W DOC AIRBUS | AMM A320F

Removal of the Engine-Pump Pressure Switch


TASK 29-13-17-000-041-A
Removal of the Engine-Pump Pressure Switch


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: 3074GD ** 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
1
ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE
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)
No specific
2
WRENCH - STANDARD
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
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 71-13-00-010-040-B
Opening of the Fan Cowl Doors
3. Job Set-up
Subtask 29-13-17-860-054-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 WARNING NOTICE(S) in position to tell persons not to pressurize the Yellow hydraulic system:
  • on the ground service panel 198CB.
   (4) Put WARNING NOTICE(S) on the access door 195BB to tell persons not to pressurize the Yellow hydraulic reservoir.
Subtask 29-13-17-941-053-A ** ON A/C NOT FOR ALL
B. Safety Precautions
   (1) On the center pedestal, on 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 five minutes before you do this procedure.
   (3) In the cockpit, on the HYD section of overhead panel 40VU:
  • Put a WARNING NOTICE(S) in position to tell persons not to pressurize the Yellow hydraulic system.
   (4) On overhead maintenance panel 50VU:
  • Make sure that the ON legend of the ENG/FADEC GND PWR/1(2) pushbutton switch is off.
   (5) Put a WARNING NOTICE(S) in position to tell persons not to energize FADEC 1(2).
   (6) Put a CONTAINER 5 L (1.32 USGAL) below the pressure switch (3) to collect the hydraulic fluid.
Subtask 29-13-17-865-053-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
Subtask 29-13-17-010-052-A ** ON A/C NOT FOR ALL
D. Get Access
   (1) Open the left fan-cowl door 447AL (Ref. AMM TASK 71-13-00-010-040).
   (2) Put the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE in position at the engine.
4. Procedure
Subtask 29-13-17-020-051-A ** ON A/C NOT FOR ALL
A. Removal of the Engine-Pump Pressure Switch
F Engine-Pump Pressure Switch ** ON A/C NOT FOR ALL
   (1) Remove the engine-pump pressure switch.

PRE SB RA32029-13

     (a) Disconnect electrical connector 3074GD-A from the pressure switch (3).
     (b) Put a CAP - BLANKING on the electrical connector and on the pressure switch (3).
     (c) Remove the bolt (12), washers (7), (8) and (11), and nut (6) from the bonding clamp (9).
     (d) Remove the bonding jumper (10) and bonding clamp (9) from the pressure switch (3).
     (e) Disconnect the hydraulic tube (5) from the pressure switch (3).
       1 Hold the pressure switch (3) with a second WRENCH - STANDARD when you loosen the coupling nut on the tube.
     (f) Remove the two bolts (1) and the clamp (2) from the pressure switch (3).
     (g) Remove the pressure switch (3) from the engine.
     (h) Put the COVER - BLANKING on the pressure switch (3) and on the hydraulic tube (5).

END OF PRE SB RA32029-13

   (2) Remove the engine-pump pressure switch.

POST SB RA32029-13

     (a) Disconnect electrical connector 3074GD-A from the pressure switch (4).
     (b) Put the CAP - BLANKING on the electrical connector and on the pressure switch (4).
     (c) Remove the bolt (13), washers (9), (10) and (12), and nut (8) from the bonding clamp (11).
     (d) Remove the bonding jumper (7) and bonding clamp (11) from the pressure switch (4).
     (e) Remove the two bolts (1), washers (2) and clamp (3) from pressure switch (4).
     (f) Remove the bonding jumper (7) from the pressure switch (4).
     (g) Disconnect the hydraulic tube (5) from the pressure switch (4).
       1 Hold the pressure switch (4) with a second WRENCH - STANDARD when you loosen the coupling nut on the tube.
     (h) Remove the pressure switch (4) from the engine.
     (i) Put the COVER - BLANKING on the pressure switch (4) and on the hydraulic tube (5).

END OF POST SB RA32029-13

   (3) Remove the engine pump pressure switch.

POST SB RA32029-15 or POST SB RA32029-16

     (a) Disconnect the electrical connector 3074GD-A from the pressure switch (20).
     (b) Put COVER - BLANKING on the electrical connector and on the switch (20).
     (c) Remove the bolt (5), the washer (10) and the clamp (15) from the pressure switch (20).
NOTE: Use a second WRENCH - STANDARD to hold the adapter (30) when you loosen the pressure switch (20).
     (d) Remove the pressure switch (20) and packing (25) from the adapter (30). Discard the packing (25).
     (e) Put COVER - BLANKING on the switch (20) and the adapter (30).

END OF POST SB RA32029-15 OR POST SB RA32029-16
[Rev.10 from 2021] 2026.04.01 00:20:00 UTC