W DOC AIRBUS | AMM A320F

Removal of the Power Transfer Unit (PTU) Manifold of the Yellow Hydraulic System


TASK 29-13-15-000-001-A
Removal of the Power Transfer Unit (PTU) Manifold of the Yellow Hydraulic System


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.
FIN: 3015GM
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 3M (10 FT)- ADJUSTABLE
No specific
AR
CAP - BLANKING
No specific
1
CONTAINER 4 L (1 USGAL)
No specific
AR
PLUG - BLANKING
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
No specific
2
WARNING NOTICE(S)
 B. Referenced Information
REFERENCE
DESIGNATION
TASK 29-00-00-864-001-A
Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action
TASK 29-00-00-910-002-A
Safety Procedures of the Hydraulic System
TASK 29-14-00-614-001-A
Depressurization of the Hydraulic Reservoirs
TASK 29-23-00-860-001-A
Disconnection of the Isolation Coupling of the Power Transfer Unit (PTU)
TASK 32-12-00-010-001-A
Open the Main Gear Doors for Access
3. Job Set-up
Subtask 29-13-15-865-050-A
A. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
121VUHYDRAULIC/HYD POWER/Y3803GXN30
** ON A/C NOT FOR ALL
121VUHYDRAULIC/HYD POWER/Y3803GXN31
** ON A/C ALL
123VUY HYD/ELEC/PUMP3802GXAB06
123VUY HYD/ELEC/ELEC PUMP/NORM3801GXAB03
Subtask 29-13-15-860-052-A
B. Aircraft Maintenance Configuration
WARNING: OBEY THE HYDRAULIC SAFETY PROCEDURES.
   (1) Obey the hydraulic safety procedures (Ref. AMM TASK 29-00-00-910-002).
   (2) Put the WARNING NOTICE(S) in position to tell persons not to pressurize the Yellow hydraulic system:
  • in the cockpit on the hydraulic section 40VU of the overhead panel
  • on the ground service panel of the Yellow hydraulic system.
   (3) Make sure that the Yellow hydraulic system is depressurized and put it in the maintenance configuration.
(Ref. AMM TASK 29-00-00-864-001).
   (4) Depressurize the reservoir of the Yellow hydraulic system (Ref. AMM TASK 29-14-00-614-001).
   (5) Open the main gear doors (Ref. AMM TASK 32-12-00-010-001).
   (6) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at the main gear doors.
   (7) Put a CONTAINER 4 L (1 USGAL) below the PTU manifold of the Yellow hydraulic system to collect unwanted hydraulic fluid.
   (8) Disconnect the isolation coupling of the Power Transfer Unit (PTU) (Ref. AMM TASK 29-23-00-860-001).
4. Procedure
Subtask 29-13-15-020-050-E
A. Removal of the PTU Manifold
CAUTION: USE A SECOND WRENCH TO APPLY COUNTERTORQUE TO THE UNION WHEN YOU DISCONNECT/CONNECT HYDRAULIC LINES ON UNIONS. IF YOU DO NOT USE THE SECOND WRENCH, THERE IS A RISK THAT YOU WILL LOOSEN OR TIGHTEN THE UNION TOO MUCH.
   (1) Disconnect the electrical connector (29) from the PTU solenoid valve.
   (2) Put the CAP-BLANKING on each disconnected electrical connector and receptacle.
   (3) Loosen the pipe end-fitting (4) and disconnect the pipe (3) from the reducer (5).
   (4) Loosen the pipe end-fitting (22) and disconnect the pipe (21) from the check valve 3093GM.
   (5) Loosen the pipe end-fitting (49) and disconnect the pipe (48) from the union (50).
   (6) Loosen the pipe end-fitting (12) and disconnect the pipe (11) from the union (13).
   (7) If the bolts (1) are safetied with lockwire:
WARNING: USE PROTECTIVE GOGGLES AND GLOVES WHEN YOU REMOVE OR INSTALL LOCKWIRE. EACH TIME YOU CUT LOCKWIRE, REMOVE AND DISCARD IT IMMEDIATELY. LOOSE LOCKWIRE CAN CUT YOU OR MAKE YOU BLIND, AND/OR CAN CAUSE DAMAGE.
     (a) Remove and discard the lockwire from the bolts (1) and the coupling half (46).
   (8) Hold the manifold (7) and remove the bolts (1) and washers (2).
   (9) Remove the manifold (7) from the aircraft.
   (10) Install a PLUG - BLANKING in all pipe connections and manifold ports.
[Rev.10 from 2021] 2026.04.01 00:19:55 UTC