What was found
DURING C-CHECK, INSPECTION FOUND VERTICAL STAB SPAR TO FRAME 75 FRETTING AT THE FUSELAGE. MAINTENANCE COMPLIED WITH THE EC 5310-01317 TO REMOVED FITTING, REMOVED CORROSION, CHECK LIMITS AND REINSTALL FITTING.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK, INSPECTION FOUND VERTICAL STAB SPAR TO FRAME 75 FRETTING AT THE FUSELAGE. MAINTENANCE COMPLIED WITH THE EC 5310-01317 TO REMOVED FITTING, REMOVED CORROSION, CHECK LIMITS AND REINSTALL FITTING.