What was found
CRACK ON EXTERNAL FUSELAGE SKIN BETWEEN LONGERON 14 RT, STA Y=1086, CARD 10, ZONE 200. AREA WAS REPAIRED IAW ER/A 547824-14, REV ORIGINAL. PERFORM EXTERNAL GVI ON REPAIR EVERY 3,000 FLIGHT CYCLES IAW ER/A 547824-14, REV ORIGINAL, SEC II AND FOLLOW UP WITH LOG 2568619. RII COMPLETED.