What was found
FOUND EVIDENCE OF CHAFING ON LOWER EDGE OF FRAME 5, X 4692, Y 2560, Z 317, DURING PRE CLOSE INSPECTION OF AVIONIC BAY. NOTE THAT CURRENT HARDWARE IS IN LINE WITH THE GAP IN-BETWEEN FRAME 5 AND MED WALL AND ONLY CONTACTS IF TRIM IS DEFLECTED BACK WHEN PUSHING ON SNAP OR MED MOUNT INSTALL.