DOC AIRBUS | TSM A320FFuel High/Low Temperature Configuration Warning, Left(Right) Inner Cell
TASK 28-42-00-810-844-A
Fuel High/Low Temperature Configuration Warning, Left(Right) Inner Cell
A. Referenced Information
3. Fault Confirmation
Subtask 28-42-00-710-093-A ** ON A/C NOT FOR ALL
Subtask 28-42-00-810-093-A ** ON A/C NOT FOR ALL
[Rev.8 from Aug 2018]
2026.04.04 04:29:07 UTC
Fuel High/Low Temperature Configuration Warning, Left(Right) Inner Cell
WARNING:
OBEY THE FUEL SAFETY PROCEDURES.
1. Possible Causes- configuration warning
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| TSM TASK 28-42-00-810-805-A | Fuel Quantity/Temperature Probe 22QT1(2), Left(Right) Wing Tank |
Subtask 28-42-00-710-093-A ** ON A/C NOT FOR ALL
A. During normal operation of the FQIS/FWC/DMC this is a configuration warning . The temperature of the fuel in the inner cell is more or less than the limit for safe operation of the aircraft in flight. It is not a warning of a system/LRU failure or malfunction.
If in flight phase 02 or 06 L (R) INNER TK HI TEMP is shown. This indication could be spurious and related to HF interference.
Follow the maintenance advice in Fault Isolation.
4. Fault IsolationIf in flight phase 02 or 06 L (R) INNER TK HI TEMP is shown. This indication could be spurious and related to HF interference.
Follow the maintenance advice in Fault Isolation.
Subtask 28-42-00-810-093-A ** ON A/C NOT FOR ALL
A. Maintenance
(1) After 2 minutes the the fuel temperature measurement will be updated. If the indication is spurious, the temperature will return to normal limits after the next refresh of the fuel temperature indication system. After 2 - 3 minutes if the fuel high temperature indication decreases to normal. The high temperature indication can be accepted as spurious. The aircraft can dispatch as normal.
(2) If the fuel temperature does not return to normal, the ECAM and FCOM procedures must be followed.
(1) After 2 minutes the the fuel temperature measurement will be updated. If the indication is spurious, the temperature will return to normal limits after the next refresh of the fuel temperature indication system. After 2 - 3 minutes if the fuel high temperature indication decreases to normal. The high temperature indication can be accepted as spurious. The aircraft can dispatch as normal.
(2) If the fuel temperature does not return to normal, the ECAM and FCOM procedures must be followed.
NOTE: For more data refer to TFU 28.42.00.44 Inner and Outer Fuel Tank High Temperature indication.
(3) If the Inner Cell temperature system is under suspicion: