Functional (BITE) Test
TASK 28-46-00-740-001-A
Functional (BITE) Test
Self explanatory
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 28-46-00-941-056-A
Subtask 28-46-00-740-051-F ** ON A/C NOT FOR ALL
Subtask 28-46-00-410-053-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.02 06:18:15 UTC
Functional (BITE) Test
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.
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | ACCESS PLATFORM 3M (10 FT) |
| No specific | AR | SAFETY BARRIER(S) |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 622KB | |
| 192MB |
| 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 31-32-00-860-001-A | Procedure to Get Access to the SYSTEM REPORT/TEST Menu Page |
Subtask 28-46-00-941-056-A
A. Safety Precautions
(2) Put the SAFETY BARRIER(S) in position.
Subtask 28-46-00-860-050-A 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) Put the SAFETY BARRIER(S) in position.
B. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
Subtask 28-46-00-010-055-C ** ON A/C NOT FOR ALL (1) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
C. Get Access
(1) If it is necessary to do a test of the high-level sensors 17QJ1(17QJ2), 20QJ and the dummy load sensor 6QJ:
Subtask 28-46-00-010-055-E ** ON A/C NOT FOR ALL (1) If it is necessary to do a test of the high-level sensors 17QJ1(17QJ2), 20QJ and the dummy load sensor 6QJ:
- put the ACCESS PLATFORM 3M (10 FT) below zone 622
- open the access door 622KB to energize the refuel/defuel control panel.
NOTE: If operating in battery power, do not keep the door open longer than necessary because the battery can discharge.
C. Get Access
(1) If it is necessary to do a test of the high-level sensors 17QJ1(17QJ2), 20QJ and the dummy load sensor 6QJ:
Subtask 28-46-00-650-053-A (1) If it is necessary to do a test of the high-level sensors 17QJ1(17QJ2), 20QJ and the dummy load sensor 6QJ:
- open the access door 192MB to energize the refuel/defuel control panel.
NOTE: If operating in battery power, do not keep the door open longer than necessary because the battery can discharge.
D. Fuel Configuration
(1) If it is necessary to test the center tank low-level sensors 21QJ and 22QJ, refuel the center tank to a minimum 650 kg (1440 lb) (Ref. AMM TASK 12-11-28-650-003).
4. Procedure(1) If it is necessary to test the center tank low-level sensors 21QJ and 22QJ, refuel the center tank to a minimum 650 kg (1440 lb) (Ref. AMM TASK 12-11-28-650-003).
Subtask 28-46-00-740-051-F ** ON A/C NOT FOR ALL
A. BITE Test
(1) Do this test:
EQUW CH1 FUEL FLSS STATUS
Subtask 28-46-00-740-051-G ** ON A/C NOT FOR ALL (1) Do this test:
NOTE: The subsequent results are only available after two minutes from the time that you energized the Fuel Quantity Indication Computer (FQIC).
| ACTION | RESULT |
|---|---|
| 1.On the MCDU, get access to the FUEL page (Ref. AMM TASK 31-32-00-860-001). |
|
| 2.Push (in) the line key adjacent to <COMMAND FLSS BITE indication. |
|
| 3.Push (in) the line key adjacent to <RETURN indication. |
|
| 4.Push (in) the line key <RETURN frequently until the CFDS menu page is shown. | |
| ------------------------------------------------------------------------------- |
| ! LFT CTR RHT ! |
| ! SURGE P - P ! |
| ! HI LEVEL P P* P* ! |
| ! LO LEVEL 1 F P* F ! |
| ! LO LEVEL 2 P* - P ! |
| ! LOGIC P - P ! |
| ! U/FULL A P* - P* ! |
| ! U/FULL B&C P - P ! |
| ! * = PREVIOUS RESULTS ! |
| !-----------------------------------------------------------------------------! |
| ! Table 1 ! |
| ! FLSS COMMAND BITE Results Displayed on MCDU ! |
| ------------------------------------------------------------------------------- |
NOTE: The letter P indicates that all sensors in that group are serviceable.
NOTE: The letter F indicates that one or more sensor(s) in that group are unserviceable.
NOTE: Where an asterisk (*) is shown, the results from the last related BITE test are given.
NOTE: The FLSS COMMAND BITE indication shown in Table 1 are for example only.
A. BITE Test
(1) Do this test:
Subtask 28-46-00-740-051-H ** ON A/C NOT FOR ALL (1) Do this test:
NOTE: When you push (in) the line key adjacent to FUEL> indication, the Multipurpose Control and Display Unit (MCDU) can initially show CH1 or CH2. In this case, the test starts with CH1. CH2 will only show first if CH1 has a failure.
NOTE: The subsequent results are only available after two minutes from the time that you energized the Fuel Quantity Indication Computer (FQIC).
| ACTION | RESULT |
|---|---|
| 1.On the MCDU, get access to the FUEL page (Ref. AMM TASK 31-32-00-860-001). |
|
| 2.Push (in) the NEXT PAGE button on the MCDU. |
|
| 3.Push (in) the line key adjacent to <COMMAND FLSS BITE indication. |
|
| 4.Push (in) the line key adjacent to <RETURN indication. |
|
| 5.Push (in) the NEXT PAGE button on the MCDU. |
|
| 6.Push (in) the line key adjacent to <SELECT CHANNEL 2 indication. |
|
| 7.Push (in) the NEXT PAGE button on the MCDU. |
|
| 8.Push (in) the line key adjacent to <COMMAND FLSS BITE indication. |
|
| 9.Push (in) the line key <RETURN frequently until the CFDS menu page is shown. | |
A. BITE Test
(1) Do this test:
5. Close-up(1) Do this test:
NOTE: When you push (in) the line key adjacent to FUEL> indication, the Multipurpose Control and Display Unit (MCDU) can initially show CH1 or CH2. In this case, the test starts with CH1. CH2 will only show first if CH1 has a failure.
NOTE: The subsequent results are only available after two minutes from the time when you energized the Fuel Quantity Indication Computer (FQIC).
| ACTION | RESULT |
|---|---|
| 1.On the MCDU, get access to the FUEL page (Ref. AMM TASK 31-32-00-860-001). |
|
| 2.Push (in) the line key adjacent to <COMMAND FLSS BITE indication. |
If FQIC channel 1 is not available, the MCDU shows the message FLSCU 1 TEST NOT AVAILABLE. NOTE: For FQIC channel 2, the message is FLSCU 2 TEST NOT AVAILABLE. If there is(are) fault(s), the MCDU shows the defective LRU with the parameters that follow:
|
| 3.Push (in) the line key <RETURN frequently until the CFDS menu page is shown. | |
Subtask 28-46-00-410-053-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) If necessary, close the access door 192MB.
Subtask 28-46-00-410-053-B ** ON A/C NOT FOR ALL (1) Make sure that the work area is clean and clear of tools and other items.
(2) If necessary, close the access door 192MB.
A. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) If necessary, close the access door 622KB.
Subtask 28-46-00-860-056-A (1) Make sure that the work area is clean and clear of tools and other items.
(2) If necessary, close the access door 622KB.
B. Aircraft Maintenance Configuration
(1) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
Subtask 28-46-00-942-053-A (1) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
C. Removal of Equipment
(1) 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) 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.