What was found
FUSELAGE BS 933 STR 38R AT DRAG SPLICE FITTING AREA FOUND ONE FASTENER HOLE CRACKED AT FUSELAGE SKIN. REPAIRED IAW SRM 53-20-01-2R2 REPAIR 2, FIG 201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE BS 933 STR 38R AT DRAG SPLICE FITTING AREA FOUND ONE FASTENER HOLE CRACKED AT FUSELAGE SKIN. REPAIRED IAW SRM 53-20-01-2R2 REPAIR 2, FIG 201.