What was found
VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE CRACKED RT SIDE AT APPROX STG DATUM 55.62 PERCENT. EVALUATED DAMAGES TO BE OUT OF LIMITS IAW SRM 55-00-00-101-001. SUMITTED TO ENGINEERING FOR PERMANENT REPAIR DISPOSITION. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. RECEIVED RESPONCE FROM THD REF: ADR JLFB-14-26550542, CAR 83335, PART HAS TO BE REPLACED. REMOVED DAMAGED RT DRAG ANGLE AT STR DATYUM 55.62 PERCENT IN REF TO SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. LOCATED HOLES COMMON TO FUSELAGE FOUND PREDRILLED PILOT HOLES ON DRAG ANGLE 73EA MISMATCHED FROM HOLES ON VERTICAL SKIN REF SRM 51-40-11-001-001-A01 AND DWG BA670-23-103.