What was found
INSPECTION FOUND A 1 INCH CRACK ON SUPPORT ANGLE ATTACHED TO FRAME AT BS 1540 BETWEEN STRINGER 37 TO 38L. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK ON SUPPORT ANGLE ATTACHED TO FRAME AT BS 1540 BETWEEN STRINGER 37 TO 38L. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-02.