W DOC AIRBUS | AMM A320F

Installation of the Center (Transfer) Tank Fuel-Quantity Probe


TASK 28-42-15-400-004-A
Installation of the Center (Transfer) Tank Fuel-Quantity Probe


WARNING: THIS PROCEDURE USES A FUEL SYSTEM ITEM THAT IS IN A CATEGORY KNOWN AS A CRITICAL DESIGN CONFIGURATION CONTROL LIMITATION (CDCCL). CDCCL IDENTIFIES AN ITEM THAT CAN BE THE SOURCE OF A POSSIBLE FUEL TANK IGNITION. YOU MUST KEEP ALL CDCCL ITEMS IN THE APPROVED CONFIGURATION. DAMAGE, WEAR OR CHANGES TO A CDCCL ITEM CAN CAUSE A POSSIBLE FUEL TANK EXPLOSION.
WARNING: MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING NOTICES ARE IN POSITION.
WARNING: MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING GEAR. THIS WILL PREVENT UNWANTED MOVEMENT OF THE LANDING GEAR, AND THUS POSSIBLE INJURY TO PERSONS AND DAMAGE TO THE AIRCRAFT AND/OR EQUIPMENT.
WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
FIN: 35QT ** ON A/C NOT FOR ALL
FIN: 36QT ** ON A/C NOT FOR ALL
FIN: 37QT ** ON A/C NOT FOR ALL
FIN: 38QT ** ON A/C NOT FOR ALL
FIN: 51QT ** 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
AR
SAFETY BARRIER(S)
No specific
Torque wrench: range to between .045 and .023 m.daN (3.98 and 2.04 lbf.in ) T
No specific
Torque wrench: range to between .124 and .102 m.daN (10.97 and 9.03 lbf.in ) T
No specific
Torque wrench: range to between .226 and .203 m.daN (20.00 and 17.96 lbf.in ) T
No specific
Torque wrench: range to between .362 and .316 m.daN (32.04 and 27.96 lbf.in ) T
No specific
Torque wrench: range to between 0.48 and 0.37 m.daN (42.48 and 32.74 lbf.in ) T
No specific
Torque wrench: range to between .56 and .45 m.daN (49.56 and 39.82 lbf.in ) T
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.06ABB1)
Polysulfide Sealant-Fuel Tank Fillet -
(Material No.06ABF1)
Polysulfide Sealant-Fuel Tank Quick Curing -
(Material No.08BAA9)
Non Aqueous Cleaner-General - -
(Material No.14SBA1)
Textile-Lint free Cotton -
 C. Expendable Parts
FIG.ITEM
DESIGNATION
IPC-CSN
1
TIE
AIPC 28-42-05-03-490
1
CABLE TIES
AIPC 28-42-05-04-020
1
CABLE TIES
AIPC 28-42-85-04-020
 D. Referenced Information
REFERENCE
DESIGNATION
TASK 12-11-28-650-003-A
Pressure Refuel with Automatic Control
TASK 20-28-00-912-802-A
Electrical Bonding - General Maintenance Procedure
TASK 28-10-00-910-001-A
Safety Procedures When You Do Work in a Fuel Tank
TASK 28-10-00-910-002-A
Access to the Fuel Tanks and the Work Areas
TASK 28-25-00-650-001-A
Pressure Defuel
TASK 28-25-00-650-003-A
To Drain Remaining Fuel from the Wing Tanks and the Center Tank
TASK 28-25-00-650-003-A-01
To Drain Remaining Fuel from the Wing Tanks and the Center Tank
TASK 28-25-00-869-001-A
Fuel Transfer
TASK 28-42-00-740-001-A
Status Report (BITE)
TASK 32-12-00-010-001-A
Open the Main Gear Doors for Access
TASK 32-12-00-410-001-A
Close the Main Gear Doors after Access
TASK 57-17-11-000-001-A
Removal of Access Cover 147AZ(148AZ)
TASK 57-17-11-000-001-B
Removal of Access Cover 148AZ or/and the ACT-Equipment Support Door
TASK 57-17-11-400-001-A
Installation of Access Cover 147AZ(148AZ)
TASK 57-17-11-400-001-B
Installation of Access Cover 148AZ or/and the ACT-Equipment Support-Door
3. Job Set-up
Subtask 28-42-15-941-064-A ** ON A/C NOT FOR ALL
A. Safety Precautions
WARNING: BEFORE YOU DO WORK IN OR NEAR A FUEL TANK, MAKE SURE THAT YOU OBEY ALL THE SAFETY PROCEDURES. THIS WILL PREVENT INJURY TO PERSONS AND/OR DAMAGE TO THE AIRCRAFT.
