What was found
CRACK IN FUSELAGE SKIN AT BS 920, STRINGER 25R ABOVE LAP SEAM. REPAIRED IAW SRM 53-30-3, FIG 48, DETAIL XIX, SHEET 46.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK IN FUSELAGE SKIN AT BS 920, STRINGER 25R ABOVE LAP SEAM. REPAIRED IAW SRM 53-30-3, FIG 48, DETAIL XIX, SHEET 46.