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Printed page 111. PDF page 129.
the WCS, and a limited amount of fuselage structure above the right wing and that the most likely source of fuel for this fire was the right wing inboard fuel tank. Many of the fractures from the portion of theOpen final report at PDF page 129NTSB AAR-00/03: In-flight breakup, TWA flight 800
Printed page 290. PDF page 308.
circuit producing excess voltage that was transferred to the CWT FQIS wiring is the most likely source of ignition energy for the TWA flight 800 CWT explosion. 2.3.2.2 Release of Ignition Energy Inside the Center Wing Fuel Tank 2.3.2.2.1 ArcingOpen final report at PDF page 308NTSB AAR-00/03: In-flight breakup, TWA flight 800
Printed page 307. PDF page 325.
transferred to the center wing tank (CWT) fuel quantity indication system wiring is the most likely source of ignition energy for the TWA flight 800 CWT explosion. 17. Silver-sulfide deposits on fuel quantity indication system components inside fuel tanks poseOpen final report at PDF page 325NTSB AAR-00/03: In-flight breakup, TWA flight 800
Printed page xvi. PDF page 18.
be determined with certainty, but, of the sources evaluated by the investigation, the most likely was a short circuit outside of the CWT that allowed excessive voltage to enter it through electrical wiring associated with the fuel quantity indication system.Open final report at PDF page 18NTSB AAR-00/03: In-flight breakup, TWA flight 800
Printed page 308. PDF page 326.
be determined with certainty, but, of the sources evaluated by the investigation, the most likely was a short circuit outside of the CWT that allowed excessive voltage to enter it through electrical wiring associated with the fuel quantity indication system.Open final report at PDF page 326NTSB AAR-00/03: In-flight breakup, TWA flight 800