write:Figure 17. Load on the Flight 587 Right Rear Main Attachment Lug and a Depiction of the Cleavage-Tension Failure ModeThe structural analyses also indicated that after the right re

which were missing from the lug when it was found in the wreckage. Figure 17. Load on the Flight 587 Right Rear Main Attachment Lug and a Depiction of the Cleavage-Tension Failure ModeThe structural analyses also indicated that
after the right rear main attachment lugfractured
all of the remaining lugs fractured sequentially. The fracture of the right rearmain attachment lug initiated a nearly instantaneous separation of the vertical stabilizerfrom the aft fuselage.Load21Load12

 

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