Installation of the Engine Pump
TASK 29-13-51-400-010-A
Installation of the Engine Pump
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Consumable Materials
C. Work Zones and Access Panels
D. Expendable Parts
E. Referenced Information
3. Job Set-up
Subtask 29-13-51-860-051-A ** ON A/C NOT FOR ALL
Subtask 29-13-51-420-057-A ** ON A/C NOT FOR ALL
Subtask 29-13-51-860-075-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.01 00:23:36 UTC
Installation of the Engine Pump
WARNING:
BE CAREFUL DURING THE REMOVAL/INSTALLATION OF THE PUMP BECAUSE IT WEIGHS 22 LB (10.2 KG).
WARNING:
DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH.
WARNING:
BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
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.
1. Reason for the JobSelf explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Consumable Materials
| REFERENCE | DESIGNATION |
|---|---|
| (Material No.V01-002) | cleaning fluid |
| (Material No.V10-039) | engine oil |
| (Material No.02ABA1) | Phosphate Ester Hydraulic Fluid-General Power - - |
| (Material No.14SBA1) | Textile-Lint free Cotton - |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 440 | ENG 2 AIR INTAKE, FAN AND ACCESS GEARBOX |
| 195BB | |
| FOR [1000EM2] (ENGINE-2) | |
| 447AL, 448AR | |
| FIG.ITEM | DESIGNATION | IPC-CSN |
|---|---|---|
| 8 | PACKING | AIPC 29-11-51-20-040 |
| 10 | PACKING | AIPC 29-13-49-80-140 |
| 13 | PACKING | AIPC 29-13-49-80-150 |
| 4 | PACKING | AIPC 29-13-49-80-170 |
| 15 | PACKING | AIPC 29-13-49-80-180 |
| 16 | PACKING | AIPC 29-13-49-80-190 |
| 19 | PACKING | AIPC 29-13-49-80-390 |
| 20 | RETAINERS | AIPC 29-13-49-80-400 |
| 21 | PACKING | AIPC 29-13-49-80-410 |
| 9 | NUTS | AIPC 29-13-51-80-010 |
| 7 | GASKET | AIPC 29-13-51-80-020 |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 29-10-00-720-001-A | Functional Check of Hydraulic Fire Shut-Off Valves |
| TASK 29-13-51-860-001-A | Hydraulic Maintenance Procedure after an Engine Installation (with Engine Pump Installed) or after an Engine Pump Installation |
| TASK 29-14-00-614-001-A | Depressurization of the Hydraulic Reservoirs |
| TASK 29-24-00-864-001-A | Depressurize the Yellow Hydraulic System |
| TASK 70-23-11-911-013-A | General Torque Tightening Techniques |
| TASK 70-23-13-911-010-A | Procedures for the Installation of Preformed Packings |
| TASK 70-23-15-912-010-A | Connection of Electrical Connectors |
| TASK 71-13-00-010-010-A | Opening of the Fan Cowls 437AL(447AL),438AR(448AR) |
| TASK 71-13-00-410-010-A | Closing of the Fan Cowls 437AL(447AL),438AR(448AR) |
Subtask 29-13-51-860-051-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
(1) Make sure that the Yellow hydraulic system is depressurized (Ref. AMM TASK 29-24-00-864-001).
(2) Make sure that the Yellow hydraulic reservoir is depressurized (Ref. AMM TASK 29-14-00-614-001).
(3) Make sure that the WARNING NOTICE(S) is (are) in position to tell persons not to pressurize the Yellow hydraulic system:
(5) Make sure that an ACCESS PLATFORM 1M (3 FT)-ADJUSTABLE is in position at the engine.
(6) Make sure that the fan cowl doors are open (Ref. AMM TASK 71-13-00-010-010):
(a) FOR [1000EM2] (ENGINE-2)
447AL 448AR.
(7) On the ECAM control panel:
Subtask 29-13-51-941-051-A ** ON A/C NOT FOR ALL (1) Make sure that the Yellow hydraulic system is depressurized (Ref. AMM TASK 29-24-00-864-001).
(2) Make sure that the Yellow hydraulic reservoir is depressurized (Ref. AMM TASK 29-14-00-614-001).
(3) Make sure that the WARNING NOTICE(S) is (are) in position to tell persons not to pressurize the Yellow hydraulic system:
- on the ground service panel 198CB.
