Installation of the Fuel Quantity-Indicating Computer (FQIC)
TASK 28-42-34-400-001-A
Installation of the Fuel Quantity-Indicating Computer (FQIC)
1. Reason for the Job
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 28-42-34-860-050-A
Subtask 28-42-34-420-050-A
Subtask 28-42-34-410-050-A
[Rev.10 from 2021]
2026.04.02 06:46:01 UTC
Installation of the Fuel Quantity-Indicating Computer (FQIC)
1. Reason for the Job
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)- ADJUSTABLE |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 122 | AVIONICS COMPARTMENT |
| 811 |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 24-42-00-861-001-A | Energize the Ground Service Network from the External Power |
| TASK 24-42-00-862-001-A | De-energize the Ground Service Network Supplied from the External Power |
| TASK 28-42-00-740-001-A | Status Report (BITE) |
| TASK 28-46-00-740-001-A | Functional (BITE) Test |
| TASK 32-69-00-860-001-A | Simulation of Flight (With Aircraft on Ground) |
Subtask 28-42-34-860-050-A
A. Aircraft Maintenance Configuration
(1) Make sure that the ground service network is energized
(Ref. AMM TASK 24-42-00-861-001).
(2) Make sure that the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE is in position at the access door 811.
(3) Make sure that the access door 811 is open.
Subtask 28-42-34-865-051-A (1) Make sure that the ground service network is energized
(Ref. AMM TASK 24-42-00-861-001).
(2) Make sure that the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE is in position at the access door 811.
(3) Make sure that the access door 811 is open.
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
4. Procedure| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C ALL | |||
| 49VU | FUEL/FQI/CHAN/1 | 1QT | A13 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | FUEL/FQI/CHANNEL/1 AND 2 | 8QT | L26 |
| ** ON A/C ALL | |||
| 121VU | FUEL/FQI/CHAN/2 | 2QT | M27 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | FUEL/FQI/CHANNEL/1 AND 2 | 8QT | L25 |
Subtask 28-42-34-420-050-A
A. Installation of the FQIC (3QT)
(1) Remove the CAP-BLANKING from each electrical connector and receptacle.
(2) Install the FQIC (4) in its rack (2).
(3) Connect the FQIC (4) to the electrical connector (1).
(4) Attach the FQIC (4) to its rack (2) with the knurled nuts (3).
Subtask 28-42-34-865-052-A (1) Remove the CAP-BLANKING from each electrical connector and receptacle.
(2) Install the FQIC (4) in its rack (2).
(3) Connect the FQIC (4) to the electrical connector (1).
(4) Attach the FQIC (4) to its rack (2) with the knurled nuts (3).
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 28-42-34-740-050-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C ALL | |||
| 49VU | FUEL/FQI/CHAN/1 | 1QT | A13 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | FUEL/FQI/CHANNEL/1 AND 2 | 8QT | L26 |
| ** ON A/C ALL | |||
| 121VU | FUEL/FQI/CHAN/2 | 2QT | M27 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | FUEL/FQI/CHANNEL/1 AND 2 | 8QT | L25 |
C. BITE test
(1) Do a BITE test of the FQIC (3QT) (Ref. AMM TASK 28-42-00-740-001) and (Ref. AMM TASK 28-46-00-740-001):
(a) If the fault messages "NO DATA FROM ADIRU 1(2)" and/or "NO DATA FROM CFDIU" are shown on the LAST LEG REPORT page, ignore them. To clear these fault messages, do a simulation of flight, with the aircraft on the ground (Ref. AMM TASK 32-69-00-860-001) two times:
1 On the MCDU, on the landing gear page, it is necessary to push the line key adjacent to the UPLOCKED indication (not the EXTENDED indication).
5. Close-up(1) Do a BITE test of the FQIC (3QT) (Ref. AMM TASK 28-42-00-740-001) and (Ref. AMM TASK 28-46-00-740-001):
(a) If the fault messages "NO DATA FROM ADIRU 1(2)" and/or "NO DATA FROM CFDIU" are shown on the LAST LEG REPORT page, ignore them. To clear these fault messages, do a simulation of flight, with the aircraft on the ground (Ref. AMM TASK 32-69-00-860-001) two times:
1 On the MCDU, on the landing gear page, it is necessary to push the line key adjacent to the UPLOCKED indication (not the EXTENDED indication).
Subtask 28-42-34-410-050-A
A. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Close the access door 811.
(3) Remove the access platform(s).
Subtask 28-42-34-862-050-A (1) Make sure that the work area is clean and clear of tools and other items.
(2) Close the access door 811.
(3) Remove the access platform(s).
Fuel Quantity-Indicating Computer (FQIC)