What was found
DURING HFEC INSPECTION OF FUSELAGE FRAME 1640 LEFT HAD A CRACK INDICATION AT THE INNER CHORD FORWARD BEND RADIUS BETWEEN THE TWO FASTENERS BELOW THE EDGE OF THE INTERCOSTAL STRAP AT STRINGER 14L.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING HFEC INSPECTION OF FUSELAGE FRAME 1640 LEFT HAD A CRACK INDICATION AT THE INNER CHORD FORWARD BEND RADIUS BETWEEN THE TWO FASTENERS BELOW THE EDGE OF THE INTERCOSTAL STRAP AT STRINGER 14L.