What was found
TE FLAPS DISAGREE EICAS DURING APPROACH, EXTENDED WITH ALTERNATE SYS LANDED WITH FLAPS AT 20. BITE TEST OF EFCU, NO EXISTING FAULTS. CYCLED FLAP HYDRAULICLY SEVERAL TIMES NO FAULTS NOTED. IAW AMM 27-51-00
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
TE FLAPS DISAGREE EICAS DURING APPROACH, EXTENDED WITH ALTERNATE SYS LANDED WITH FLAPS AT 20. BITE TEST OF EFCU, NO EXISTING FAULTS. CYCLED FLAP HYDRAULICLY SEVERAL TIMES NO FAULTS NOTED. IAW AMM 27-51-00