What was found
RIGHT ENGINE AFT STRUT #1 FRAME SUPPORT OUTBOARD 2 HOLES COMMON TO STIFFENER SUPPORT ARE ELONGATED TO .387 / RIGHT ENGINE AFT STRUT #1 FRAME SUPPORT OUTBOARD 2 HOLES COMMON TO STIFFENER SUPPORT ARE ELONGATED TO .387. COMPLIED WITH TIME LIMITED REPAIR PER EA 1-754-2491. REPETITIVE INSPECTION EVERY 30 DAYS TO REMOVE PANEL 444AR FOR ACCESS AND PERFORM VISUAL INSPECTION FOR GENERAL SECURITY AND DAMAGE AT THE OUTBOARD INTERSECTION OF AFT FAIRING FRAME 1 AND FRAME 1 CROSS STIFFENER. REINSTALL PANEL 444AR AND RESTORE AIRPLANE TO NORMAL. PERMANENT REPAIR WITHIN 758 DAYS TO REPLACE AFT FARING FRAME 1 P/N 313A2710-1 REFERENCE DRAWING 313A2700-10#A