What was found
AIRCRAFT FUSELAGE SKIN DAMAGE AT STA 500G-500H BETWEEN S18L A S19L. REF EC/RA 5330-06738. SEE L/P 4633454 FOR WORK ACCOMPLI ED.DIP REQUIREMENTS, ACCOMPLISH A INSPECTION PER PART 2 ON OR BEFORE 50,000. TOTAL AIRFRAME CYCLES.PLANNNING TO CONTACT ENGI ERING AFTER 47,000 TOTAL AIRFRAME CYCLES BUT BEFOERE 48,000 TO L AIRFRAME CYCLES FOR INSPECTION PROCEDURE. ACCOMPLISH AN INSPECTION PER PART 2 ON OR BEFORE 50,000. TOTAL A IRFRAF CYCLES.PLANNING TO CONTACT ENGINEERING AFTER 47,000. BUT BEFORE 48,000 AIRFRAME CYCLES FOR INSPECTION PROCEDURE. DIP INITIATED TO ACCOMPLISH INSPECTION PER PART 2 ON OR BEFORE 50,000 TOTAL AIRFRAME CYCLES. CONTACT ENGINEERING AFTER 47,000 TOTAL AIRFRAME CYCLES BUT BEFORE 48,000 TOTAL AIRFRAME CYCLES FOR INSPECTION PROCEDURES. TOMC-APPROVAL FROM SC1ELBYC COMMENT DIP INITIATED TO ACCOMPLISH INSPECTION PER PART 2 ON OR BEFORE 50,000 TOTAL AIRFRAME CYCLES. CONTACT ENGINEERING AFTER 47,000 TOTAL AIRFRAME CYCLES BUT BEFORE 48,000 TOTAL AIRFRAME CYCLES FOR INSPECTION PROCEDURES. QC REVIEWED QC REVIEWED RECORDS UPDATE....SS INIT : PLN/ENG > 47,000 < 48,000 TAFC T/A : 50,000 TAFC.....SS/U366014