What was found
DURING ROUTINE INSP, FUSELAGE SKIN FOUND CRACKED AT LAP JOINT, STR 20L, BS 1185. *S/D* FAB FILLER, DOUBLER AND INSTALLED IAW SRM 53-30-3 FIG 3A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ROUTINE INSP, FUSELAGE SKIN FOUND CRACKED AT LAP JOINT, STR 20L, BS 1185. *S/D* FAB FILLER, DOUBLER AND INSTALLED IAW SRM 53-30-3 FIG 3A.