What was found
LE SLAT NO 9 INTERNAL SKIN WITH CRACK REMOVED L/E SLAT NO 9 INTERNAL SKIN PANEL IAW B757 SRM 51-40-02-0G, FORMED TRIMMED, LOCATED, DRILLED AND INSTALLED NEW SKIN PANEL IAW B757 SRM 51-40-02-0G AND BOEING DWG # 114N4076 REV C.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LE SLAT NO 9 INTERNAL SKIN WITH CRACK REMOVED L/E SLAT NO 9 INTERNAL SKIN PANEL IAW B757 SRM 51-40-02-0G, FORMED TRIMMED, LOCATED, DRILLED AND INSTALLED NEW SKIN PANEL IAW B757 SRM 51-40-02-0G AND BOEING DWG # 114N4076 REV C.