What was found
A BULGE IN THE EXTERIOR FUSELAGE SKIN WAS IDENTIFIED AT FRAME 20 & STRINGER 36R. REMOVED CORROSION FROM FUSELAGE SKIN & REPAIRED IAW EA 253023 & 253028.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
A BULGE IN THE EXTERIOR FUSELAGE SKIN WAS IDENTIFIED AT FRAME 20 & STRINGER 36R. REMOVED CORROSION FROM FUSELAGE SKIN & REPAIRED IAW EA 253023 & 253028.