   (1) You must obey the fuel safety procedures (Ref. AMM TASK 28-10-00-910-001) when you do work in a fuel tank.
   (2) Make sure that the SAFETY BARRIER(S) are in position.
Subtask 28-42-15-860-053-A ** ON A/C NOT FOR ALL
B. Aircraft Maintenance Configuration
   (1) Make sure that the applicable fuel tank is defueled (Ref. AMM TASK 28-25-00-650-001).
   (2) Make sure that the remaining fuel has been drained from the applicable fuel tank (Ref. AMM TASK 28-25-00-650-003).
   (3) Make sure that the applicable MLG door(s) are open (Ref. AMM TASK 32-12-00-010-001).
   (4) Make sure that the 460005835 SLEEVE - GROUND LOCK is installed on the applicable MLG door actuator.
   (5) Make sure that the access platform is below the applicable access panel 147AZ (148AZ).
   (6) Make sure that the applicable access panel 147AZ (148AZ) is removed (Ref. AMM TASK 28-10-00-910-002), (Ref. AMM TASK 57-17-11-000-001).
Subtask 28-42-15-860-053-B ** ON A/C NOT FOR ALL
B. Aircraft Maintenance Configuration
   (1) Make sure that the applicable fuel tank is defueled (Ref. AMM TASK 28-25-00-650-001).
   (2) Make sure that the remaining fuel has been drained from the applicable fuel tank (Ref. AMM TASK 28-25-00-650-003).
   (3) Make sure that the applicable MLG door(s) are open (Ref. AMM TASK 32-12-00-010-001).
   (4) Make sure that the 460005835 SLEEVE - GROUND LOCK is installed on the applicable MLG door actuator.
   (5) Make sure that the access platform is below the applicable access panel 148AZ and/or the ACT Equipment Support Door.
   (6) Make sure that the applicable access panel 148AZ and/or the ACT Equipment Support Door is removed (Ref. AMM TASK 28-10-00-910-002), (Ref. AMM TASK 57-17-11-000-001).
Subtask 28-42-15-865-060-A ** ON A/C NOT FOR ALL
C. 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 28-42-15-420-060-A ** ON A/C NOT FOR ALL
A. Preparation for Installation
   (1) Clean the component interfaces and the adjacent areas with a Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) .
   (2) Do an inspection of the component interfaces and the adjacent area.
   (3) Make sure that the parts retained from the removed component are clean and in the correct condition.
Subtask 28-42-15-420-055-A ** ON A/C NOT FOR ALL
B. Installation of the Center (Transfer) Tank Fuel-Quantity-Probe
CAUTION: REFER TO THE MATCH MARKS MADE DURING THE REMOVAL WHEN YOU CONNECT THE ELECTRICAL WIRES. INCORRECT CONNECTION OF THE WIRES WILL CAUSE DAMAGE TO EQUIPMENT.
   (1) Install the bracket (11) on the probe (10).
   (2) Put the probe (10) in the correct position and loosely install the bolts (9) and (12).
   (3) Measure the clearance between the structure and the top and bottom of the probe (10).
WARNING: THIS INSTRUCTION IS APPLICABLE TO A CRITICAL DESIGN CONFIGURATION CONTROL LIMITATION (CDCCL) ITEM. CAREFULLY OBEY ALL GIVEN INSTRUCTIONS WHEN YOU DO THIS STEP. IF YOU DO NOT OBEY THESE INSTRUCTIONS, A DANGEROUS CONDITION CAN OCCUR THAT CAN CAUSE A POSSIBLE FUEL TANK EXPLOSION.
