Test of the Additional Center Tank (ACT) High-Level-Sensing System
TASK 28-46-00-710-002-A
Test of the Additional Center Tank (ACT) High-Level-Sensing System
To test at the refuel/defuel panels 800VU and 801VU the:
A. Fixtures, Tools, Test and Support Equipment
B. Work Zones and Access Panels
C. Referenced Information
3. Job Set-up
Subtask 28-46-00-941-058-A ** ON A/C NOT FOR ALL
Subtask 28-46-00-710-058-A ** ON A/C NOT FOR ALL
Subtask 28-46-00-860-060-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.02 07:03:14 UTC
Test of the Additional Center Tank (ACT) High-Level-Sensing System
WARNING:
OBEY THE FUEL SAFETY PROCEDURES.
WARNING:
PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU START A TASK ON OR NEAR:
1. Reason for the Job- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
To test at the refuel/defuel panels 800VU and 801VU the:
- HI LVL lights (for the wing tanks, the center tank and the ACT(s))
- High level sensors in the fuel tanks(for wing tanks 17QJ1 (17QJ2) and 28QJ1 (28QJ2), center tank 5QJ and ACTs 61QJX (62QJX) (X will be defined by the number of the ACT))
- FLSCU 7QJ (9QJ) (high level channels)
- ALSCU 60QJ (high level channels).
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | 1 | ACCESS PLATFORM 2M (6 FT) |
| No specific | AR | SAFETY BARRIER(S) |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 120 | AVIONICS COMPARTMENT |
| 192 | AIR CONDITIONING COMPT AND FAIRINGS |
| 211 | COCKPIT |
| 192MB, 811 |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 24-41-00-861-002-A | Energize the Aircraft Electrical Circuits from the External Power |
| TASK 24-41-00-861-002-A-01 | Energize the Aircraft Electrical Circuits from the APU |
| TASK 24-41-00-861-002-A-02 | Energize the Aircraft Electrical Circuits from Engine 1(2) |
| TASK 24-41-00-862-002-A | De-energize the Aircraft Electrical Circuits Supplied from the External Power |
| TASK 24-41-00-862-002-A-01 | De-energize the Aircraft Electrical Circuits Supplied from the APU |
| TASK 24-41-00-862-002-A-02 | De-energize the Aircraft Electrical Circuits Supplied from the Engine 1(2) |
| TASK 28-00-00-910-001-A | Fuel Safety Procedures |
Subtask 28-46-00-941-058-A ** ON A/C NOT FOR ALL
A. Safety Precautions
(1) Obey the fuel safety procedures (Ref. AMM TASK 28-00-00-910-001).
(2) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
Subtask 28-46-00-860-059-A ** ON A/C NOT FOR ALL (1) Obey the fuel safety procedures (Ref. AMM TASK 28-00-00-910-001).
(2) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
B. Aircraft Maintenance Configuration
(Ref. AMM TASK 24-41-00-861-002).
Subtask 28-46-00-010-057-B ** ON A/C NOT FOR ALL WARNING:
MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED BEFORE YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT. UNWANTED ELECTRICAL POWER CAN BE DANGEROUS.
(1) Energize the aircraft electrical circuits(Ref. AMM TASK 24-41-00-861-002).
C. Get Access
(1) Get access to ACT high-level-sensor-selector-switches 72QJ1, 72QJ2 (if ACT AFT2 is installed) and 72QJ4 (if ACT FWD is installed) in the avionics compartment (on panel 102VU):
(a) Put an ACCESS PLATFORM 2M (6 FT) in position at access door 811.
(b) Open access door 811.
(2) Get access to refuel/defuel control-panels 800VU and 801VU:
(a) Open access door 192MB.
4. Procedure(1) Get access to ACT high-level-sensor-selector-switches 72QJ1, 72QJ2 (if ACT AFT2 is installed) and 72QJ4 (if ACT FWD is installed) in the avionics compartment (on panel 102VU):
(a) Put an ACCESS PLATFORM 2M (6 FT) in position at access door 811.
