What was found
FUSELAGE RT INNER CHORD FITTING CORRODED AT STA 1002 TO STA 1006. R&R FITTING PER SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE RT INNER CHORD FITTING CORRODED AT STA 1002 TO STA 1006. R&R FITTING PER SRM.