What was found
DURING INSPECTION, FOUND A CRACK INDICATION IN FUSELAGE SKIN AT BS 539, TWO INCHES BELOW STRINGER 18R. MAINTENANCE REPAIRED IAW 5331-01257-10.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION, FOUND A CRACK INDICATION IN FUSELAGE SKIN AT BS 539, TWO INCHES BELOW STRINGER 18R. MAINTENANCE REPAIRED IAW 5331-01257-10.