What was found
FUSELAGE SKIN CRACKED AT BS 540, STRINGER 22R. CHORD FWD FASTENER ROW, FIRST FASTENER BELOW STRINGER 22R. REPAIRED SKIN IAW EA.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN CRACKED AT BS 540, STRINGER 22R. CHORD FWD FASTENER ROW, FIRST FASTENER BELOW STRINGER 22R. REPAIRED SKIN IAW EA.