What was found
DURING LCK, FUSELAGE SKIN PANELS REQUIRED REPAIR BY BLENDING OUT WEAR DAMAGE AT THE VERTICAL STAB SEAL INTERFACE. FOLLOW-ON SURFACE HFEC INSP ARE REQ PER EM 5331-01190, SECTION 02. BOEING SB 747-53A2470, REV 2 / FAA AD 2009-14-02. ACCOMP SURFACE HFEC INSP PER SECT II OF ER/A 491632-14AD PRIOR TO 20,000 TOTAL FC AND REPEAT AT INTERVALS NOT TO EXCEED 6,000 FC. AA 5331-01190 ADDED FOR AC 6309 ASSOCIATED ER/A 13-491632 ADDED FOR AC 6309.