What was found
LE SLAT NO 8 INTERNAL SKIN WITH CRACK REMOVED SKIN PANEL L/E SLAT NO 8 IAW B757 SRM 51-40-02-0G FORMED, TRIMMED, LOCATED DRILLED AND INSTALL NEW SKIN PANEL IAW BOEING DWG # 114N4077 REV D AND B757 SRM 51-40- 02-0G.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LE SLAT NO 8 INTERNAL SKIN WITH CRACK REMOVED SKIN PANEL L/E SLAT NO 8 IAW B757 SRM 51-40-02-0G FORMED, TRIMMED, LOCATED DRILLED AND INSTALL NEW SKIN PANEL IAW BOEING DWG # 114N4077 REV D AND B757 SRM 51-40- 02-0G.