As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AT TOP OF CLIMB LEFT FUEL QTY AND TOTALIZER INOP. DIVERTED A/C TO OAK. ON DESCENT BECAME INTERMITTENT. REMOVED AND REPLACED FUEL QUANTITY INDICATING SYSTEM PROCESSOR UNIT PER AMM 28-41-08. PERFORMED OPERATIONAL TEST PER AMM 28-41-00 AND OPS CHECKS GOOD WITH NO FAULTS NOTED ON PROCESSOR. OK FOR SVC.