What was found
NO.10 V/C FLAP TOP EDGE METAL STRIP O/B AREA FOUND DAMAGE(<P>NO.10 V/C FLAP TOP EDGE METAL STRIP REPLACED AS PER CMM 57-55-42 ASSEMBLY PAR 2C 5A ( 6 ).</P>)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NO.10 V/C FLAP TOP EDGE METAL STRIP O/B AREA FOUND DAMAGE(<P>NO.10 V/C FLAP TOP EDGE METAL STRIP REPLACED AS PER CMM 57-55-42 ASSEMBLY PAR 2C 5A ( 6 ).</P>)