(5) Make sure that an ACCESS PLATFORM 1M (3 FT)-ADJUSTABLE is in position at the engine.
(6) Make sure that the fan cowl doors are open (Ref. AMM TASK 71-13-00-010-010):
(a) FOR [1000EM2] (ENGINE-2)
447AL 448AR.
(7) On the ECAM control panel:
- Make sure that the HYD key is pushed.
- Make sure that the ENG2/FIRE pushbutton is released.
- Make sure that the fire shut-off valve (3046GD) is closed.
B. Safety Precautions
(1) On the center pedestal, on the ENG panel 115VU:
(3) Make sure that the WARNING NOTICE(S) is (are) in position to tell persons not to pressurize the Yellow hydraulic system:
(6) Make sure that a CONTAINER 5 L (1.32 USGAL) is below the hydraulic connections of the engine pump to collect the remaining fluid.
Subtask 29-13-51-865-051-A ** ON A/C NOT FOR ALL (1) On the center pedestal, on the ENG panel 115VU:
- make sure that the WARNING NOTICE(S) is (are) in position to tell persons not to start the engine.
(3) Make sure that the WARNING NOTICE(S) is (are) in position to tell persons not to pressurize the Yellow hydraulic system:
- in the cockpit, on the HYD section of the overhead panel 40VU.
- make sure that the ON legend of the ENG/FADEC GND PWR/1(2) pushbutton switch is off.
(6) Make sure that a CONTAINER 5 L (1.32 USGAL) is below the hydraulic connections of the engine pump to collect the remaining fluid.
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
4. Procedure| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 121VU | HYDRAULIC/Y HYD/PUMP ENG2/CTL | 3701GD | Q36 |
Subtask 29-13-51-420-057-A ** ON A/C NOT FOR ALL
A. Installation of the Unions
PRE SBN 29-0265
(1) Lightly lubricate the threads and abutment faces of the unions with the Phosphate Ester Hydraulic Fluid-General Power - - (Material No.02ABA1) used in the aircraft hydraulic system.
(2) Put new AIPC 29-13-49-80-190 PACKING (16), AIPC 29-13-49-80-180 PACKING (15) and AIPC 29-13-49-80-170 PACKING (4) on the union (3), AIPC 29-13-49-80-140 PACKING (10) on the union (11) and AIPC 29-13-49-80-150 PACKING (13) on the union (14) (Ref. AMM TASK 70-23-13-911-010).
(3) Install the unions (3), (11) and (14) in the pump (6).
(4) TORQUE the union (11) to between 24.46 and 22.13 lbf.ft (3.32 and 3.00 m.daN )
.
(5) TORQUE the union (14) to between 78.98 and 71.38 lbf.ft (10.71 and 9.68 m.daN )
.
(6) TORQUE the union (3) to between 65.81 and 59.55 lbf.ft (8.92 and 8.07 m.daN )
.
(7) Install the self-sealing coupling (17).
(8) TORQUE the self-sealing coupling (17) to between 75 and 66.7 lbf.ft (10.17 and 9.04 m.daN )
.
(9) Visual inspection of the self-sealing coupling (17):
(a) Make sure that the valve is correctly aligned with the body.
(b) Make sure that there is no leak.
(c) Replace if necessary.
END OF PRE SBN 29-0265
Subtask 29-13-51-420-078-A ** ON A/C NOT FOR ALL PRE SBN 29-0265
(1) Lightly lubricate the threads and abutment faces of the unions with the Phosphate Ester Hydraulic Fluid-General Power - - (Material No.02ABA1) used in the aircraft hydraulic system.
(2) Put new AIPC 29-13-49-80-190 PACKING (16), AIPC 29-13-49-80-180 PACKING (15) and AIPC 29-13-49-80-170 PACKING (4) on the union (3), AIPC 29-13-49-80-140 PACKING (10) on the union (11) and AIPC 29-13-49-80-150 PACKING (13) on the union (14) (Ref. AMM TASK 70-23-13-911-010).
(3) Install the unions (3), (11) and (14) in the pump (6).
(4) TORQUE the union (11) to between 24.46 and 22.13 lbf.ft (3.32 and 3.00 m.daN )
. (5) TORQUE the union (14) to between 78.98 and 71.38 lbf.ft (10.71 and 9.68 m.daN )
. (6) TORQUE the union (3) to between 65.81 and 59.55 lbf.ft (8.92 and 8.07 m.daN )
. (7) Install the self-sealing coupling (17).
