- closed circuit for the switch in the TEST position.
NOTE : The LTS test checks the 28VDC supply to the Panel Assy-Refuel
____
(800VU).
(7) Replace the CTL PNL-REFUEL/DEFUEL (800VU), if it fails Step (6), (Ref. AMM TASK 28-25-55-000-001), and (Ref. AMM TASK 28-25-55-400-001).
NOTE : If due to airline operational conditions it is not possible to
____ replace the Panel Assy-Refuel (800VU) and internal Trouble-shooting is required, go to Step (12).
(8) If the fault continues do a wiring check (Ref. AWM 28-46-01), (Ref. AWM 28-46-02), and (Ref. AWM 28-46-03) of the aircraft wiring :
- between the Panel Assy-Refuel (800VU), connector 4024VC, pin R and the FLSCU-1 rack connector AA, pin 13B
- between the Panel Assy-Refuel (800VU), connector 4024VC, pin P and the FLSCU-1 rack connector AA, pin 7C
- between the FLSCU-1 rack connector AA, pin 6C and the DC1 ground/earth point
「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 : ALL ∞∞28-46-00∞∞∞∞∞∞∞∞∞∞Page A274
May 01/05 CES
- between the FLSCU-1 rack connector AB, pin 11A and the tank wall connector 7509VC, pin <B
- between the FLSCU-1 rack connector AB, pin 11B and the tank wall connector 7509VC, pin <C.
(9) Repair all the unserviceable wiring and connectors.
(10) Do the test given in Para. 3.A.
(11) If the fault continues:
(a) Drain, open and vent the tank (Ref. AMM TASK 28-10-00-910-001).
(b) Do a check of the HARNESS-CHAN A, CTR TK (17QT) (Ref. AWM 28-46-02).
(c) If the harness is unserviceable:
- replace the harness (Ref. AMM TASK 28-42-44-000-001) and (Ref. AMM TASK 28-42-44-400-001).
(d) If the harness is serviceable:
- replace the SENSOR-HIGH LEVEL, CENTER TANK (20QJ) (Ref. AMM TASK 28-46-15-000-004) and (Ref. AMM TASK 28-46-15-400-012).
(12) Panel Assy-Refuel (800VU) Internal Trouble-shooting (Ref. AWM 28-46-01) (Ref. AWM 28-46-02) and (Ref. AWM 28-46-03):
(a) Check/replace the SW-TEST/LTS/HIGH (2QJ).
(b) Check/repair the Panel Assy-Refuel (800VU) internal wiring as follows:
- connector 4023VC, pin <C to terminal block 4001VT, terminal 5C
- terminal block 4001VT, terminal 5J to SW-TEST/HI/LTS (2QJ), terminal 1B
- SW-TEST/HI/LTS (2QJ), terminal 3B to connector 4024VC, pin R
- connector 4024VC, pin P to IND-HI LVL/CTR (5QJ), terminal II.
(c) Install the Panel Assy-Refuel (800VU) (Ref. AMM TASK 28-25-55-400-001).
(d) Do the test given in Para. 3.A.
「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 : ALL ∞∞28-46-00∞∞∞∞∞∞∞∞∞∞Page A275
May 01/05 CES
**ON A/C 301-399,
TASK 28-46-00-810-843
Dummy Temperature Sensor 41QJ
WARNING : OBEY THE FUEL SAFETY PROCEDURES.
_______
WARNING : WHEN YOU DO WORK ON THE FUEL SYSTEM WIRING, YOU MUST USE TEST
_______ EQUIPMENT THAT IS APPROVED (REFER TO INTERNATIONAL OR NATIONAL SPECIFICATIONS FOR INTRINSICALLY SAFE TEST EQUIPMENT, E.G. EN50-020, UL913 OR EQUIVALENT). TEST EQUIPMENT THAT IS NOT APPROVED CAN CAUSE FIRE OR AN EXPLOSION.
1. Possible Causes
_______________
- FLSCU-1 (7QJ)
- aircraft wiring
- aircraft wiring (dummy sensor input line - L) between the FLSCU-1 rack connector AB, pin 7C and the terminal block 202VT, terminal 21C
- aircraft wiring (FLSCU-1 BITE 4 test command line) between the FLSCU-1 rack connector AA, pin 15D and the FQIC rack connector AB, pin 15E
- aircraft wiring (FLSCU-1 T2 output line) between the FLSCU-1 rack
connector AB, pin 4D and the FQIC rack connector AC, pin 2D
- RESISTOR-TEMP SENSOR DUMMY LOAD 41QJ
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
28-46-00-810-818 FLSCU1(2) 7QJ(9QJ)
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)
ASM 28-46/04
AWM 28-46-11
3. Fault Confirmation 中國(guó)航空網(wǎng) www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320 Trouble Shooting Manual 排故手冊(cè) FUEL 燃油4(109)
