File:TWA 800 lower portion of the fuselage skin.jpg

TWA_800_lower_portion_of_the_fuselage_skin.jpg(412 × 512 pixels, file size: 90 KB, MIME type: image/jpeg)

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English: Figure 30. A schematic drawing of the lower portion of the fuselage skin in the area.
  • The detailed examinations of the fuselage red zone pieces are an example of how these examinations were successful in determining an important segment of the breakup sequence. Figure 30 shows a schematic drawing of the lower portion of the fuselage skin in the area forward of the front spar. In this figure, the earlier fuselage skin fractures have been highlighted, and arrows have been added to indicate the direction of cracking in these earlier fractures. Of all of the fuselage fractures examined, only a limited number (all of which were on pieces recovered from the red zone) could be classified as earlier fractures (that is, consistent with in-plane loading). Further detailed examination of the rivet-torivet fracture pattern in these earlier fuselage fractures generated information on crack propagation directions and indicated that the earliest fracturing was of the lower fuselage, beginning at the front spar of the WCS (wing center section).
Date
Source NTSB Accident Report, Trans World Airlines Flight 800, AAR0003.pdf, Page 105
Author NTSB

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Public domain
This image is a work of a National Transportation Safety Board employee, taken or made as part of an employee's official duties. As a work of the U.S. federal government, all NTSB images are in the public domain in the United States.

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current01:33, 12 March 2020Thumbnail for version as of 01:33, 12 March 2020412 × 512 (90 KB)Ras67 (talk | contribs)== {{int:filedesc}} == {{Information |description={{en|1=''Figure 39.'' A schematic drawing of the lower portion of the fuselage skin in the area. * The detailed examinations of the fuselage red zone pieces are an example of how these examinations were successful in determining an important segment of the breakup sequence. '''Figure 30''' shows a schematic drawing of the lower portion of the fuselage skin in the area forward of the front spar. In this figure, the earlier fuselage skin fractur...

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