What was found
UPON COMPLIANCE OF 2C INSPECTION TASK 5310-121-01I, THE LEFT FLOOR PROP AT FUSELAGE FRAME 13 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT #3647-1, IR, 5/3/00.