What was found
WEAR WAS FOUND AT FUSELAGE SKIN AND VERTICAL STABILIZER SEAL INTERFACE. STA 2521-2628. MAX DEPTH: 0.027" IAW ER/A 488622-14AD, REV 0 AND SRM 53-00-01, REPAIR 15, FIG 201 PERFORMED MED FUSELAGE SKIN-BUTT JOINT EXTERNAL REPAIR, THIS IS A CATEGORY" B" REPAIR INSP. REQUIREMENTS INSPECTION THRESHOLD: 1500 FLIGHT CYCLES, METHOD: INTERNAL HFEC INTERVAL 6000 FLIGHT CYCLES, REF: NDT PART6 51-00-00, FIG4. METHOD: EXTERNAL LFEC: INTERVAL: 1500 FLIGHT CYCLES, REF: NDT PART6, 53-30-00, FIG5.RII COMPLETED.