What was found
INSPECTION FOUND A .5 INCH CRACK IN UPPER RADIUS OF FITTING AFT OF FRAME JUST BELOW STRINGER 17L AND CREASE BEAM AT STA 616. A NEW FITTING WAS INSTALLED IAW SRM 51-10-2 AND 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK IN UPPER RADIUS OF FITTING AFT OF FRAME JUST BELOW STRINGER 17L AND CREASE BEAM AT STA 616. A NEW FITTING WAS INSTALLED IAW SRM 51-10-2 AND 51-40-02.