As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING D-CHECK, FRAME UPPER FLANGE CRACKED TWO PLACES BS 560 BETWEEN STRINGER 29L TO OUTBOARD OF 29R. STOP DRILLED CRACKS AS PER SRM 51-10-1. REMOVED DAMAGED AREA AS PER SRM 53-10-4. FABRICATED FILLER 7075-T6 1 INCH BY 3 INCH BY 30 INCHES AS PER SRM 53-10-4. TREATED AND PRIMED PER SRM 51-10-2 AND INSTALLED AS PER SRM 51-30-2. TOTAL CYCLES 29,235.