What was found
RT FWD (WING SIDE) O/B FLAP I/B HINGE, BARREL NUT HOLE SPOTFACE CORRODED. RT FWD (WING SIDE) O/B FLAP I/B HINGE, BARREL NUT HOLE SPOTFACE CORROSION. REMOVED AS PER CMM 57-44-08, PAGES 402 - 407. ORIGINAL THICKNESS = 0.427 INCH, MATERIAL REMOVED = 0.006 INCH, REMAINING THICKNESS = 0.421 INCH FOUND WITHIN TOLERANCE OF DWG ARC0502.