(8) TORQUE the self-sealing coupling (17) to between 75 and 66.7 lbf.ft (10.17 and 9.04 m.daN )
. (9) Visual inspection of the self-sealing coupling (17):
(a) Make sure that the valve is correctly aligned with the body.
(b) Make sure that there is no leak.
(c) Replace if necessary.
END OF PRE SBN 29-0265
B. Installation of the Unions and Dampener
POST SBN 29-0265
(1) Lightly lubricate the threads and abutment faces of the unions with the Phosphate Ester Hydraulic Fluid-General Power - - (Material No.02ABA1) used in the aircraft hydraulic system.
(2) Put new AIPC 29-13-49-80-140 PACKING (10) on the union (11) and new AIPC 29-13-49-80-150 PACKING (13) on the union (14). Put new AIPC 29-13-49-80-390 PACKING (19), new AIPC 29-13-49-80-410 PACKING (21) and AIPC 29-13-49-80-400 RETAINERS (20) on the dampener (18) (Ref. AMM TASK 70-23-13-911-010).
(3) Install the dampener (18), the unions (11) and (14) on the pump (6).
(4) TORQUE the union (11) to between 24.46 and 22.13 lbf.ft (3.32 and 3.00 m.daN )
.
(5) TORQUE the union (14) to between 78.98 and 71.38 lbf.ft (10.71 and 9.68 m.daN )
.
(6) TORQUE the dampener (18) to between 88.33 and 81.25 lbf.ft (11.98 and 11.02 m.daN )
.
(7) Install the self-sealing coupling (17).
(8) TORQUE the self-sealing coupling (17) to between 75 and 66.7 lbf.ft (10.17 and 9.04 m.daN )
.
(9) Visual inspection of the self-sealing coupling (17):
(a) Make sure that the valve is correctly aligned with the body.
(b) Make sure that there is no leak.
(c) Replace if necessary.
END OF POST SBN 29-0265
Subtask 29-13-51-630-051-A ** ON A/C NOT FOR ALL POST SBN 29-0265
(1) Lightly lubricate the threads and abutment faces of the unions with the Phosphate Ester Hydraulic Fluid-General Power - - (Material No.02ABA1) used in the aircraft hydraulic system.
(2) Put new AIPC 29-13-49-80-140 PACKING (10) on the union (11) and new AIPC 29-13-49-80-150 PACKING (13) on the union (14). Put new AIPC 29-13-49-80-390 PACKING (19), new AIPC 29-13-49-80-410 PACKING (21) and AIPC 29-13-49-80-400 RETAINERS (20) on the dampener (18) (Ref. AMM TASK 70-23-13-911-010).
(3) Install the dampener (18), the unions (11) and (14) on the pump (6).
(4) TORQUE the union (11) to between 24.46 and 22.13 lbf.ft (3.32 and 3.00 m.daN )
. (5) TORQUE the union (14) to between 78.98 and 71.38 lbf.ft (10.71 and 9.68 m.daN )
. (6) TORQUE the dampener (18) to between 88.33 and 81.25 lbf.ft (11.98 and 11.02 m.daN )
. (7) Install the self-sealing coupling (17).
(8) TORQUE the self-sealing coupling (17) to between 75 and 66.7 lbf.ft (10.17 and 9.04 m.daN )
. (9) Visual inspection of the self-sealing coupling (17):
(a) Make sure that the valve is correctly aligned with the body.
(b) Make sure that there is no leak.
(c) Replace if necessary.
END OF POST SBN 29-0265
C. Preparation before Installation
(2) Remove the plugs from the openings of the pump and the hoses.
(3) Cleaning of the pump mating face:
(a) Use a clean Textile-Lint free Cotton - (Material No.14SBA1) , made moist with cleaning fluid (Material No.V01-002) , to clean the hydraulic pump mating face on the gearbox.
(4) Put the new AIPC 29-11-51-20-040 PACKING (8) on the hydraulic pump shaft (Ref. AMM TASK 70-23-13-911-010).
(5) Lubricate the splines of the hydraulic pump shaft with engine oil (Material No.V10-039) .
