What was found
POST LANDING INSPECTION REVEALED AFT FUSELAGE PRESSURE PANEL CRACKED AT FS 1035, RBL 8.48 TO LBL 27.83, WL 275. REPLACED PANEL IAW SMP583 CH 51-10.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
POST LANDING INSPECTION REVEALED AFT FUSELAGE PRESSURE PANEL CRACKED AT FS 1035, RBL 8.48 TO LBL 27.83, WL 275. REPLACED PANEL IAW SMP583 CH 51-10.