What was found
LEFT LOWER CTR WING SKIN, UPPER SURFACE HAS NUMEROUS GOUGES FROM FASTENER. REMOVAL OF THE SPLICE ANGLE, BETWEEN XCW=95 & XCW=99, BETWEEN THE FRONT SPAR & STRINGER 49. REPAIRED IAW EA 8-5710-T0324689.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT LOWER CTR WING SKIN, UPPER SURFACE HAS NUMEROUS GOUGES FROM FASTENER. REMOVAL OF THE SPLICE ANGLE, BETWEEN XCW=95 & XCW=99, BETWEEN THE FRONT SPAR & STRINGER 49. REPAIRED IAW EA 8-5710-T0324689.