What was found
CRACK INDICATION NOTED ON FRAME BS 440 BETWEEN STRINGER S8-9L DURING MFEC INSPECTION. FRAME BS 440 HAS BEEN REPAIRED IAW EA 5310-04716, REV D OP1 FIG 3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK INDICATION NOTED ON FRAME BS 440 BETWEEN STRINGER S8-9L DURING MFEC INSPECTION. FRAME BS 440 HAS BEEN REPAIRED IAW EA 5310-04716, REV D OP1 FIG 3.