Indicating - Power Supplies
 Figure 002

R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 28-40-00Page 6 1201-299, 401-499, 1Aug 01/05 1 1 1CES 11EFF : ALL 1 28-40-00Page 7 1 1 Aug 01/05 1 1 1CES 1

 **ON A/C 301-399,
 (Ref. Fig. 002A) **ON A/C ALL
R  5. Interfaces__________ **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 (Ref. Fig. 003) **ON A/C 301-399,
 (Ref. Fig. 003A) **ON A/C ALL
R  6. Operation/Control and Indicating________________________________ **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299,
R  (Ref. Fig. 004) **ON A/C 301-399,
R  (Ref. Fig. 004A) **ON A/C 401-499,
R  (Ref. Fig. 004B) 

R  Indicating - Power Supplies 
R  Figure 002A
 1EFF :  301-399,  1  28-40-00 Page 8 
1  1  May 01/04
 1  1
 1CES  1

 Indicating - Interfaces
 Figure 003

R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 28-40-00Page 9 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1

R  Indicating - Interfaces 
R  Figure 003A
 1EFF :  301-399,  1  28-40-00 Page 10 
1  1  May 01/04
 1  1
 1CES  1

 Cockpit Indications
 Figure 004

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 Cockpit Indications 
R  Figure 004A 
R 1EFF :  301-399,  1  28-40-00 Page 12 
1  1  Aug 01/05
 1  1
 1CES  1

 Cockpit Indications 
R  Figure 004B 
R 1EFF :  401-499,  1  28-40-00 Page 13 
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 1  1
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 **ON A/C ALL
 A. Control and Indicating
 (1) Control
 The FQIC and the FLSCU automatically control the FQI system and the FLSS. The MLIs are a secondary system used to calculate the fuel in the fuel tanks when the A/C is on the ground.
R 1EFF : ALL 1 28-40-00Page 14 1 1 Aug 01/05 1 1 1CES 1 (2) Indications

 The FQI, and the temperature measurement indications are shown on the SD (FUEL page). When specified FQI and FLSS conditions occur, the EWD (Ref. 31-66-00) gives a warning message and the Flight Warning Computer (FWC) (Ref. 31-53-00) gives an audible warning.
 The MLIs have fuel level marks which can be seen when the MLI is extended.
 7. BITE Test
_________
 The built-in test equipment (BITE) is installed in the FQI computer. It monitors inputs, outputs and operations to give results from the regular system tests. Fault information for each flight, and up to sixty-four flight legs are kept in the BITE memories. The menus on the Multipurpose Control and Display Units (MCDUs) (Ref. 28-42-00) give access to the test results. The tests also monitor some of the fuel system inputs to the Flight Warning System (FWS). Test modes are not available in flight. A high level test switch is provided to allow limited BITE testing of the high level sensors only.
 1EFF : ALL 1 28-40-00Page 15 1 1 Aug 01/05R 1 1 1CES 1

 INDICATING - DEACTIVATION/REACTIVATION
______________________________________
 TASK 28-40-00-040-001
 APU LP Valve Indication - Valve Closure Procedure
 WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
 START A TASK ON OR NEAR:

 -
THE FLIGHT CONTROLS

 -
THE FLIGHT CONTROL SURFACES

 -
THE LANDING GEAR AND THE RELATED DOORS

 -COMPONENTS THAT MOVE.
 WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
 GEAR.

 1. Reason for the Job
__________________
 Refer to the MMEL TASK: 28-40-06-C)
 Indications on ECAM FUEL page
 APU LP valve indication

 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------
REFERENCE  QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific safety barriers
 No specific warning notice
 460005835 1 GROUND LOCK SLEEVE

 B. Referenced Information
 -------------------------------------------------------------------------------
　
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