What was found
CRACK INDICATION NOTED AT FRAME BS 500C BETWEEN STRINGER S8-9L DURING MFEC INSPECTION. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR ANGLES IAW EA 5 310-04716, REV D, OP1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK INDICATION NOTED AT FRAME BS 500C BETWEEN STRINGER S8-9L DURING MFEC INSPECTION. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR ANGLES IAW EA 5 310-04716, REV D, OP1.