What was found
INSPECTION FOUND THE FORWARD INTERMEDIATE FUSELAGE FRAME CAP CORRODED AT STA 899, LONGERON 51L AND 50R; STA 959, LONGERON S50L AND 50R; AND STA 1019, LONGERON 49L AND 51L. REPAIRS WERE PERFORMED IAW ECRA 5310-03264.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND THE FORWARD INTERMEDIATE FUSELAGE FRAME CAP CORRODED AT STA 899, LONGERON 51L AND 50R; STA 959, LONGERON S50L AND 50R; AND STA 1019, LONGERON 49L AND 51L. REPAIRS WERE PERFORMED IAW ECRA 5310-03264.