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Printed page 302. PDF page 320.
Aging Issues As previously discussed, no evidence was found that preexisting airplane fatigue or corrosion contributed to the accident.657 Although small fatigue cracks were found in the lower chord of the front spar and in shear ties for the floorOpen final report at PDF page 320NTSB AAR-00/03: In-flight breakup, TWA flight 800
Printed page 116. PDF page 134.
portions of the STA 520 joint that separated were examined for evidence of preexisting fatigue or other preexisting damage. The Safety Board's examination of this joint revealed that all fractures were typical of overstress separations, with no evidence of fatigue,Open final report at PDF page 134NTSB AAR-00/03: In-flight breakup, TWA flight 800
Printed page 257. PDF page 275.
the wreckage revealed no evidence of preexisting airplane structural faults (such as fatigue, corrosion, or mechanical damage) that could have contributed to the in-flight breakup. The examination revealed that the structure did have minimal preexisting corrosion damageOpen final report at PDF page 275NTSB AAR-00/03: In-flight breakup, TWA flight 800