Search report text, read a short matching passage, then open the source page.
Exact phrases match first; otherwise all words must occur close together. Six excerpts maximum. Text extraction cannot search image-only charts. Warsaw uses a report transcription with missing figures and appendices.
6 matching PDF pages. Showing 6 short source excerpts. Open the document for full context.
Printed page 2. PDF page 20.
assigned altitude. At 2029:15, the CVR recorded the captain stating, "Look at that crazy fuel flow indicator there on number four...see that?"7 At 2030:15, Boston ARTCC advised, "TWA 800 climb and maintain [15,000 feet msl]." The CVR recorded the captainOpen final report at PDF page 20NTSB AAR-00/03: In-flight breakup, TWA flight 800
Printed page 34. PDF page 52.
from other systems (such as lights) that were bundled with both the CVR and the No. 4 fuel flow indicator wires for a portion of their paths. Further, the wiring diagrams show that the right wing FQIS wires were routedOpen final report at PDF page 52NTSB AAR-00/03: In-flight breakup, TWA flight 800
Printed page 42. PDF page 60.
computer located adjacent to the VSO computer in the electrical/electronics (E/E) bay, a fuel flow indicator located near the fuel quantity indicators at the flight engineer station, and a repeater indicator located in the cockpit near the center of theOpen final report at PDF page 60NTSB AAR-00/03: In-flight breakup, TWA flight 800
Printed page 71. PDF page 89.
valve switch was found in the "Off" (closed) position.141 The Nos. 1, 2, and 3 engine fuel flow indicators showed zero fuel flow, whereas the No. 4 engine fuel flow indicator showed 900 pounds per hour. The Safety Board examinedOpen final report at PDF page 89NTSB AAR-00/03: In-flight breakup, TWA flight 800
Printed page 79. PDF page 97.
flight engineer station included the CWT fuel panel (including the quantity gauge and fuel flow indicators), the FQIS wiring connector at the flight engineer station, the resistor installed between the FQIS wire and the attached AIDS wiring,150 and most circuitOpen final report at PDF page 97NTSB AAR-00/03: In-flight breakup, TWA flight 800
Printed page 289. PDF page 307.
could also explain the electrical anomalies indicated on the CVR recording and the No. 4 fuel flow indicator. Although no evidence of arcing was found in any of the components connected to the CWT FQIS (the fuel quantity indicator, totalizerOpen final report at PDF page 307NTSB AAR-00/03: In-flight breakup, TWA flight 800