What was found
UPPER RT SIDE OF FUSELAGE SKIN IS CRACKED AT APPROXIMATELY BS 1654, STRINGER 3 - 5R. DAMAGED AREA WAS R & R IAW SRM 53-80-01 FIG 201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
UPPER RT SIDE OF FUSELAGE SKIN IS CRACKED AT APPROXIMATELY BS 1654, STRINGER 3 - 5R. DAMAGED AREA WAS R & R IAW SRM 53-80-01 FIG 201.