What was found
DURING 2C CHECK TASK 5310-221-05I, THE LT FUSELAGE SKIN SUPPORT AT FRAME 9, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 660-1, REV IR, 2-16-93.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING 2C CHECK TASK 5310-221-05I, THE LT FUSELAGE SKIN SUPPORT AT FRAME 9, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 660-1, REV IR, 2-16-93.