Subtask 29-13-51-420-051-A ** ON A/C NOT FOR ALL CAUTION:
DO NOT APPLY LUBRICANT ON POLYAMIDE-TYPE INTERNAL COUPLING- SHAFTS WHEN YOU INSTALL THE SHAFT ON THE PUMP. IF YOU APPLY LUBRICANT, DAMAGE CAN OCCUR.
(1) Remove the covers from the mating face of the pump and the gearbox. (2) Remove the plugs from the openings of the pump and the hoses.
(3) Cleaning of the pump mating face:
(a) Use a clean Textile-Lint free Cotton - (Material No.14SBA1) , made moist with cleaning fluid (Material No.V01-002) , to clean the hydraulic pump mating face on the gearbox.
(4) Put the new AIPC 29-11-51-20-040 PACKING (8) on the hydraulic pump shaft (Ref. AMM TASK 70-23-13-911-010).
(5) Lubricate the splines of the hydraulic pump shaft with engine oil (Material No.V10-039) .
D. Installation of the Hydraulic Pump
(2) Align the pump shaft with the gearbox splined drive and the slots in the mounting flange with the mounting studs.
(3) Push the pump rearward until the mating faces touch. Turn the pump counterclockwise until the ends of the slots come against the mounting studs.
(4) Attach the pump with the nuts (9).
(5) Do a running torque check of the nuts (9) with a WRENCH - TORQUE.
(b) Set the WRENCH - TORQUE to 9.5 lbf.in (0.11 m.daN) and turn each nut in the tightening direction. The nut(s) must not turn before the set torque value.
(c) If the nut(s) turn before you get a torque of 9.5 lbf.in (0.11 m.daN), replace the nut(s) and do Step 4.D.(5) again for each replacement nut.
(d) If the running torque check is correct, do not remove the nut(s) from the stud(s) and do Step 4.D.(6).
(6) TORQUE the nuts to between 320 and 260 lbf.in (3.62 and 2.94 m.daN )
(Ref. AMM TASK 70-23-11-911-013).
Subtask 29-13-51-420-050-A ** ON A/C NOT FOR ALL CAUTION:
BE CAREFUL DURING REMOVAL/INSTALLATION OF THE PUMP, SUPPORT THE WEIGHT OF THE PUMP. MAKE SURE THAT THE SPLINED DRIVE SHAFT IS PERPENDICULAR TO THE MOUNTING FLANGE. IF NOT, SIDE LOADS CAN BEND THE DRIVE SHAFT AND:
(1) Put the AIPC 29-13-51-80-020 GASKET (7) on the gearbox mating face (Ref. AMM TASK 70-23-13-911-010). - PREVENT CORRECT INSTALLATION OF THE PUMP.
- CAUSE DAMAGE WHEN THE PUMP OPERATES.
(2) Align the pump shaft with the gearbox splined drive and the slots in the mounting flange with the mounting studs.
(3) Push the pump rearward until the mating faces touch. Turn the pump counterclockwise until the ends of the slots come against the mounting studs.
(4) Attach the pump with the nuts (9).
(5) Do a running torque check of the nuts (9) with a WRENCH - TORQUE.
CAUTION:
DISCARD THE NUT(S) IF YOU CAN TURN THEM BY HAND WITH NO RESISTANCE.
(a) Install new AIPC 29-13-51-80-010 NUTS (9) on the studs of the mount pad and turn the nuts until resistance is felt. (b) Set the WRENCH - TORQUE to 9.5 lbf.in (0.11 m.daN) and turn each nut in the tightening direction. The nut(s) must not turn before the set torque value.
(c) If the nut(s) turn before you get a torque of 9.5 lbf.in (0.11 m.daN), replace the nut(s) and do Step 4.D.(5) again for each replacement nut.
(d) If the running torque check is correct, do not remove the nut(s) from the stud(s) and do Step 4.D.(6).
(6) TORQUE the nuts to between 320 and 260 lbf.in (3.62 and 2.94 m.daN )
(Ref. AMM TASK 70-23-11-911-013). E. Installation of the Hoses
(a) Connect the case drain hose (12) to the pump union.
(b) TORQUE the hose nut to between 245 and 215 lbf.in (2.77 and 2.43 m.daN )
(Ref. AMM TASK 70-23-11-911-013).
(2) Connect the suction hose (1):
(a) Connect the suction hose (1) to the pump union.
(b) TORQUE the hose nut to between 900 and 800 lbf.in (10.17 and 9.04 m.daN )
(Ref. AMM TASK 70-23-11-911-013).
