What was found
TE FLAP DISAGREE EICAS FLAPS 20 USING ALT SYS PERFORMED OPS CHECK OF TE FLAP SYSTEM IAW AMM 27-51-00. PERFORMED FIM 27-51-00. NO CURRENT FAULTS. UNABLE TO DUPLICATE FAULT.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
TE FLAP DISAGREE EICAS FLAPS 20 USING ALT SYS PERFORMED OPS CHECK OF TE FLAP SYSTEM IAW AMM 27-51-00. PERFORMED FIM 27-51-00. NO CURRENT FAULTS. UNABLE TO DUPLICATE FAULT.