-----------------------------------------------------------------------------| LRU/CHANNEL | SENSOR | FLSCU-1 FLSCU-2 FQIC | | OUTPUT WIRE | FIN | CONNECTOR CONNECTOR CONNECTOR| | | | AND PIN AND PIN AND PIN | |------------------|--------|-------------------------------------------------| -----------------------------------------------------------------------------
(a) Repair all the unserviceable wiring and connectors.
(b) Do the test given in Para. 3.B.
「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 : 301-399, ∞∞28-46-00∞∞∞∞∞∞∞∞∞∞Page A243
May 01/05 CES
**ON A/C ALL
TASK 28-46-00-810-819
Fuel Low Level Configuration Warning, Left(Right) Wing Tank
1. Possible Causes
_______________
- FLSCU-1 (7QJ)
- FLSCU-2 (9QJ)
- SDAC-1 (1WV1)
- SDAC-2 (1WV2)
- aircraft wiring
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 28-46-00-740-001 Functional (BITE) Test AMM 28-46-34-000-001 Removal of the Fuel-Level Sensing Control-Unit (FLSCU) (7QJ,9QJ) AMM 28-46-34-400-001 Installation of the Fuel-Level Sensing Control-Unit
(FLSCU) (7QJ,9QJ)
AMM 31-55-34-000-001 Removal of the SDAC (1WV1,1WV2)
AMM 31-55-34-400-001 Installation of the SDAC (1WV1,1WV2)
ASM 28-46/02
3. Fault Confirmation
__________________
A. Table of the circuit breakers used in this procedure:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU SDAC/1/SPLY 3WV F04 121VU EIS/SDAC/2/SPLY 2WV Q06
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
B. During normal operation of the FLSS/FWC/DMC this is a configuration warning. If in the inner cell a pair of low level sensors that are AND gated together become dry indicating a fuel level of less than approximately 750kg (1650lb) for more than 30 seconds a low level warning is given. It is not a warning of a system/LRU failure or malfunction.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞28-46-00∞∞∞∞∞∞∞∞∞∞Page A244
Aug 01/05 CES
However, if the low level warning system is under suspicion:
(1) On the ECAM CONTROL PANEL push (in) the FUEL P/BSW.
(2) On the FUEL System Display (Lower ECAM) examine the wing tank FQIs.
(3) If the wing tank FQI(s) on the related side(s) show less than approximately 750kg (1650lb) when the L(R) or L + R WING TK LO LVL warning is given:
- no maintenance steps are necessary.
NOTE : Although this procedure has been written for when a permanent
____ LO LVL warning is given, the steps in the procedure are also applicable for when the wing tank FQIs show less than 750kg (1650lb) and the warning is not given.
**ON A/C 301-399,
B. During normal operation of the FLSS/FWC/DMC this is a configuration warning. If in a wing tank a pair of low level sensors that are AND gated together become dry indicating a fuel level of less than approximately 750kg (1650lb) for more than 30 seconds a low level warning is given. It is not a warning of a system/LRU failure or malfunction.
However, if the low level warning system is under suspicion:
(1) On the ECAM CONTROL PANEL push (in) the FUEL P/BSW.
(2) On the FUEL System Display (Lower ECAM) examine the wing tank FQIs.
(3) If the wing tank FQI(s) on the related side(s) show less than approximately 750kg (1650lb) when the L(R) or L + R WING TK LO LVL warning is given:
- no maintenance steps are necessary.
NOTE : Although this procedure has been written for when a permanent
____ LO LVL warning is given, the steps in the procedure are also applicable for when the wing tank FQIs show less than 750kg (1650lb) and the warning is not given.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞28-46-00∞∞∞∞∞∞∞∞∞∞Page A245
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 FUEL 燃油4(96)
