What was found
DURING C-CHECK INSPECTION, FOUND FITTING ON LEFT FUSELAGE SKIN THAT TIES INTO THE MAIN FRAME AND INTO LEFT TRAPEZOID PANEL HAD CORROSION IN THE BOLT HOLE. REPAIRED IAW ABX REA D953-12649-MR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK INSPECTION, FOUND FITTING ON LEFT FUSELAGE SKIN THAT TIES INTO THE MAIN FRAME AND INTO LEFT TRAPEZOID PANEL HAD CORROSION IN THE BOLT HOLE. REPAIRED IAW ABX REA D953-12649-MR.