     (a) Make sure that the clearance is a minimum of 10.0 mm (0.3937 in.).
     (b) To prevent possible static discharge, make sure that the fuel probe is not less than 5.0 mm (0.1969 in.) from:
  • The nearest structure
  • Rib and tank wall
  • Pipework
  • Brackets and p-clips
  • Fasteners and other metal parts.
   (4) TORQUE the bolts (9) to between .56 and .45 m.daN (49.56 and 39.82 lbf.in ) T.
   (5) TORQUE the bolts (12) to between 0.48 and 0.37 m.daN (42.48 and 32.74 lbf.in )
T.
   (6) Do the electrical bonding (
Ref. AMM TASK 20-28-00-912-802).
   (7) Apply a Polysulfide Sealant-Fuel Tank Fillet - (Material No.06ABB1) or Polysulfide Sealant-Fuel Tank Quick Curing - (Material No.06ABF1) to the ends of the bolts (9) and (12).
   (8) Remove the CAP-BLANKING from each electrical connector and receptacle.
CAUTION: MAKE SURE THAT THE ELECTRICAL CONNECTORS ARE CLEAN BEFORE YOU DISCONNECT OR CONNECT THEM. CONTAMINATION ON THE ELECTRICAL CONNECTORS CAN CAUSE DAMAGE TO EQUIPMENT.
   (9) Identify and connect the electrical connectors of the cable (8) with the screws (3), (4) and (5).
   (10) TORQUE the screw (3) to between .124 and .102 m.daN (10.97 and 9.03 lbf.in ) T.
   (11) TORQUE the screw (4) to between .226 and .203 m.daN (20.00 and 17.96 lbf.in )
T.
   (12) TORQUE the screw (5) to between .362 and .316 m.daN (32.04 and 27.96 lbf.in )
T.
   (13) Put the cable (8) in position under the clamp block (6) and install the clamp screw (7).
   (14) TORQUE the clamp screw (7) to between .045 and .023 m.daN (3.98 and 2.04 lbf.in )
T.
   (15) Install the
AIPC 28-42-05-04-020 CABLE TIES (1) or AIPC 28-42-85-04-020 CABLE TIES (1) or AIPC 28-42-05-03-490 TIE (1), as necessary, to attach the cable (8) to the probe (10).
5. Close-up
Subtask 28-42-15-410-054-A ** ON A/C NOT FOR ALL
Subtask 28-42-15-410-054-B ** ON A/C NOT FOR ALL
A. Close Access
WARNING: MAKE SURE THAT THE TRAVEL RANGES OF THE LANDING GEAR DOORS ARE CLEAR.
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Install the applicable access panel 148AZ and/or the ACT Equipment Support Door (Ref. AMM TASK 57-17-11-400-001).
   (3) Remove the access platform(s).
   (4) Close the applicable MLG door(s) (Ref. AMM TASK 32-12-00-410-001).
Subtask 28-42-15-865-061-A ** ON A/C NOT FOR ALL
B. 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 28-42-15-740-053-A ** ON A/C NOT FOR ALL
C. Test
   (1) Do a status report (BITE) of the FQI system (Ref. AMM TASK 28-42-00-740-001).
Subtask 28-42-15-650-057-A ** ON A/C NOT FOR ALL
D. Fuel Configuration
   (1) Refuel, defuel or transfer fuel as necessary (Ref. AMM TASK 12-11-28-650-003), (Ref. AMM TASK 28-25-00-650-001) or (Ref. AMM TASK 28-25-00-869-001).
Subtask 28-42-15-942-053-A ** ON A/C NOT FOR ALL
E. Removal of Equipment
   (1) Remove the safety barriers.
   (2) Remove the WARNING NOTICE(S).
   (3) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
[Rev.10 from 2021] 2026.04.02 06:18:07 UTC