W DOC AIRBUS | AMM A320F

Removal of the Engine-2 Pump-Suction Self-Sealing-Coupling


TASK 29-13-38-000-802-A
Removal of the Engine-2 Pump-Suction Self-Sealing-Coupling


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) - ADJUSTABLE
No specific
1
CONTAINER 5 L (1.32 USGAL)
No specific
AR
COVER - PROTECTION
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
No specific
AR
WARNING NOTICE(S)
No specific
1
WRENCH - STANDARD
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
195BB
FOR [1000EM2] (ENGINE-2)
447AL
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 29-10-00-864-002-A
Depressurize the Yellow Hydraulic System
TASK 29-14-00-614-001-A
Depressurization of the Hydraulic Reservoirs
TASK 71-13-00-010-010-A
Opening of the Fan Cowls 437AL(447AL),438AR(448AR)
3. Job Set-up
Subtask 29-13-38-860-054-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
   (1) Depressurize the Yellow hydraulic system (Ref. AMM TASK 29-10-00-864-002).
   (2) Depressurize the Yellow hydraulic reservoir (Ref. AMM TASK 29-14-00-614-001).
   (3) Put a WARNING NOTICE(S) in position to tell persons not to pressurize the Yellow hydraulic system.
   (4) Put a WARNING NOTICE(S) on access door 195BB to tell persons not to pressurize the Yellow hydraulic reservoir.
Subtask 29-13-38-941-054-A ** ON A/C NOT FOR ALL
B. Safety Precautions
   (1) On the center pedestal, on ENG panel 115VU, put a WARNING NOTICE(S) to tell persons not to start the engine.
   (2) Make sure that the engine 2 shutdown occurred not less than five minutes before you do this procedure.
   (3) In the cockpit, on the HYD section of the HYD/FUEL panel 40VU:
  • Put a WARNING NOTICE(S) in position to tell persons not to pressurize the Yellow hydraulic system.
   (4) On the overhead maintenance panel 50VU:
  • Make sure that the ON legend of the ENG/FADEC GND PWR/1(2) pushbutton switch is off.
  • Put a WARNING NOTICE(S) in position to tell persons not to energize the FADEC 1(2).
   (5) Put a CONTAINER 5 L (1.32 USGAL) in position below the fluid disconnect panel to collect the hydraulic fluid.
Subtask 29-13-38-865-052-A ** ON A/C NOT FOR ALL
C. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
121VUHYDRAULIC/Y HYD/PUMP ENG2/MONG3700GDQ37
121VUHYDRAULIC/Y HYD/PUMP ENG2/CTL3701GDQ36
Subtask 29-13-38-010-052-A ** ON A/C NOT FOR ALL
D. Get Access
   (1) Open the left fan-cowl door (Ref. AMM TASK 71-13-00-010-010).
     (a) FOR [1000EM2] (ENGINE-2)
   (2) Open access door 195BB.
   (3) Put the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE in position at engine 2.
4. Procedure
Subtask 29-13-38-020-052-A ** ON A/C NOT FOR ALL
A. Removal of the Engine-2 Pump-Suction Self-Sealing-Coupling (3672GM)
CAUTION: BE CAREFUL WHEN YOU DISCONNECT THE SUCTION HOSE AS THE HYDRAULIC FLUID WILL FLOW OUT.
   (1) Disconnect the hose coupling half from the fluid disconnect panel.
   (2) Disconnect the suction hose (5) from the self-sealing coupling (15). Drain the hydraulic fluid directly into the container.
     (a) Use a second WRENCH - STANDARD to hold the self-sealing coupling (15) when you loosen the coupling nut on the suction hose (5).
   (3) Disconnect the self-sealing coupling (15) from the union on the hydraulic pump (10).
     (a) Use a second WRENCH - STANDARD to hold the self-sealing coupling (15) when you loosen it.
   (4) Install COVER - PROTECTION on the self-sealing coupling (15), the suction hose (5) and the union on the hydraulic pump (10).
[Rev.10 from 2021] 2026.04.01 00:20:48 UTC