What was found
CRACK IN FUSELAGE SKIN AT BS 937, STRINGER 24R. 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 937, STRINGER 24R. REPAIRED IAW SRM 53-30-3, FIG 48, DETAIL XIX, SHEET 46.