What was found
DURING RE-INSTALLATION OF LEADING EDGE SLAT COVE PANEL 623DB FOUND CRACKED AT LOWER I/B FASTENER HOLE / REPLACED R/H L/E SLAT #6 COVE PANEL 623DB IAW BOEING DWG 114A5030 REV B P/N 114A8131-8
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING RE-INSTALLATION OF LEADING EDGE SLAT COVE PANEL 623DB FOUND CRACKED AT LOWER I/B FASTENER HOLE / REPLACED R/H L/E SLAT #6 COVE PANEL 623DB IAW BOEING DWG 114A5030 REV B P/N 114A8131-8