What was found
FUSELAGE EXTERIOR, AFTER REMOVAL OF LOWER STRESS PANELS, CTR SECTION KEEL BEAM HAS CORROSION, GAINED ACCESS. REMOVED KEEL BEAM SECTION. FABRICATED NEW KEEL BEAM SECTION & INSTALLED IAW EA 008-5302-38-A5957.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE EXTERIOR, AFTER REMOVAL OF LOWER STRESS PANELS, CTR SECTION KEEL BEAM HAS CORROSION, GAINED ACCESS. REMOVED KEEL BEAM SECTION. FABRICATED NEW KEEL BEAM SECTION & INSTALLED IAW EA 008-5302-38-A5957.