As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPON COMPLIANCE OF 2C INSPECTION TASK 231-01Z, WHILE GAINING ACCESS THE LT COCKPIT SKIN SUPPORT BRACKET BEHIND TO DV WINDOW FRAME WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.