What was found
FWD PIT FUSELAGE CIRCUMFERENTIAL FRAME UPPER CHORD CRACKED AT BS 840 ABOVE STR 40L.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FWD PIT FUSELAGE CIRCUMFERENTIAL FRAME UPPER CHORD CRACKED AT BS 840 ABOVE STR 40L.