W DOC AIRBUS | AMM A320F

Installation of the Vent Outlet of the Vacuum Vent Line


TASK 38-31-65-400-802-A
Installation of the Vent Outlet of the Vacuum Vent Line


WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
WARNING: DO NOT DO WORK ON THE TOILET WASTE SYSTEM AND THE POTABLE WATER SYSTEM AT THE SAME TIME. THIS WILL PREVENT CONTAMINATION OF THE POTABLE WATER SYSTEM. SUCH CONTAMINATION CAN BE DANGEROUS TO HEALTH.
WARNING: ALWAYS USE RUBBER GLOVES WHEN YOU DO WORK:
  • ON THE TOILET WASTE SYSTEM, OR
  • ON PARTS THAT HAVE CONTAMINATION FROM THE WASTE SYSTEM.
WHEN YOU COMPLETE THE WORK PROCEDURE, CLEAN YOUR HANDS WITH SOAP AND WATER. THIS WILL PREVENT INFECTION (TOILET WASTE IS DANGEROUS FOR HEALTH).
ZONE: 170
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 1M(3 FT)
No specific
1
ACCESS PLATFORM 2M (6 FT)
No specific
1
BAG - PLASTIC
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.06AAB1)
Polysulfide Sealant-General Purpose Fillet -
(Material No.06AAC1)
Polysulfide Sealant-General Purpose Interfay -
(Material No.06AEA1)
Polysulfide Sealant-Low Adhesion Brushable -
(Material No.06LCG9)
Non Hardening Jointing Putty-Medium Temp. Area - -
(Material No.06LDG2)
Non Hardening Jointing Putty-High Temp. Area - Structure
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
170
AFT CAB U/FLOOR COMPT AFT BHD OF BULK
161DW, 162DW, 826
 D. Referenced Information
REFERENCE
DESIGNATION
TASK 20-28-00-912-802-A
Electrical Bonding - General Maintenance Procedure
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 25-55-12-000-001-A
Removal of the Aft Cargo-Compartment Partition at FR65
TASK 25-55-12-400-001-A
Installation of the Aft Cargo-Compartment Partition at FR65
TASK 38-31-00-710-009-A
Operational Test of the Toilet Unit
TASK 52-30-00-860-001-A
Open the FWD or Aft Cargo-Compartment Door with the Yellow Electric Pump
TASK 52-30-00-860-002-A
Close the FWD or Aft Cargo-Compartment Door with the Yellow Electric Pump
3. Job Set-up
Subtask 38-31-65-860-051-A
A. Aircraft Maintenance Configuration
   (1) Make sure that the aircraft electrical circuits are energized (Ref. AMM TASK 24-41-00-861-002).
   (2) Make sure that the ACCESS PLATFORM 1M(3 FT) is in position below the vacuum-vent line outlet.
   (3) Make sure that the ACCESS PLATFORM 2M (6 FT) is in position at aft cargo-compartment door 826.
   (4) Make sure that aft cargo-compartment door 826 is open (Ref. AMM TASK 52-30-00-860-001).
   (5) Make sure that access panels 161DW and 162DW are removed (Ref. AMM TASK 25-55-12-000-001).
Subtask 38-31-65-865-064-A
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
2001VUVACU TOIL SYS-VACUUM-SYS35MGA06
** ON A/C NOT FOR ALL
2001VUVACU TOIL SYS-VACUUM-GEN33MGA08
** ON A/C NOT FOR ALL
2001VUVACU TOIL SYS-LAV PWR-E34MGA04
** ON A/C NOT FOR ALL
2001VUVACU TOIL SYS-LAV PWR-D39MGA03
** ON A/C ALL
2001VUVACU TOIL SYS-LAV PWR-A32MGA01
** ON A/C NOT FOR ALL
2001VUVACU TOIL SYS-VACU-SYS35MGA06
** ON A/C NOT FOR ALL
2001VUVACU TOIL SYS-VACU-GEN33MGA08
** ON A/C NOT FOR ALL
2001VUVACU TOIL SYS-LAV PWR-G34MGA04
2001VUVACU TOIL SYS-LAV PWR-F39MGA03
2001VUVACU TOIL SYS-LAV PWR-D45MGA02
** ON A/C NOT FOR ALL
2001VUVACU TOIL SYS-LAV PWR-L45MGA02
** ON A/C NOT FOR ALL
2001VUVACU TOIL SYS-LAV PWR-L23MGA05
** ON A/C NOT FOR ALL
2001VUVACU TOIL SYS-LAV PWR-M34MGA04
4. Procedure
Subtask 38-31-65-420-051-A ** ON A/C NOT FOR ALL
A. Installation of the Vent Outlet
