What was found
CABIN FUSELAGE INTERIOR FRAME WITH EXISTING REPAIR DOUBLER AT STA 1140, BETWEEN STRINGER S-1L TO S-3L. CABIN MAIN FRAME AT STA 1140, S-6L TO S-6R REPAIRED IAW SRM 53-00-07 REPAIR 1, REV. 99. INITIAL INSP THRESHOLD AT 50,000 FLIGHT CYCLES AND AN INTERVAL INSPECTION AT 12,000 FLIGHT CYCLES, INSP METHOD: DETAILED VISUAL INSPECTION. THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.