What was found
CRACK ON STRINGER 8 UPPER SURFACE AND WS 479.00 FUEL TANK RT/WING L=1.5" APPROX (S-8R). PERFORMED REPAIR ON STRINGER 8 UPPER PANEL STRINGER LOCATED WS 479.00 IAW EA 1-357-7804 REV 0 AND EO AEM-HC57-297/12 RO.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON STRINGER 8 UPPER SURFACE AND WS 479.00 FUEL TANK RT/WING L=1.5" APPROX (S-8R). PERFORMED REPAIR ON STRINGER 8 UPPER PANEL STRINGER LOCATED WS 479.00 IAW EA 1-357-7804 REV 0 AND EO AEM-HC57-297/12 RO.