What was found
IN BS 616 FRAME TO STUB BEAM INNER CHORD LT SIDE CRACKED. REMOVED DAMAGE AND INSTALLED REPAIR STIFFENER ANGLE IAW TR 53-62-01, DEFECT SIZE: 1.5 INCH.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
IN BS 616 FRAME TO STUB BEAM INNER CHORD LT SIDE CRACKED. REMOVED DAMAGE AND INSTALLED REPAIR STIFFENER ANGLE IAW TR 53-62-01, DEFECT SIZE: 1.5 INCH.