What was found
DURING 2C CHECK TASK 232-01Z, THE FUSELAGE RT SKIN SUPPORT AT FRAME 13A, STRINGER 14R WAS FOUND CRACKED. THE PART WAS REPAIRED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 3653-2, REV IR, 11-7-00.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING 2C CHECK TASK 232-01Z, THE FUSELAGE RT SKIN SUPPORT AT FRAME 13A, STRINGER 14R WAS FOUND CRACKED. THE PART WAS REPAIRED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 3653-2, REV IR, 11-7-00.