What was found
LEFT UPPER AFT FUSELAGE SKIN WAS CRACKED AT FRAME 75, ABOVE STRINGER 2L. REPAIRED THE SKIN IAW SRM 53-31-01 ITEM 11 FIG 219
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT UPPER AFT FUSELAGE SKIN WAS CRACKED AT FRAME 75, ABOVE STRINGER 2L. REPAIRED THE SKIN IAW SRM 53-31-01 ITEM 11 FIG 219