TASK 28-42-00-810-839

 Fuel Temperature Shows XX, Right Inner Cell WARNING : OBEY THE FUEL SAFETY PROCEDURES.
_______
 1. Possible Causes
_______________
 - FQIC (3QT)

 - PROBE-FUEL QTY NO 2, RIB 1-2 R WNG TK INR GROUP B (22QT2)

 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
28-42-00-810-805  Fuel Quantity/Temperature Probe 22QT1(2), Left(Right) Wing Tank
 3. Fault Confirmation
__________________
 A. On the ECAM CONTROL PANEL, push (in) the FUEL pushbutton switch (P/BSW).
 (1) Examine the fuel temperatures on the FUEL system page.

 (2) If the right inner cell fuel temperature shows correctly:

 - maintenance steps are not necessary.
 4. Fault Isolation
_______________
 A. If the right inner cell fuel temperature shows XX.
 (1) Examine the Post Flight Report (PFR) for the LRUs:

 - FQIC (3QT)

 - PROBE-FUEL QTY NO 2, RIB 1-2 R WNG TK INR GROUP B (22QT2).

 (2) If the LRUs listed in Para. (1) are shown:

 - do (Ref. TASK 28-42-00-810-805).
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 051-099, 101-149, 151-199, ∞∞28-42-00∞∞∞∞∞∞∞∞∞∞Page C258
 201-299, 401-499, Aug 01/05 CES

 TASK 28-42-00-810-840

 Fuel Temperature Shows XX, Right Outer Cell WARNING : OBEY THE FUEL SAFETY PROCEDURES.
_______
 1. Possible Causes
_______________
 - FQIC (3QT)

 - PROBE-FUEL QTY NO 13, RIB 16-17 R WNG TK OUTR GROUP A (33QT2)

 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
28-42-00-810-816  Fuel Quantity/Temperature Probe 33QT1(2), Left(Right) Wing Tank
 3. Fault Confirmation
__________________
 A. On the ECAM CONTROL PANEL, push (in) the FUEL pushbutton switch (P/BSW).
 (1) Examine the fuel temperatures on the FUEL system page.

 (2) If the right outer cell fuel temperature shows correctly:

 - maintenance steps are not necessary.
 NOTE : The right outer cell fuel temperature is not shown on the FUEL

____ System Display when the related fuel probe/temperature sensor 33QT2 is dry. Less than 130kg (290lb) of fuel in that cell.
 4. Fault Isolation
_______________
 A. If the right outer cell fuel temperature shows XX.
 (1) Examine the Post Flight Report (PFR) for the LRUs:

 - FQIC (3QT)

 - PROBE-FUEL QTY NO 13, RIB 16-17 R WNG TK OUTR GROUP A (33QT2).

 (2) If the LRUs identified in Para. (1) are shown:

 - do (Ref. TASK 28-42-00-810-816).
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 051-099, 101-149, 151-199, ∞∞28-42-00∞∞∞∞∞∞∞∞∞∞Page C259
 201-299, 401-499, Aug 01/05 CES

 **ON A/C 301-399,

 TASK 28-42-00-810-841
 Fuel Temperature Shows XX, Left Wing Tank
 WARNING : OBEY THE FUEL SAFETY PROCEDURES.

_______
 1. Possible Causes
_______________
 - FQIC (3QT)

 - PROBE-FQI NO 2 AND TEMP, RIB 1-2 L WNG TK GROUP B (54QT1)

 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
28-42-00-810-830  Fuel Quantity/Temperature Probe 54QT1(2), Left(Right) Wing Tank
 3. Fault Confirmation
__________________
 A. On the ECAM CONTROL PANEL, push (in) the FUEL pushbutton switch (P/BSW).
 (1) Examine the fuel temperatures on the FUEL system page.

 (2) If the left wing tank fuel temperature shows correctly:

 - maintenance steps are not necessary.
 NOTE : The left wing tank fuel temperature is supplied by a dual

____ element temperature sensor located within the fuel probe 54QT1.
　
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