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123 matching PDF pages. Showing 6 short source excerpts. Open the document for full context.
Printed page Unnumbered PDF sheet. PDF page 5.
Information--General and Specific to Accident Airplane . . . . . 22 1.6.1.3.3 Separation of 747 Wire Circuits . . . . . . . . . . . . . . . . . . . . . .Open final report at PDF page 5NTSB AAR-00/03: In-flight breakup, TWA flight 800
Printed page Unnumbered PDF sheet. PDF page 10.
center wing fuel tank . . . . . . . . . . . . . . . 21 10. Diagram of a BMS13-42A Poly-X wire . . . . . . . . . . . . .Open final report at PDF page 10NTSB AAR-00/03: In-flight breakup, TWA flight 800
Printed page Unnumbered PDF sheet. PDF page 11.
fuel pump conduit wear rate that was identified by the FAA during representative 500 wire inspections . . . . . . . . . . . . . . . . . . . . . . . .Open final report at PDF page 11NTSB AAR-00/03: In-flight breakup, TWA flight 800
Printed page Unnumbered PDF sheet. PDF page 17.
Commission on Aviation Safety and Security WL body waterline WS wing station WSSIWG Wire System Safety Interagency Working Group XL-ETFE cross-linked ethylenetetrafluoroethyleneOpen final report at PDF page 17NTSB AAR-00/03: In-flight breakup, TWA flight 800
Printed page 16. PDF page 34.
modified to carry fuel. 32 An electrical conduit is a rigid tube that contains electrical wires. 33 According to postaccident interviews with TWA ground operations personnel, while the accident airplane was on the ground at JFK, two of the threeOpen final report at PDF page 34NTSB AAR-00/03: In-flight breakup, TWA flight 800
Printed page 21. PDF page 39.
which a number of terminals are installed; however, it can also consist of a section of wire from which power is distributed to other wires/circuits.Open final report at PDF page 39NTSB AAR-00/03: In-flight breakup, TWA flight 800