Level Sensing Test - ACT
TASK 28-46-00-740-002-A
Level Sensing Test - ACT
The FLSCU3 (47QJ) and related fuel level sensors are not Automatic FLSS BITE tested or monitored by the FQIC (3QT).
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Work Zones and Access Panels
C. Referenced Information
3. Job Set-up
Subtask 28-46-00-941-057-A ** ON A/C NOT FOR ALL
Subtask 28-46-00-740-052-A ** ON A/C NOT FOR ALL
Subtask 28-46-00-410-055-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.02 06:18:15 UTC
Level Sensing Test - ACT
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.
The FLSCU3 (47QJ) and related fuel level sensors are not Automatic FLSS BITE tested or monitored by the FQIC (3QT).
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE |
| No specific | AR | MULTIMETER - STANDARD |
| No specific | AR | SAFETY BARRIER(S) |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 192MB, 811 |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 12-11-28-650-003-A | Pressure Refuel with Automatic Control |
| 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 |
| TASK 28-25-00-869-001-A | Fuel Transfer |
| TASK 28-46-00-740-001-A | Functional (BITE) Test |
| TASK 28-46-34-000-001-B | Removal of the Fuel-Level Sensing Control-Unit (FLSCU) |
| TASK 28-46-34-400-001-B | Installation of the Fuel-Level Sensing Control-Unit (FLSCU) |
| TASK 31-60-00-860-002-A | EIS Stop Procedure |
Subtask 28-46-00-941-057-A ** ON A/C NOT FOR ALL
A. Safety Precautions
(2) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
Subtask 28-46-00-010-056-A ** ON A/C NOT FOR ALL WARNING:
OBEY THE FUEL SAFETY PROCEDURES.
(1) You must obey the fuel safety procedures when you do work on the fuel system (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. Get Access
(1) Put the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE in position at the access door 811 in zone 122.
(2) Open the access doors 811 and 192MB.
Subtask 28-46-00-860-057-A ** ON A/C NOT FOR ALL (1) Put the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE in position at the access door 811 in zone 122.
(2) Open the access doors 811 and 192MB.
C. Aircraft Maintenance Configuration
(Ref. AMM TASK 24-41-00-861-002).
(2) If the external power is not available, on the refuel/defuel panel 800VU:
Subtask 28-46-00-865-056-A ** 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).
(2) If the external power is not available, on the refuel/defuel panel 800VU:
- put the BATT POWER switch to the ON position.
NOTE: HOT BUSS 701PP is energized for ten minutes only to prevent discharge of the aircraft batteries, unless you put the MODE SELECT switch to REFUEL.
D. Make sure that this(these) circuit breaker(s) is(are) closed:
4. Procedure| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | FUEL/FQI/CHAN/1 | 1QT | A13 |
| 49VU | FUEL/AFT LOW LVL/& OVFL/WING R | 44QJ | A11 |
| 49VU | FUEL/AFT LOW LVL/& OVFL/WING L | 43QJ | A10 |
| 121VU | ACT1/REFUEL & SPLY | 33QU | L29 |
| 121VU | FUEL/FQI/CHANNEL/1 AND 2 | 8QT | L26 |
| 121VU | FUEL/HI/LVL/SPLY | 1QJ | L25 |
| 121VU | FUEL/RFL/DFL/SPLY | 2QU | L24 |
| 121VU | FUEL/RFL/DFL/XFR/DEFUEL/VALVE | 1QU | L23 |
| 121VU | ACT LOW LVL R | 51QJ | M29 |
| 121VU | ACT LOW LVL L | 52QJ | M28 |
| 121VU | FUEL/FQI/CHAN/2 | 2QT | M27 |
| 121VU | FUEL/FWD LOW LVL/WING/R | 45QJ | M23 |
| 121VU | FUEL/FWD LOW LVL/WING/L | 46QJ | M22 |
| 121VU | ACT XFR VALVE MAN CTL | 30QH | N29 |
| 121VU | ACT1/CTL & SPLY | 9QH | P29 |
| 121VU | ACT PUMP SUPPLY | 25QH | Q29 |
| 121VU | FUEL/CTR TK/L&R XFR/CTL & IND | 2QL | R26 |
| 121VU | FUEL/CTR TK/L&R XFR/CTL & IND | 1QL | R25 |
Subtask 28-46-00-740-052-A ** ON A/C NOT FOR ALL
A. Test of the FLSCU3 with BITE
(1) Do the BITE test of the FLSCU1 (7QJ) and the FLSCU2 (9QJ) (Ref. AMM TASK 28-46-00-740-001). Make sure that the test result is good.
