What was found
LEVEL 2 CORROSION, RIGHT WING UPPER SKIN AT XW 0.000 CENTER SPAR AREA SKIN HAS SURFACE CORROSION AT FUSELAGE STA 781.500. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER RICH DRAWING 95-10-06-OO1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEVEL 2 CORROSION, RIGHT WING UPPER SKIN AT XW 0.000 CENTER SPAR AREA SKIN HAS SURFACE CORROSION AT FUSELAGE STA 781.500. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER RICH DRAWING 95-10-06-OO1.