What was found
LEFT WING LE NOTCH FLAP, CRACKED AT AFT CORNER. REMOVED THE NOTCH FLAP ASSEMBLY IAW AMM 27-87-13-04. FOUND FAIRING CRACKED & REMOVED FAIRING IAW AMM 27-87-13-04. THE FASTENER HOLE TRANSFER DRILL TO NEW FAIRING PANEL, PN A5351036620000, IAW SRM 51-40-40. ACCOMPLISHED THE WORK IAW EA 6-5720-T0307672. TITLE WING SECONDARY WING STRUCTURE LT KRUEGER NOTCH FLAP ASSEMBLY CRACK, TEMPORARY REPAIR. ADJUSTMENT & OPERATION CHECK OF THE SLAT KRUEGER & NOTCH FLAP IAW AMM 27- 80-00-03 & 27-87-13-04. IAW GMM 6-2-100 REPAIR CLASSIFIED AS MAJOR.