1. PDF page 19.
JFK for CDG about 1900; however, the flight was delayed because of a disabled piece of ground equipment4 and concerns about a suspected passenger/baggage mismatch. According to the cockpit voice recorder (CVR),5 at 1959:44, gate agent personnel advised the flightOpen final report at PDF page 19NTSB AAR-00/03: In-flight breakup, TWA flight 800
Printed page 301. PDF page 319.
research on ground-based inerting indicated that the costs associated with the needed ground equipment are significantly less than what was estimated by the FTHWG and, further, that analysis indicated that ground-based inerting would reduce the fleetwide average flammabiOpen final report at PDF page 319NTSB AAR-00/03: In-flight breakup, TWA flight 800
Printed page 55. PDF page 73.
1996, when a mechanic was scheduled to install the cables while the airplane was on the ground at JFK. However, the mechanic told Safety Board investigators that he was unable to complete the repair before the airplane's scheduled departure, soOpen final report at PDF page 73NTSB AAR-00/03: In-flight breakup, TWA flight 800
Printed page 159. PDF page 177.
radio frequency (RF) emitters317 in the TWA flight 800 environment were identified. Ground-based emitters with frequency assignments318 for the eastern United States (as identified in the JSC-maintained frequency assignment databases) comprised the fixed emitters. ThesOpen final report at PDF page 177NTSB AAR-00/03: In-flight breakup, TWA flight 800
Printed page 200. PDF page 218.
The FAA indicated that it had therefore initiated studies of directed ventilation and ground-based inerting methods and that, after equipment requirements for ground-based inerting had been determined, it intended to task the ARAC to perform a detailed study of inertingOpen final report at PDF page 218NTSB AAR-00/03: In-flight breakup, TWA flight 800
Printed page 322. PDF page 340.
receiver/transmitter portion of a radar system that responds to interrogation signals received from ground-based equipment. Ullage: The space in a fuel containing tank not occupied by liquid fuel. Upper flammability limit: The maximum temperature at which a concentration of fuelOpen final report at PDF page 340NTSB AAR-00/03: In-flight breakup, TWA flight 800