What was found
AT C-CHECK, CORROSIN BLEEDING FROM RT WING SPAR TO BODY FITTING. REMOVED CORROSION, BLENDED OUT FACE OF FITTING. FLAP PEENED FITTING, INSTALLED BUSHING AND INSTALLED BOTTLE PIN PER AVITAS EO PMSI191R0-3. N/R 7815.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C-CHECK, CORROSIN BLEEDING FROM RT WING SPAR TO BODY FITTING. REMOVED CORROSION, BLENDED OUT FACE OF FITTING. FLAP PEENED FITTING, INSTALLED BUSHING AND INSTALLED BOTTLE PIN PER AVITAS EO PMSI191R0-3. N/R 7815.