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
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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
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Cockpit Indications
Figure 004
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Cockpit Indications
R Figure 004A
R 1EFF : 301-399, 1 28-40-00 Page 12
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Cockpit Indications
R Figure 004B
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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.
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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
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REFERENCE QTY DESIGNATION
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No specific safety barriers
No specific warning notice
460005835 1 GROUND LOCK SLEEVE
B. Referenced Information
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