What was found
RIGHT WING INBOARD T/E UPPER FIXED PANEL SKIN CRACK, WBL 235.2. I.A.W. 747-400F SRM 57-51-01-2R-1 REFER TO SRM 51-70-07-0G-0 REV. 106 PERFORM REPAIR AS BELOW STEP: 1.1 REMOVE THE CRACK MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 260°F FOR 130 MINUTES WITH A MINIMUM VACUUM OF 22 IN/HG. INSTALLED FASTENERS OF R/H WING INBD T/E UPPER FIXED PANEL WBL 235.2 I.A.W SRM 51-40-02-0G REV.106 AND BOEING DWG: 113U1011 SHEET 22 REV.A.