What was found
DURING GVI OF THE WING BOX SHEAR TIE FITTING, FOUND CRACK AFT OF FASTENER HOLE TO EDGE FITTING AT STA 548 /LBL 16. HFEC INSPECTION OF SHEAR TIE CONFIRMED CRACK. REMOVED & REPLACED SHEAR TIE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING GVI OF THE WING BOX SHEAR TIE FITTING, FOUND CRACK AFT OF FASTENER HOLE TO EDGE FITTING AT STA 548 /LBL 16. HFEC INSPECTION OF SHEAR TIE CONFIRMED CRACK. REMOVED & REPLACED SHEAR TIE.