As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ULTRASONIC INSPECTION INDICATED A CRACK IN THE LOWER FILLET RADIUS OF THE LATERAL PANEL STRINGER 36 JUST FORWARD OF FRAME 54 BETWEEN THE 4TH AND 5TH FASTENER HOLES, CRACK LENGTH ESTIMATED AT 1 INCH. REPAIRED AREA AT FRAME 54 STRINGER 36R IAW EA NR 6-5330-112997 "FUSELAGE -AD 98-26-01 SKIN PANEL AT FRAME 54 AND STRINGER 36R REPAIR".