What was found
UPON COMPLIANCE 2C INSPECTION TASK 231/232 - 01Z THE FRAME 13A SKIN SUPPORT WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 3653-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
UPON COMPLIANCE 2C INSPECTION TASK 231/232 - 01Z THE FRAME 13A SKIN SUPPORT WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 3653-2.