   (1) Remove the vent outlet (5) from the BAG - PLASTIC.
   (2) Clean the component interfaces and the adjacent area.
   (3) Remove the PLUG-BLANKING from each disconnected line end.
   (4) Make sure that the clamps (6) are in position on the vacuum vent line (8).
   (5) Put the vent outlet (5) in its installation position and connect it to the vacuum vent line (8).
   (6) Install the vent outlet (5) with the screws (4).
   (7) Apply Non Hardening Jointing Putty-Medium Temp. Area - - (Material No.06LCG9) to the screws (4).
   (8) Tighten the clamps (6).
   (9) Install the bonding lead (7) with the washer (3), the screw (2) and the nut (1) (Ref. AMM TASK 20-28-00-912-802).
   (10) Apply Polysulfide Sealant-Low Adhesion Brushable - (Material No.06AEA1) to:
  • The vent outlet base-plate and inner structure
  • The gap between the skin and the base plate.
Subtask 38-31-65-420-051-B ** ON A/C NOT FOR ALL
A. Installation of the Vent Outlet
   (1) Remove the vent outlet (5) from the BAG - PLASTIC.
   (2) Clean the component interfaces and the adjacent area.
   (3) Remove the PLUG-BLANKING from each disconnected line end.
   (4) Make sure that the clamps (6) are in position on the vacuum vent line (8).
   (5) Put the vent outlet (5) in its installation position and connect it to the vacuum vent line (8).
   (6) Install the vent outlet (5) with the new screws (4).
   (7) Apply Non Hardening Jointing Putty-High Temp. Area - Structure (Material No.06LDG2) to the screws (4).
   (8) Tighten the clamps (6).
   (9) Install the bonding lead (7) with the new washer (3), new screw (2) and new nut (1) (Ref. AMM TASK 20-28-00-912-802).
   (10) Apply Non Hardening Jointing Putty-Medium Temp. Area - - (Material No.06LCG9) to the vent outlet base, nut plates and the screws (4).
   (11) Apply Polysulfide Sealant-General Purpose Interfay - (Material No.06AAC1) to the vent outlet base-plate and inner structure.
   (12) Apply Polysulfide Sealant-General Purpose Fillet - (Material No.06AAB1) to the gap between the skin and the base plate.
Subtask 38-31-65-865-065-A
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
2001VUVACU TOIL SYS-VACUUM-SYS35MGA06
** ON A/C NOT FOR ALL
2001VUVACU TOIL SYS-VACUUM-GEN33MGA08
** ON A/C NOT FOR ALL
2001VUVACU TOIL SYS-LAV PWR-E34MGA04
** ON A/C NOT FOR ALL
2001VUVACU TOIL SYS-LAV PWR-D39MGA03
** ON A/C ALL
2001VUVACU TOIL SYS-LAV PWR-A32MGA01
** ON A/C NOT FOR ALL
2001VUVACU TOIL SYS-VACU-SYS35MGA06
** ON A/C NOT FOR ALL
2001VUVACU TOIL SYS-VACU-GEN33MGA08
** ON A/C NOT FOR ALL
2001VUVACU TOIL SYS-LAV PWR-G34MGA04
2001VUVACU TOIL SYS-LAV PWR-F39MGA03
2001VUVACU TOIL SYS-LAV PWR-D45MGA02
** ON A/C NOT FOR ALL
2001VUVACU TOIL SYS-LAV PWR-L45MGA02
** ON A/C NOT FOR ALL
2001VUVACU TOIL SYS-LAV PWR-L23MGA05
** ON A/C NOT FOR ALL
2001VUVACU TOIL SYS-LAV PWR-M34MGA04
Subtask 38-31-65-710-051-A
C. Operational Test of the Toilet Unit
   (1) Operate the toilet and make sure that it flushes correctly (Ref. AMM TASK 38-31-00-710-009).
5. Close-up
Subtask 38-31-65-410-051-A
A. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Install access panels 161DW and 162DW (Ref. AMM TASK 25-55-12-400-001).
   (3) Close aft cargo-compartment door 826 (Ref. AMM TASK 52-30-00-860-002).
   (4) Remove the access platform(s).
Subtask 38-31-65-862-051-A
B. De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
[Rev.10 from 2021] 2026.04.01 01:20:51 UTC