As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
#8 SLAT WEDGE IS DELAMINATED ON O/B END.<[01] #8 SLAT O/B END SEAL REMOVED AND REPLACED. IAW AIPC 27-81-21 & SOPM 20-50-01;[02] VERIFIED CA #1 #8 SLAT O/B END SEAL REMOVED AND REPLACED. IAW AIPC 27-81-21 & SOPM 20-50-01;[03] ADDED TORQUE WRENCH;[04] PARTS ADDED