As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CAPT F/D INOP. AFTER ENG START ON RECALL SPEED TRIM FAIL LIGHT AND MACH TRIM FAIL LIGHT ILLUMINATED. CYCLED POWER TO "A" FCC COMPUTER. PERFORMED FCC LRU INTERFACE TEST REF MM 22 11 33/401 & LAND VERIFY TEST REF MM 22 11 00/201 BITE 49, ALL TESTS PASSED. HGS SENSOR TEST FOR FCC/AT PASSED REF MM 34 36 00. A/C REMAINS CAT IIIA AUTOLAND & HGS QUAL. SCREW POSTION REFLECTS SAME.