What was found
UPON COMPLIANCE OF 2C INSPECTION TASK 5310-022-05I, THE FUSELAGE FRAME 9 SKIN SUPPORT JUST BELOW F/O''S DV WINDOW WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 660-1, REV IR, 2-16-93.