- aircraft wiring (CTR TK low level 2 off latch (ground) line) between the RELAY (68QA) terminal 2 and the RELAY (14QU), terminal D3
- SEQUENCE VALVE
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
28-21-00-810-816 Fuel Pumps - Center Tank Autofeed Warning and/or
FAULT Legend Failure AMM 12-11-28-650-003 Pressure Refuel with Automatic Control AMM 27-51-34-000-001 Removal of the SFCC (21CV,22CV) AMM 27-51-34-400-001 Installation of the SFCC (21CV,22CV) AMM 27-80-00-866-005 Retracting the Slats on the Ground AMM 28-21-00-710-007 Operational Test of the Main Fuel-Pump System with
Fuel Flow by Transfer
AMM 28-21-00-720-001 Functional Test of the Center-Tank Fuel Control
AMM 28-21-45-000-001 Removal of the Sequence Valve
AMM 28-21-45-400-003 Installation of the Sequence Valve
AMM 28-21-51-000-002 Removal of the Fuel Pumps 37QA(38QA)
AMM 28-21-51-400-002 Installation of the Fuel Pumps 37QA(38QA)
AMM 28-25-00-650-001 Pressure Defuel
「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, ∞∞28-21-00∞∞∞∞∞∞∞∞∞∞Page A266
201-299, 401-499, Aug 01/05 CES -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 28-25-00-869-001 Fuel Transfer
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 31-60-00-860-001 EIS Start Procedure
ASM 28-21/04
3. Fault Confirmation
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A. During normal operation of the ECAM, the FUEL - AUTO FEED FAULT is a configuration warning.
NOTE : This ECAM warning is only given in certain flight phases, and is
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controlled by the FWC.
This warning function is activated simultaneously with the FAULT legend on the P/BSW-CTR TK/MODE SEL/AUTO (48QA).
NOTE : The FAULT is only given with the P/BSW in the AUTO (in) position.
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These indications are given because the fuel load distribution is not correct or the fuel has not been used in the correct sequence.
The warnings will be activated if for 60 seconds the fuel distribution (for any reason) is as follows:
- the left wing tank, less than 5000 kg (11000 lb) AND the center tank, more than 250 kg (550 lb)
- the right wing tank, less than 5000 kg (11000 lb) AND the center tank, more than 250 kg (550 lb).
The warnings will be reset immediately when the fuel distribution
conditions no longer exist.
The source of the comparison logic which activates and resets this
warning is contained in the FQIC (3QT).
The FQIC warning/FAULT logic output is inhibited during automatic
pressure refuel.
The FQIC warning/FAULT logic output is transmitted on:
- two (2) ARINC bus lines to the FWC (ECAM)
- two (2) discrete signal lines OR gated together to the P/BSW-CTR TK/MODE SEL/AUTO (48QA), FAULT legend.
(1) Examine the aircraft log/investigate the fuel configuration at the time of the original/repeat failure. Compare this with the fuel configuration given before.
「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, ∞∞28-21-00∞∞∞∞∞∞∞∞∞∞Page A267
201-299, 401-499, Aug 01/05 CES
(2) Do the BITE test of the FLSS (Ref. AMM TASK 28-46-00-740-001).
(3) If failures are detected examine the FLSS STATUS page for any of the messages that follow:
- FLSCU1(2) 7QJ(9QJ)
- C LO LEVEL SENSOR 21QJ
- C LO LEVEL SENSOR 22QJ
- L(R) FULL LEVEL SENSOR 23QJ1(2)
- L(R) UNDERFULL LEVEL SENSOR 24QJ1(2)
- L(R) UNDERFULL LEVEL SENSOR 25QJ1(2)
- L(R) UNDERFULL LEVEL SENSOR 26QJ1(2)
- L(R) FULL LEVEL SENSOR 27QJ1(2).
(4) If none of the messages identified in Step (3) are shown:
- go to Step (6).
(5) If one or more of the messages identified in Step (3) are shown: 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址:A320 Trouble Shooting Manual 排故手册 FUEL 燃油1(140)