W DOC AIRBUS | AMM A320F

Installation of the Fuel Quantity-Indicating Computer (FQIC) On Board Removable Memory


TASK 28-42-34-400-002-A
Installation of the Fuel Quantity-Indicating Computer (FQIC) On Board Removable Memory


FIN: 3QT ** ON A/C NOT FOR ALL
1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
1
ACCESS PLATFORM 2M (6 FT)
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
811
 C. Referenced Information
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)
3. Job Set-up
Subtask 28-42-34-860-051-A ** ON A/C NOT FOR ALL
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 2M (6 FT) is in position at the access door 811.
   (3) Make sure that the access door 811 is open.
Subtask 28-42-34-865-054-A ** ON A/C NOT FOR ALL
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUFUEL/FQI/CHAN/11QTA13
** ON A/C NOT FOR ALL
121VUFUEL/FQI/CHANNEL/1 AND 28QTL26
** ON A/C NOT FOR ALL
121VUFUEL/FQI/CHAN/22QTM27
** ON A/C NOT FOR ALL
121VUFUEL/FQI/CHANNEL/1 AND 28QTL25
4. Procedure
Subtask 28-42-34-420-051-A ** ON A/C NOT FOR ALL
A. Installation of the FQIC OBRM (3QT1)
NOTE: If the standard of the OBRM has changed, refer to SB A320-28-1046.
   (1) Install the OBRM module (7).
   (2) Tighten the screws (6) on the front of the FQIC (3QT).
Subtask 28-42-34-420-052-A ** ON A/C NOT FOR ALL
B. 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 28-42-34-865-056-A ** ON A/C NOT FOR ALL
C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUFUEL/FQI/CHAN/11QTA13
** ON A/C NOT FOR ALL
121VUFUEL/FQI/CHANNEL/1 AND 28QTL26
** ON A/C NOT FOR ALL
121VUFUEL/FQI/CHAN/22QTM27
** ON A/C NOT FOR ALL
121VUFUEL/FQI/CHANNEL/1 AND 28QTL25
Subtask 28-42-34-740-051-A ** ON A/C NOT FOR ALL
D. 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) Supply electrical power to the FQIC for a minimum period of one minute.
     (b) 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
Subtask 28-42-34-410-051-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 door 811.
   (3) Remove the access platform(s).
Subtask 28-42-34-862-051-A ** ON A/C NOT FOR ALL
B. De-energize the ground service network (Ref. AMM TASK 24-42-00-862-001).
[Rev.10 from 2021] 2026.04.02 06:18:09 UTC