DOC AIRBUS | AMM A320FInstallation of the Oil Transfer Tubes (APS 3200)
TASK 49-21-00-400-001-A
Installation of the Oil Transfer Tubes (APS 3200)
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Consumable Materials
C. Work Zones and Access Panels
D. Referenced Information
3. Job Set-up
Subtask 49-21-00-860-055-A ** ON A/C NOT FOR ALL
Subtask 49-21-00-420-055-A ** ON A/C NOT FOR ALL
Subtask 49-21-00-410-055-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.01 01:28:52 UTC
Installation of the Oil Transfer Tubes (APS 3200)
WARNING:
LOCK THE MECHANISM OF THE ACCESS DOOR 316AR WITH THE PIP PIN WHEN YOU OPEN THE ACCESS DOOR. THIS WILL PREVENT INJURY.
WARNING:
BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
CAUTION:
DO NOT APPLY MORE THAN THE SPECIFIED TORQUE. IF YOU DO, YOU CAN CAUSE DAMAGE TO THE TUBES.
1. Reason for the JobSelf explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | SAFETY CLIP - CIRCUIT BREAKER |
| No specific | Torque wrench: range to between 16.5 and 13.5 lbf.ft (2.24 and 1.83 m.daN )  | |
| No specific | Torque wrench: range to between 2.3 and 1.89 m.daN (16.96 and 13.94 lbf.ft ) | |
| 98L12003001000 | AR | HARNESS,SAFETY |
| REFERENCE | DESIGNATION |
|---|---|
| (Material No.03LBB1) | Grease-Thread Anti-seize Graphited and Petrolatum - |
| (Material No.03PGG6) | Lubricant-General Assembly - Turbine Engine |
| (Material No.08BPA1) | Non Aqueous Cleaner-Non structural use - - |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 315 | TAIL CONE APU AND ACCESSORY COMPARTMENT |
| 316 | TAIL CONE APU AND ACCESSORY COMPARTMENT |
| 315AL, 316AR |
| REFERENCE | DESIGNATION |
|---|---|
| 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 29-00-00-864-001-A | Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action |
| TASK 29-14-00-614-002-A | Pressurization of the Hydraulic Reservoirs through the Ground Connector |
| TASK 29-14-00-614-002-A-01 | Pressurization of the Hydraulic Reservoirs with the Auxiliary Power Unit (APU) |
| TASK 49-00-00-790-002-A | Leak Test of the APU |
| TASK 52-41-00-010-001-A | Open the APU Doors for Access |
| TASK 52-41-00-410-001-A | Close the APU Doors after Access |
Oil Transfer Tube 6 o'clock (APS 3200)Subtask 49-21-00-860-055-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
(1) Make sure that the aircraft electrical circuits are energized
(Ref. AMM TASK 24-41-00-861-002).
(2) On overhead panel 25VU, make sure that the APU MASTER SW pushbutton switch is released (ON legend is off).
(3) Make sure that the WARNING NOTICE(S) are on the APU section of overhead panel 25VU to tell persons not to start the APU.
(4) Make sure that the hydraulic systems are depressurized
(Ref. AMM TASK 29-00-00-864-001).
Subtask 49-21-00-865-051-A ** ON A/C NOT FOR ALL (1) Make sure that the aircraft electrical circuits are energized
(Ref. AMM TASK 24-41-00-861-002).
(2) On overhead panel 25VU, make sure that the APU MASTER SW pushbutton switch is released (ON legend is off).
(3) Make sure that the WARNING NOTICE(S) are on the APU section of overhead panel 25VU to tell persons not to start the APU.
(4) Make sure that the hydraulic systems are depressurized
(Ref. AMM TASK 29-00-00-864-001).
B. Open, safety and tag this(these) circuit breaker(s):
Subtask 49-21-00-010-056-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 121VU | APU/APU/CTL | 2KD | L42 |
| 121VU | APU/ECB/SPLY | 1KD | L41 |
C. Get Access
(2) Make sure that the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE is in position below the APU compartment.
(3) Make sure that APU access doors 316AR and 315AL are open (Ref. AMM TASK 52-41-00-010-001).
(4) Make sure that the light switch 11LJ is in the ON position.
4. ProcedureWARNING:
BEFORE YOU START WORK, YOU MUST PUT ON A SAFETY HARNESS AND ATTACH IT TO THE ACCESS PLATFORM. WITHOUT A SAFETY HARNESS, YOU CAN FALL. THIS CAN KILL YOU OR CAUSE YOU INJURY.
