As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C2 PRESSURE PANEL AT STA 857 RBL 26 TO 46 REAR SPAR TO FUSELAGE ANGLE EXFOLIATED. REMOVED ANGLE CHORD AT STA 857 RBL 26 TO 46 IAW SRM 51-1-20D. LOCATED AND DRILLED RT UPPER AFT SPAR CHORD AND INSTALLED SPAR CHORD IAW SRM 51-1-20D AND SRM 53-2-05-0 FIG 16.