As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MULTIPLES CRACKS ON PANEL 211A (MARKED)<[01] UPON INVESTIGATION FOUND COCKPIT PANEL 211A IS ACTUALLY 212B. FOUND ONE CRACK ON PANEL 212B; REPAIRED PANEL 212B PER CMM 25-00-66 REPAIR 3-1 PARAGRAPH 4 APPLIED FIBERGLASS AT 10:30 AM;[02] VERIFIED 24HR CURE OF FIBERGLASS REPAIR TO PANEL 212B IAW CMM 25-00-66 REPAIR 3-1 PARAGRAPH 4 AND REPLACED RIVET IN REPAIRED AREA IAW SRM 51-40-02-0G-0;[03] VERIFIED ITEMS 1 AND2