What was found
DURING HIGH FREQUENCY EDDY CURRENT SURFACE INSPECTION ON THE RIGHT HAND FORWARD FLANGE OF LOWER VERTICAL STABILIZER REAR SPAR CAP AT STATION Y = 2164 , FOUND 01EA CRACK WITH LENGTH APPROXIMATELY 1.5" BETWEEN THE FIRST AND THIRD FASTENER FROM BELOW. VERTICAL STABILIZER REAR SPAR CAP RIGHT HAND FORWARD FLANGE AT STATION Y = 2164 CRACKED APPROXIMATELY 1.5" BETWEEN THE FIRST AND THIRD FASTENER FROM BELOW TRIMMED AS PER SRM 55-30-02-2R FIGURE 201 REPAIR 5, REPAIR CARRIED OUT AS PER SRM 55- 30-02-2R FIGURE 204 REPAIR 5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. TO CARRY OUT INITIAL INSPECTION AT EVERY 5,400 FLIGHT CYCLES AND REPETITIVE INSPECTION AT EVERY 2,700 FLIGHT CYCLES AS PER SRM 55-30-02-2R TABLE 203 REPAIR 5. METHOD OF INSPECTION BY ULTRASONIC AND HIGH FREQUENCY EDDY CURRENT PER SN10550000.