As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ON APPROACH; WHEN SETTING FLAPS 15 FLAP ASSYMETRY OCCURED; FLAPS 10 ON LEFT WING; FLAPS 15 ON RIGHT WING *CALL MOC SO WE CAN UPDATE THE LOGPAGE AND PAGE #*<[01] VERIFIED INTEGRITY OF WIRING FROM #7 & 8 SKEW SENSORS TO D43104J PER WDM 27-53-21<BR>REPLACED #7 SKEW SENSOR DUE TO POWER LOSS TO #8 SKEW SENSOR PER MM 27-59-01