(1) Put on and attach the HARNESS, SAFETY before you start work in the work area.(2) Make sure that the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE is in position below the APU compartment.
(3) Make sure that APU access doors 316AR and 315AL are open (Ref. AMM TASK 52-41-00-010-001).
(4) Make sure that the light switch 11LJ is in the ON position.
Subtask 49-21-00-420-055-A ** ON A/C NOT FOR ALL
A. Installation of the Oil Transfer Tube
(2) Apply a small amount of Lubricant-General Assembly - Turbine Engine (Material No.03PGG6) fluid to the end of the oil transfer tube (2).
(4) Apply Grease-Thread Anti-seize Graphited and Petrolatum - (Material No.03LBB1) to the threads of the oil transfer tube (2).
.
.
(8) Clean the oil transfer tube (2) and oil line (4) with a Non Aqueous Cleaner-Non structural use - - (Material No.08BPA1) .
(9) Clean the APU compartment and remove presence of oil inside the compartment with cleaning solvent.
Subtask 49-21-00-865-052-A ** ON A/C NOT FOR ALL NOTE: This installation procedure is applicable to the oil scavenge transfer-tube (6 o'clock position), oil supply transfer-tube (11 o'clock position) and oil vent transfer-tube (1 o'clock position).
(1) Clean the end of the oil transfer tube (2). (2) Apply a small amount of Lubricant-General Assembly - Turbine Engine (Material No.03PGG6) fluid to the end of the oil transfer tube (2).
NOTE: The assembly fluid will help retain the copper seal (1) during installation of the oil transfer tube (2).
(3) Install the copper seal (1) onto the end of the oil transfer tube (2). (4) Apply Grease-Thread Anti-seize Graphited and Petrolatum - (Material No.03LBB1) to the threads of the oil transfer tube (2).
NOTE: Do not allow the Anti-Seize Grease to migrate into the inner diameter of the oil transfer tube (2).
(5) Install the oil transfer tube (2). CAUTION:
USE A COUNTER TORQUE WRENCH TO HOLD THE OIL TRANSFER TUBE WHILE CONNECTING THE NUT ON THE OIL SCAVENGE LINE.
(6) TORQUE the oil transfer tube (2) to between 2.3 and 1.89 m.daN (16.96 and 13.94 lbf.ft ) . NOTE: When tightening the B-nut (3) on the oil line (4) that attaches to the oil transfer tube (2), it is important that 2 wrenches be used to minimize the movement of the oil transfer tube (2) to the rear bearing housing. One to hold the oil transfer tube (2) and the second wrench to connect the B-NUT (3) on the oil line (4).
(7) TORQUE the B-nut (3) on the oil line (4) to between 16.5 and 13.5 lbf.ft (2.24 and 1.83 m.daN ) . (8) Clean the oil transfer tube (2) and oil line (4) with a Non Aqueous Cleaner-Non structural use - - (Material No.08BPA1) .
(9) Clean the APU compartment and remove presence of oil inside the compartment with cleaning solvent.
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 49-21-00-790-050-A ** ON A/C NOT FOR ALL 5. Close-up| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 121VU | APU/APU/CTL | 2KD | L42 |
| 121VU | APU/ECB/SPLY | 1KD | L41 |
Subtask 49-21-00-410-055-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) Set the light switch 11LJ to the OFF position.
(3) Close APU access doors 315AL and 316AR
(Ref. AMM TASK 52-41-00-410-001).
(4) Remove the access platform(s).
(5) Remove the safety harness.
Subtask 49-21-00-860-056-A ** ON A/C NOT FOR ALL (1) Make sure that the work area is clean and clear of tools and other items.
(2) Set the light switch 11LJ to the OFF position.
(3) Close APU access doors 315AL and 316AR
(Ref. AMM TASK 52-41-00-410-001).
(4) Remove the access platform(s).
(5) Remove the safety harness.
B. Aircraft Maintenance Configuration
(1) Pressurize the reservoirs of the hydraulic systems.
(Ref. AMM TASK 29-14-00-614-002).
(2) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
(3) Remove the WARNING NOTICE(S).
(1) Pressurize the reservoirs of the hydraulic systems.
(Ref. AMM TASK 29-14-00-614-002).
(2) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
(3) Remove the WARNING NOTICE(S).