What was found
LT AFT FUSELAGE HAS A TEAR IN THE FUSELAGE SKIN BETWEEN THE 1ST AND 2ND NUMBERS IN THE REGISTRATION NUMBER. AFT FUSELAGE STA 887 STRINGER 19L REMOVED DAMAGED AREA AND INSTALLED REPAIR IN REF TO SRM 53-00-01, REPAIR 3. INITIATED DIP REF SRM 53-00-01 REPAIR 3 STEP 5D TABLE 205 CONTROL 53-DIP. REINSPECT STARTING AT 50,000 FLIGHT AND THEREAFTER PER TABLE 205. INSPECT AT 50,000 TOTAL FLT CYCS AND EVERY 4000 FLT CYCS ACCOMP DV AND EVERY 7000 FLT CYCS ACCOMP LFEC, AND INTERNAL LFEC AND VISUAL EVERY 36,000 FLT CYCS.