As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFTER ROTATION PRIOR TO GEAR RETRACTION THE LEFT I/B AND RIGHT O/B ANTI SKID RELEASE LIGHTS ILLUMINATED. PLACED ANTI SKID SYS ON DMI 2456 PER MEL 32-5. TROUBLESHOT SYS PER M/M 32-42-0, SYS CHKS OK. SWAPPED TRANSDUCERS FOR T/S. TEST OK PER M/M 32-42-0.