Narrative:

During the initial takeoff roll; we received an erroneous EFIS alert for low fuel temperature in the #2 main fuel tank. Since the tank temperature showed -55 degree C (-67 degree F) and the outside air temperature was above 80 degrees F; it was obvious that the indication was incorrect; so we continued the takeoff. Within 1 min after liftoff; the temperature indication returned to normal. The A319 is designed to inhibit all but a number of alerts during takeoff once the thrust has been set. Prior to that; alerts are displayed on the ECAM and a chime is sounded. For true malfunctions; the benefit is obvious. However; erroneous indications can create temporary distraction and confusion during a critical phase of flight. Fortunately for us; it was daylight VFR with no traffic considerations and a long runway available. Had the WX been low IFR with a lot of traffic on the taxiway or traffic on short final; the potential existed for an unnecessary abort or go around. Computerized aircraft system can occasionally generate faulty information requiring the crew to analyzesituation correctly. During certain phases of flight; this can be difficult and pose a reduction in the margin of safety if the information is not correctly interpreted.

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Original NASA ASRS Text

Title: A319 CAPTAIN REPORTS DISTRACTION FROM FALSE FUEL TANK TEMPERATURE ECAM WARNING DURING TKOF ROLL.

Narrative: DURING THE INITIAL TKOF ROLL; WE RECEIVED AN ERRONEOUS EFIS ALERT FOR LOW FUEL TEMP IN THE #2 MAIN FUEL TANK. SINCE THE TANK TEMP SHOWED -55 DEG C (-67 DEG F) AND THE OUTSIDE AIR TEMP WAS ABOVE 80 DEGS F; IT WAS OBVIOUS THAT THE INDICATION WAS INCORRECT; SO WE CONTINUED THE TKOF. WITHIN 1 MIN AFTER LIFTOFF; THE TEMP INDICATION RETURNED TO NORMAL. THE A319 IS DESIGNED TO INHIBIT ALL BUT A NUMBER OF ALERTS DURING TKOF ONCE THE THRUST HAS BEEN SET. PRIOR TO THAT; ALERTS ARE DISPLAYED ON THE ECAM AND A CHIME IS SOUNDED. FOR TRUE MALFUNCTIONS; THE BENEFIT IS OBVIOUS. HOWEVER; ERRONEOUS INDICATIONS CAN CREATE TEMPORARY DISTRACTION AND CONFUSION DURING A CRITICAL PHASE OF FLT. FORTUNATELY FOR US; IT WAS DAYLIGHT VFR WITH NO TFC CONSIDERATIONS AND A LONG RWY AVAILABLE. HAD THE WX BEEN LOW IFR WITH A LOT OF TFC ON THE TXWY OR TFC ON SHORT FINAL; THE POTENTIAL EXISTED FOR AN UNNECESSARY ABORT OR GAR. COMPUTERIZED ACFT SYS CAN OCCASIONALLY GENERATE FAULTY INFO REQUIRING THE CREW TO ANALYZESITUATION CORRECTLY. DURING CERTAIN PHASES OF FLT; THIS CAN BE DIFFICULT AND POSE A REDUCTION IN THE MARGIN OF SAFETY IF THE INFO IS NOT CORRECTLY INTERPED.

Data retrieved from NASA's ASRS site as of May 2009 and automatically converted to unabbreviated mixed upper/lowercase text. This report is for informational purposes with no guarantee of accuracy. See NASA's ASRS site for official report.