(3) Remove the FLSCU3 (Ref. AMM TASK 28-46-34-000-001).
(4) Install the FLSCU initially installed in the FLSCU3 position in the FLSCU1 position (Ref. AMM TASK 28-46-34-400-001).
(5) Do the BITE test (Ref. AMM TASK 28-46-00-740-001). Make sure that the test result is good.
(6) Remove the FLSCU3 from the FLSCU1 position (Ref. AMM TASK 28-46-34-000-001).
(7) Install the FLSCU1 and the FLSCU3 in their initial positions (Ref. AMM TASK 28-46-34-400-001).
Subtask 28-46-00-740-055-A ** ON A/C NOT FOR ALL (1) Do the BITE test of the FLSCU1 (7QJ) and the FLSCU2 (9QJ) (Ref. AMM TASK 28-46-00-740-001). Make sure that the test result is good.
NOTE: The FLSS BITE test is only done on the FLSCUs installed in the FLSCU1 and the FLSCU2 positions. There is no FLSS BITE test function done to the FLSCU installed in the FLSCU3 position.
(2) Remove and retain the FLSCU1 (Ref. AMM TASK 28-46-34-000-001). (3) Remove the FLSCU3 (Ref. AMM TASK 28-46-34-000-001).
(4) Install the FLSCU initially installed in the FLSCU3 position in the FLSCU1 position (Ref. AMM TASK 28-46-34-400-001).
(5) Do the BITE test (Ref. AMM TASK 28-46-00-740-001). Make sure that the test result is good.
(6) Remove the FLSCU3 from the FLSCU1 position (Ref. AMM TASK 28-46-34-000-001).
(7) Install the FLSCU1 and the FLSCU3 in their initial positions (Ref. AMM TASK 28-46-34-400-001).
B. Manual Test of the High Level Sensors of 65QT1(65QT2) and 66QT1(66QT2)
(1) Do this test:
Subtask 28-46-00-710-056-A ** ON A/C NOT FOR ALL (1) Do this test:
| ACTION | RESULT |
|---|---|
On the panel 800VU:
| On the panel 800VU and 801VU:
|
| | On the preselector 5QT:
|
| | On the indicator 6QT:
|
| On the panel 800VU and 801VU:
NOTE: If the ACT1 contains more than approximately 2349 kg (5179 lb), the ACT1 HI LVL light will be on. If the ACT2 is installed and contains more than approximately 2349 kg (5179 lb), the ACT2 HI LVL light will be on. This is a full indication as the high level sensors are wet. |
| | On the preselector 5QT:
|
| | On the indicator 6QT:
NOTE: The correct indication of high level sensor states may not show for 60 seconds after you switch the power on. This can occur at extreme conditions of temperature and battery voltage. |
| On the panel 800VU and 801VU:
|
| On the panel 800VU and 801VU:
|
C. Functional Test of the Low Level Sensors of 65QT1 and 66QT1
(1) Make sure that the ACT1 contains more than 250 kg (551 lb) of fuel. Refuel the ACT1 if necessary (Ref. AMM TASK 12-11-28-650-003).
