What was found
DURING SCHEDULED C-11 CHECK, FOUND FUSELAGE RT UPPER LONGERON HAD STRESS CORROSION AT FS 470 TO 476, RBL 60, WL 258 AT BAR FITTING ATTACHMENT. REPAIRED IAW SMP583, 51-60 AND 51-70.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED C-11 CHECK, FOUND FUSELAGE RT UPPER LONGERON HAD STRESS CORROSION AT FS 470 TO 476, RBL 60, WL 258 AT BAR FITTING ATTACHMENT. REPAIRED IAW SMP583, 51-60 AND 51-70.