What was found
FUSELAGE SKIN CRACKED 4.5 INCHES AT BS 884, S25R. CUT OUT DAMAGE. INSTALLED REPAIR IAW SRM REV. 101, 53-00-01, REPAIR 31, FIG. 201, DETAIL XIX. CAT A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN CRACKED 4.5 INCHES AT BS 884, S25R. CUT OUT DAMAGE. INSTALLED REPAIR IAW SRM REV. 101, 53-00-01, REPAIR 31, FIG. 201, DETAIL XIX. CAT A.