W DOC AIRBUS | AMM A320F

Removal of the Green Engine Pump


TASK 29-11-51-000-040-A
Removal of the Green Engine Pump


WARNING: OBEY THE HYDRAULIC SAFETY PROCEDURES.
WARNING: DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS FOR A SHORT TIME AFTER THE ENGINE IS SHUTDOWN. THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY.
CAUTION: DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS.
FIN: 1030GK ** 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
CAP - BLANKING
No specific
1
CONTAINER 5 L (1.32 USGAL)
No specific
AR
COVER - BLANKING
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
No specific
AR
WARNING NOTICE(S)
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
195BB, 197CB, 437AL
 C. Referenced Information
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 29-00-00-280-005-A
Check of the Green, Yellow or Blue Hydraulic System after Operation in an Overheat Condition
TASK 29-00-00-280-006-A
Check of the Green or Yellow Hydraulic System after Engine Pump Failure or Operation in a Possible Cavitation Condition - with Ground Cart Available
TASK 29-00-00-280-006-A-01
Check of the Green or Yellow Hydraulic System after Engine Pump Failure or Operation in a Possible Cavitation Condition - Ground Cart not Available
TASK 29-10-00-864-001-A
Depressurize the Green Hydraulic System
TASK 29-14-00-614-001-A
Depressurization of the Hydraulic Reservoirs
TASK 71-13-00-010-040-A
Opening of the Fan Cowl Doors
3. Job Set-up
Subtask 29-11-51-861-050-A ** ON A/C NOT FOR ALL
A. Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
Subtask 29-11-51-860-052-A ** ON A/C NOT FOR ALL
B. Aircraft Maintenance Configuration
   (1) Do the system check applicable after pump damage (Ref. AMM TASK 29-00-00-280-006), if you remove the pump:
  • Because of operation without fluid (dry running)
  • Or because of malfunction if you think that there is a pump internal damage.
    If there is a pump damage and an overheat condition, do also the system check applicable after overheat condition (Ref. AMM TASK 29-00-00-280-005).
   (2) Depressurize the Green hydraulic system (Ref. AMM TASK 29-10-00-864-001).
   (3) Depressurize the Green hydraulic reservoir (Ref. AMM TASK 29-14-00-614-001).
   (4) Put a WARNING NOTICE(S) in position to tell persons not to pressurize the Green hydraulic system:
  • on the ground service panel 197CB.
   (5) Put a WARNING NOTICE(S) in position on the access door 195BB to tell persons not to pressurize the Green hydraulic reservoir.
   (6) On the ECAM control panel, push the HYD key:
  • On the SD, the HYD page comes into view.
   (7) On the overhead panel 20VU:
  • Lift the guard and release the ENG1/FIRE pushbutton switch.
   (8) On the SD:
  • Make sure that the fire shut-off valve (1046GK) is closed.
Subtask 29-11-51-941-053-A ** ON A/C NOT FOR ALL
C. Safety Precautions
   (1) On the center pedestal, on the ENG panel 115VU:
  • Put a WARNING NOTICE(S) in position to tell persons not to start the engine.
   (2) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure.
   (3) Put a WARNING NOTICE(S) in position to tell persons not to pressurize the Green hydraulic system:
  • in the cockpit, on the HYD section of the panel 40VU.
   (4) On the 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) below the Green engine pump to collect the remaining fluid.
Subtask 29-11-51-865-053-A ** ON A/C NOT FOR ALL
D. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
121VUHYDRAULIC/G HYD/PUMP ENG1/CTL1701GKR35
121VUHYDRAULIC/G HYD/PUMP ENG1/MONG1702GKR34
Subtask 29-11-51-010-051-A ** ON A/C NOT FOR ALL
E. Get Access
   (1) Open the left fan cowl door 437AL (Ref. AMM TASK 71-13-00-010-040).
4. Procedure
Subtask 29-11-51-020-051-A ** ON A/C NOT FOR ALL
A. Removal of the Green Engine Pump Vickers
   (1) Disconnect the electrical connector (1030GKA).
   (2) Put a CAP - BLANKING on the electrical connector (1030GKA).
   (3) Disconnect the three hoses (case drain, suction and pressure hoses).
   (4) Disconnect the adapter (70) from the union (10) on the pump (5).
     (a) Use a second wrench to hold the union (10) on the pump(s) when you loosen the adapter.
   (5) Put COVER - BLANKING on the disconnected hose couplings, the pump unions (10), (15) and the reducer (20).
   (6) Slightly loosen the pump unions (10), (15) and the reducer (20).
   (7) Loosen the four mount nuts (25).
   (8) Turn the pump (5) clockwise to put the large portions of the pump mount holes in line with the nuts. Remove the pump from the gearbox.
NOTE: The pump weighs approximately 12.25 kg (27 lb).
   (9) Remove and discard the nuts (25).
   (10) Remove and discard the packing (50) from the pump shaft.
   (11) Remove and discard the gasket (30) from the mount pad.
   (12) Remove the union (10) from the pump (5) suction port.
   (13) Remove and discard the packing (40).
   (14) Put blanking covers on the pump (5) suction port and the union (10) port.
   (15) Remove the union (15) from the pump (5) case drain port.
   (16) Remove and discard the packing (45).
   (17) Put blanking covers on the pump (5) case drain port and the union (15) port.
   (18) Remove the reducer (20) from the pump (5) pressure port.
   (19) Remove and discard the back-up ring (35) and the packing (55).
   (20) Put blanking covers on the pump (5) pressure port and the reducer (20) port.
Subtask 29-11-51-020-057-A ** ON A/C NOT FOR ALL
B. Removal of the Green Engine Pump Abex
   (1) Disconnect the electrical connector (1030GKA).
   (2) Put a CAP - BLANKING on the electrical connector (1030GKA).
   (3) Disconnect the three hoses (case drain, suction and pressure hoses).
   (4) Disconnect the adapter (70) from the union (10) on the pump (5).
     (a) Use a second wrench to hold the union (10) on the pump(s) when you loosen the adapter.
   (5) Put COVER - BLANKING on the disconnected hose couplings, the pump unions (10), (15) and the reducer (20).
   (6) Slightly loosen the pump unions (10), (15) and the reducer (20).
   (7) Loosen the four mount nuts (25).
   (8) Turn the pump (5) clockwise to put the large portions of the pump mount holes in line with the nuts. Remove the pump from the gearbox.
NOTE: The pump weighs approximately 12.25 kg (27 lb).
   (9) Remove and discard the nuts (25).
   (10) Remove and discard the packing (50) from the pump shaft.
   (11) Remove and discard the gasket (30) from the mount pad.
   (12) Remove the union (10) from the pump (5) suction port.
   (13) Remove and discard the packing (40).
   (14) Put blanking covers on the pump (5) suction port and the union (10) port.
   (15) Remove the union (15) from the pump (5) case drain port.
   (16) Remove and discard the packing (45).
   (17) Put blanking covers on the pump (5) case drain port and the union (15) port.
   (18) Remove the reducer (20) from the pump (5) pressure port.
   (19) Remove and discard the back-up ring (35) and the packing (55).
   (20) Put blanking covers on the pump (5) pressure port and the reducer (20) port.
[Rev.10 from 2021] 2026.04.01 00:18:06 UTC