(3) With a MULTIMETER - STANDARD at the free connector 4065VC-A, do a resistance test between the pins <A and <B and a resistance test between pin <D and a ground point. The result must be open circuit for both tests.
(6) Connect the free connector 4065VC-A to the Relay Panel (802VU).
Subtask 28-46-00-710-061-A ** ON A/C NOT FOR ALL (1) Make sure that the ACT1 contains more than 250 kg (551 lb) of fuel. Refuel the ACT1 if necessary (Ref. AMM TASK 12-11-28-650-003).
NOTE: This is to make sure that the low level sensors are wet.
(2) Disconnect the free connector 4065VC-A from the Relay Panel (802VU). (3) With a MULTIMETER - STANDARD at the free connector 4065VC-A, do a resistance test between the pins <A and <B and a resistance test between pin <D and a ground point. The result must be open circuit for both tests.
NOTE: The tests are related to the low level sensors as follows:
(4) Defuel the ACT1 (Ref. AMM TASK 28-25-00-869-001). - between pin <D and ground is for 65QT1 (FLSCU3 channel LS1)
- between pins <A and <B is for 66QT1 (FLSCU3 channel LS5).
NOTE: This is to make sure that the low level sensors are dry.
(5) With a multimeter at the free connector 4065VC-A, do a resistance test between the pins <A and <B and a resistance test between pin <D and a ground point. The result must be a low resistance for both tests. (6) Connect the free connector 4065VC-A to the Relay Panel (802VU).
D. Functional Test of the Low Level Sensors of 65QT2 and 66QT2
(1) Make sure that the ACT2 contains more than 250 kg (551 lb) of fuel. Refuel the ACT2 if necessary (Ref. AMM TASK 12-11-28-650-003).
(3) With a MULTIMETER - STANDARD at the free connector 4065VC-A, do a resistance test between these positions:
5. Close-up(1) Make sure that the ACT2 contains more than 250 kg (551 lb) of fuel. Refuel the ACT2 if necessary (Ref. AMM TASK 12-11-28-650-003).
NOTE: This is to make sure that the low level sensors are wet.
(2) Disconnect the free connector 4065VC-A from the Relay Panel (802VU). (3) With a MULTIMETER - STANDARD at the free connector 4065VC-A, do a resistance test between these positions:
- pins B and D
- pin C and a ground point.
The result must be open circuit for both tests.
NOTE: The tests are related to the low level sensors as follows:
(4) Defuel the ACT2 (Ref. AMM TASK 28-25-00-869-001). - between pin C and ground is for 65QT2 (FLSCU3 channel LS8)
- between pins B and D is for 66QT2 (FLSCU3 channel LS2).
NOTE: This is to make sure that the low level sensors are dry.
(5) With a MULTIMETER - STANDARD at the free connector 4065VC-A, do a resistance test between these positions: - pins B and D
- pin C and a ground point.
The result must be a low resistance for both tests.
Subtask 28-46-00-410-055-A ** ON A/C NOT FOR ALL
A. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Close the access doors 811 and 192MB.
Subtask 28-46-00-860-058-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 the access doors 811 and 192MB.
B. Aircraft Maintenance Configuration
(1) If the aircraft is refueled with the battery power, on the refuel/defuel control panel (800VU):
(a) Do the EIS stop procedure
(Ref. AMM TASK 31-60-00-860-002).
(b) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
Subtask 28-46-00-942-057-A ** ON A/C NOT FOR ALL (1) If the aircraft is refueled with the battery power, on the refuel/defuel control panel (800VU):
- put the BATT POWER switch to the NORM position.
(a) Do the EIS stop procedure
(Ref. AMM TASK 31-60-00-860-002).
(b) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
C. Removal of Equipment
(1) Remove the access platform(s).
(2) Remove the safety barriers.
(3) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
(1) Remove the access platform(s).
(2) Remove the safety barriers.
(3) Remove the ground support and maintenance equipment, the special and standard tools and all other items.