What was found
DURING SCHEDULED C-11 CHECK, FOUND AFT FUSELAGE INTERIOR BULKHEAD-TO-SLOPING LONGERON FITTING HAD CRACKED AT FS 902 WL 200 LBL 63, REPAIRED IAW SMP581-52-30, FIG. 52-30-06, PG. 242.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED C-11 CHECK, FOUND AFT FUSELAGE INTERIOR BULKHEAD-TO-SLOPING LONGERON FITTING HAD CRACKED AT FS 902 WL 200 LBL 63, REPAIRED IAW SMP581-52-30, FIG. 52-30-06, PG. 242.