What was found
DURING SCHEDULED B1 INSPECTION, FOUND INTERIOR FUSELAGE BULKHEAD FLANGE CRACKED AT FS 847, WL 200, LBL 72. REPAIR ACCOMPLISHED IAW SMP583, FIG 51-140-19.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED B1 INSPECTION, FOUND INTERIOR FUSELAGE BULKHEAD FLANGE CRACKED AT FS 847, WL 200, LBL 72. REPAIR ACCOMPLISHED IAW SMP583, FIG 51-140-19.