(d) If the harness is serviceable:
- replace the SENSOR-HI LEVEL, LEFT WING TANK INNER CHANNEL A (17QJ1) (Ref. AMM TASK 28-46-15-000-001) and (Ref. AMM TASK 28-46-15-400-009).
(12) CTL PNL-REFUEL/DEFUEL internal trouble-shooting (Ref. AWM 28-46-01) and (Ref. AWM 28-46-02):
(a) Check/replace the SW-TEST/LTS/HIGH (2QJ) (part of 800VU).
(b) Check/repair the CTL PNL-REFUEL/DEFUEL 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 T to IND-HI LVL/LEFT (3QJ), terminal I.
(c) Install the CTL PNL-REFUEL/DEFUEL (800VU) (Ref. AMM TASK 28-25-55-400-001).
(d) Do the test given in Para. 3.A.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : 301-399, ∞∞28-46-00∞∞∞∞∞∞∞∞∞∞Page A265
May 01/05R
CES **ON A/C ALL
TASK 28-46-00-810-824
RIGHT HI LVL Manual TEST
WARNING : OBEY THE FUEL SAFETY PROCEDURES.
_______
1. Possible Causes
_______________
- FLSCU-2 (9QJ)
- HARNESS-CHAN A, R WING TK INR (13QT2)
- SENSOR-HI LEVEL, RIGHT WING TANK INNER CHANNEL A (17QJ2)
- TANK HARNESS INNER A (58QT)
- Panel Assy-Refuel (800VU)
- aircraft wiring
- SWITCH-TEST/HIGH/LTS (2QJ) (part of 800VU)
- Panel Assy-Refuel (800VU) internal wiring
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific multimeter
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 28-10-00-910-001 Safety Procedures When You Do Work in a Fuel Tank AMM 28-25-55-000-001 Removal of the Refuel Panel 800VU AMM 28-25-55-400-001 Installation of the Refuel Panel 800VU AMM 28-42-43-000-005 Removal of the Wing Tank Harness 57QT(58QT),
63QT(64QT) AMM 28-42-43-000-006 Removal of the Wing-Tank Inner-Cell Group A Harness R 13QT1(13QT2) AMM 28-42-43-400-005 Installation of the Wing Tank Harness 57QT(58QT), 63QT(64QT) AMM 28-42-43-400-006 Installation of the Wing-Tank Inner-Cell Group A
Harness 13QT1(13QT2) AMM 28-46-00-710-001 Test of the Tank High Level Sensing System AMM 28-46-15-000-001 Removal of the Wing-Tank Fuel-Level Sensors AMM 28-46-15-400-009 Installation of the Wing-Tank Fuel-Level Sensors AMM 28-46-34-000-001 Removal of the Fuel-Level Sensing Control-Unit
(FLSCU) (7QJ,9QJ)
「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 A266
May 01/05 CES -------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 28-46-34-400-001 Installation of the Fuel-Level Sensing Control-Unit
(FLSCU) (7QJ,9QJ)
AWM 28-46-01
AWM 28-46-02
3. Fault Confirmation
__________________
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
A. Do the Operational Test of the HI LVL Lights (Ref. AMM TASK 28-46-00-710-001).
NOTE : You can get more Trouble-shooting data from the CFDS(FUEL):
____
- Input Parameters Page 3 (Ref. P. Block 301), used with the Fuel Level Sensors Operating (Changeover) Values (Ref. P. Block 301)
- FLSCU Trouble-shooting Data (Ref. P. Block 301).
With the HIGH LVL TEST switch in the central (released) position
the lamp state, off or on, must agree with the bit indicator 0 or
1 respectively, in the Input Parameters Page 3.
NOTE : OPTIONAL TESTING:
____ Where a PSD A320-2 Fuel Level Sensing Test Set is available measurements can be taken before a decision is made to go into or close up a fuel tank. The Test Set enables the tank mounted components and tank wiring to be tested from the tank wall connectors.
**ON A/C 301-399,
A. Do the Operational Test of the HI LVL Lights (Ref. AMM TASK 28-46-00-710-001).
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