What was found
STA 601 RIGHT SIDE ON INNER CORD ANGLE JUST BELOW CABIN FLOOR LEVEL CRACKED. REMOVED DAMAGED MATERIAL, INSTALLED FILLER AND STIFFENER ANGLE IAW TR 53-62-01 & EA 97193, DEFECT SIZE: 1.5 INCH CRACK.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
STA 601 RIGHT SIDE ON INNER CORD ANGLE JUST BELOW CABIN FLOOR LEVEL CRACKED. REMOVED DAMAGED MATERIAL, INSTALLED FILLER AND STIFFENER ANGLE IAW TR 53-62-01 & EA 97193, DEFECT SIZE: 1.5 INCH CRACK.