What was found
LT WING (WING SIDE) OTBD FLAP, OTBD HINGE SIDE LOAD FITTING SURFACE FOUND CORROSION. REWORKED IAW CMM 20-11-02, REVISION 72. UPPER EXISTING THICKNESS: 0.425", MATERIAL REMOVED: 0.009", REMAINING THICKNESS: 0.416". LOWER EXISTING THICKNESS: 0.413", MATERIAL REMOVED: 0.010", REMAINING THICKNESS: 0.403". REPAIR ACCOMPLISHED IAW EA NR 1-5750-160020 PART 1, STEPS 5, 7 AND 8. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 114.