TWA 800
Printed page 302. PDF page 320.
"Open--Acceptable Response." 2.5 Maintenance and 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 inOpen final report at PDF page 320NTSB AAR-00/03: In-flight breakup, TWA flight 800