What was found
FUSELAGE SKIN IS CORRODED AT BS 559.112 CIRCUMFERENTIAL JOINT BETWEEN STRINGERS 27 AND 26R. REPAIRED CORRODED FUSELAGE SKIN IAW REO 601R-53-51-745 REV --.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN IS CORRODED AT BS 559.112 CIRCUMFERENTIAL JOINT BETWEEN STRINGERS 27 AND 26R. REPAIRED CORRODED FUSELAGE SKIN IAW REO 601R-53-51-745 REV --.