PRE SBN 26-0265
(3) Connect the pressure hose (2):
(a) Connect the pressure hose (2) to the pump union.
(b) TORQUE the hose nut to between 945 and 855 lbf.in (10.68 and 9.66 m.daN )
(Ref. AMM TASK 70-23-11-911-013).
END OF PRE SBN 29-0265
POST SBN 29-0265
(4) Connect the pressure hose (2):
(a) Connect the pressure hose (2) to the dampener (18).
(b) TORQUE the nut of the pressure hose (2) to between 70 and 62.5 lbf.ft (9.49 and 8.47 m.daN )
(Ref. AMM TASK 70-23-11-911-013).
END OF POST SBN 29-0265
(5) Connect the electrical connector (5) to the pump.
(a) Remove the blanking caps from the electrical connector (5) and the electrical receptacle.
(b) Connect the electrical connector (5) to the electrical receptacle (Ref. AMM TASK 70-23-15-912-010).
Subtask 29-13-51-865-052-A ** ON A/C NOT FOR ALL CAUTION:
USE A SECOND WRENCH TO HOLD THE UNION DURING THE TORQUE PROCEDURE. THIS IS TO PREVENT DAMAGE TO THE PUMP.
(1) Connect the case drain hose (12): (a) Connect the case drain hose (12) to the pump union.
(b) TORQUE the hose nut to between 245 and 215 lbf.in (2.77 and 2.43 m.daN )
(Ref. AMM TASK 70-23-11-911-013). (2) Connect the suction hose (1):
(a) Connect the suction hose (1) to the pump union.
(b) TORQUE the hose nut to between 900 and 800 lbf.in (10.17 and 9.04 m.daN )
(Ref. AMM TASK 70-23-11-911-013). PRE SBN 26-0265
(3) Connect the pressure hose (2):
(a) Connect the pressure hose (2) to the pump union.
(b) TORQUE the hose nut to between 945 and 855 lbf.in (10.68 and 9.66 m.daN )
(Ref. AMM TASK 70-23-11-911-013). END OF PRE SBN 29-0265
POST SBN 29-0265
(4) Connect the pressure hose (2):
(a) Connect the pressure hose (2) to the dampener (18).
(b) TORQUE the nut of the pressure hose (2) to between 70 and 62.5 lbf.ft (9.49 and 8.47 m.daN )
(Ref. AMM TASK 70-23-11-911-013). END OF POST SBN 29-0265
(5) Connect the electrical connector (5) to the pump.
(a) Remove the blanking caps from the electrical connector (5) and the electrical receptacle.
(b) Connect the electrical connector (5) to the electrical receptacle (Ref. AMM TASK 70-23-15-912-010).
F. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 29-13-51-860-062-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 121VU | HYDRAULIC/Y HYD/PUMP ENG2/CTL | 3701GD | Q36 |
G. Do the hydraulic maintenance procedure after an engine pump installation (Ref. AMM TASK 29-13-51-860-001).
5. Close-upSubtask 29-13-51-860-075-A ** ON A/C NOT FOR ALL
A. Put the aircraft back to its initial configuration.
(1) On the ECAM control panel, push the HYD key:
Subtask 29-13-51-410-050-A ** ON A/C NOT FOR ALL (1) On the ECAM control panel, push the HYD key:
- On the SD, the HYD page comes into view.
- Push the ENG2/FIRE pushbutton switch.
- Make sure that the fire shut-off valve (3046GD) is opened.
B. Remove the Safety Precautions
(1) Remove the WARNING NOTICE(S).
(2) Remove the access platform(s).
(3) Remove the container.
(4) Make sure that the work area is clean and clear of tools and other items.
(5) Close the fan cowl doors (Ref. AMM TASK 71-13-00-410-010):
(a) FOR [1000EM2] (ENGINE-2)
447AL 448AR.
(6) Close the access door 195BB.
(1) Remove the WARNING NOTICE(S).
(2) Remove the access platform(s).
(3) Remove the container.
(4) Make sure that the work area is clean and clear of tools and other items.
(5) Close the fan cowl doors (Ref. AMM TASK 71-13-00-410-010):
(a) FOR [1000EM2] (ENGINE-2)
447AL 448AR.
(6) Close the access door 195BB.
Abex Hydraulic Pump