(b) Open access door 811.
(2) Get access to refuel/defuel control-panels 800VU and 801VU:
(a) Open access door 192MB.
Subtask 28-46-00-710-058-A ** ON A/C NOT FOR ALL
A. Test of the HI LVL Lights (lamp check)
(1) Do this test:
Subtask 28-46-00-710-059-B ** ON A/C NOT FOR ALL (1) Do this test:
| ACTION | RESULT |
|---|---|
| 1.On panels 800VU and 801VU: | |
| |
| 2.On panel 800VU: | On panels 800VU and 801VU: |
|
|
|
|
B. High-Level-Sensing System Test
(a) Record the position of ACT high-level-sensor selector-switches 72QJ1, 72QJ2 (if ACT AFT2 is installed) and 72QJ4 (if ACT FWD is installed).
(b) Set ACT high-level-sensor selector-switches 72QJ1, 72QJ2 (if ACT AFT2 is installed) and 72QJ4 (if ACT FWD is installed) to the NORM position.
(2) Do this test:
(3) In the avionics compartment, on panel 102VU:
(a) Set ACT high-level-sensor selector-switches 72QJ1, 72QJ2 (if ACT AFT2 is installed) and 72QJ4 (if ACT FWD is installed) in the SPARE position.
(4) Do the test from step (2) again.
(5) In the avionics compartment, on panel 102VU:
(a) Set ACT high-level-sensor selector-switches 72QJ1, 72QJ2 (if ACT AFT2 installed) and 72QJ4 (if ACT FWD is installed) back to their initial positions.
5. Close-upNOTE: The HI LVL lights of the ACT(s) that are not installed will not operate in the tests that follow.
NOTE: Quantity of fuel in each tank to be equal to the subsequent results of the high level test. You can do a check (for each tank) on FUEL QTY indicator 6QT and ACT refuel/defuel-panel 801VU to find which of these conditions is applicable:
(1) In the avionics compartment, on panel 102VU: - Condition 1. The quantity of fuel is less than the high level.
- Condition 2. The quantity of fuel is at or more than the high level.
(a) Record the position of ACT high-level-sensor selector-switches 72QJ1, 72QJ2 (if ACT AFT2 is installed) and 72QJ4 (if ACT FWD is installed).
(b) Set ACT high-level-sensor selector-switches 72QJ1, 72QJ2 (if ACT AFT2 is installed) and 72QJ4 (if ACT FWD is installed) to the NORM position.
(2) Do this test:
| ACTION | RESULT |
|---|---|
| 1.On panel 800VU: | On panel 800VU and 801VU: |
| For condition 1 (see note):
|
| | For condition 2 (see note):
|
| For condition 1 (see note):
|
| | For condition 2 (see note):
|
(a) Set ACT high-level-sensor selector-switches 72QJ1, 72QJ2 (if ACT AFT2 is installed) and 72QJ4 (if ACT FWD is installed) in the SPARE position.
(4) Do the test from step (2) again.
(5) In the avionics compartment, on panel 102VU:
(a) Set ACT high-level-sensor selector-switches 72QJ1, 72QJ2 (if ACT AFT2 installed) and 72QJ4 (if ACT FWD is installed) back to their initial positions.
Subtask 28-46-00-860-060-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
(1) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
Subtask 28-46-00-410-056-A ** ON A/C NOT FOR ALL (1) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
B. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Close access door 192MB.
(3) Close access door 811.
Subtask 28-46-00-942-058-A ** ON A/C NOT FOR ALL (1) Make sure that the work area is clean and clear of tools and other items.
(2) Close access door 192MB.
(3) Close access door 811.
C. Removal of Equipment
(1) If installed, remove the safety barriers.
(2) Remove the access platform(s).
(3) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
(1) If installed, remove the safety barriers.
(2) Remove the access platform(s).
(3) Remove the ground support and maintenance equipment, the special and standard tools and all other items.