What was found
RIGHT WING, UPPER SURFACE, AFTER REAR SPAR AREA, CLOSE TO RIB 18, SKIN PANEL HAS A CRACK. ACCOMPLISHED REPAIR IAW SRM 57-51-12-2 PAR. 4.G.3.(S) AND (T).
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT WING, UPPER SURFACE, AFTER REAR SPAR AREA, CLOSE TO RIB 18, SKIN PANEL HAS A CRACK. ACCOMPLISHED REPAIR IAW SRM 57-51-12-2 PAR. 4.G.3.(S) AND (T).