What was found
DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND 2, 2 INCH CRACKS IN THE LEFT ENGINE PYLON CLOSING RIB WEB. REPAIRED WEB PER EA 12-5410-9-C0782.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND 2, 2 INCH CRACKS IN THE LEFT ENGINE PYLON CLOSING RIB WEB. REPAIRED WEB PER EA 12-5410-9-C0782.