W DOC AIRBUS | AMM A320F

Fill the Hydraulic Fluid Reservoir with a Hand Pump


TASK 12-12-29-611-001-A
Fill the Hydraulic Fluid Reservoir with a Hand Pump


WARNING: DO NOT GET THE FLUID ON YOUR SKIN OR IN YOUR EYES. IF YOU DO:
  • FLUSH IT AWAY WITH CLEAN WATER
  • GET MEDICAL AID.
WARNING: MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS SURFACES ARE CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT.
WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
FIN: 1000GQ
FIN: 2000GQ
FIN: 3000GQ
1. Reason for the Job
NOTE: If the hydraulic reservoir is too full, adjust the fluid level accurately. It is not necessary to drain the hydraulic reservoir fully.
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
1
ACCESS PLATFORM 2M (6 FT)
No specific
1
CONTAINER - HYDRAULIC FLUID RESISTANT
No specific
1
THERMOMETER-INFRARED
No specific
1
WARNING NOTICE(S)
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.02ABA1)
Phosphate Ester Hydraulic Fluid-General Power - -
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
197CB, 197EB, 198CB
 D. Referenced Information
REFERENCE
DESIGNATION
TASK 12-14-29-614-001-A
Fill the Hydraulic Power Accumulators with Nitrogen
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 24-41-00-862-002-A
De-energize the Aircraft Electrical Circuits Supplied from the External Power
TASK 24-41-00-862-002-A-01
De-energize the Aircraft Electrical Circuits Supplied from the APU
TASK 24-41-00-862-002-A-02
De-energize the Aircraft Electrical Circuits Supplied from the Engine 1(2)
TASK 29-00-00-864-001-A
Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action
TASK 29-00-00-870-003-A
Bleeding Procedure of the Green Hydraulic System Downstream of the Engine Pump
TASK 29-00-00-870-007-A
Bleeding Procedure of the Yellow Hydraulic System Downstream of the Engine Pump
TASK 29-00-00-870-008-A
Bleeding Procedure of the Blue Hydraulic System Upstream of the Blue E-Pump
TASK 29-00-00-870-009-A
Bleeding Procedure of the Blue Hydraulic System Downstream of the Blue E-Pump
TASK 29-00-00-910-002-A
Safety Procedures of the Hydraulic System
TASK 29-10-00-680-001-A
Drainage of the Reservoir of the Green Hydraulic System
TASK 29-10-00-680-002-A
Drainage of the Reservoir of the Yellow Hydraulic System
TASK 29-10-00-680-003-A
Drainage of the Reservoir of the Blue Hydraulic System
TASK 29-14-00-614-002-A
Pressurization of the Hydraulic Reservoirs through the Ground Connector
TASK 29-14-00-614-002-A-01
Pressurization of the Hydraulic Reservoirs with the Auxiliary Power Unit (APU)
TASK 29-24-00-863-001-A
Pressurize the Yellow Hydraulic System with the Electric Pump
TASK 29-24-00-864-001-A
Depressurize the Yellow Hydraulic System
TASK 31-36-00-740-008-A
Access to the Parameter Call-Up Menus
TASK 32-12-00-010-001-A
Open the Main Gear Doors for Access
TASK 32-12-00-410-001-A
Close the Main Gear Doors after Access
TASK 32-44-11-200-001-A
Functional Check of Parking/Emergency Brake Accumulator by Reading the Charge Pressure on the Accumulator Gauge
3. Job Set-up
Subtask 12-12-29-860-051-A
A. Aircraft Maintenance Configuration
WARNING: OBEY THE HYDRAULIC SAFETY PROCEDURES.
   (1) Obey the hydraulic safety procedures (Ref. AMM TASK 29-00-00-910-002).
   (2) Make sure that the aircraft is in this configuration:
  • The speed brakes and the spoilers are retracted
  • The thrust reversers are stowed (closed)
  • The landing gear is extended and the landing gear doors are closed
NOTE: One main landing gear door may be kept open.
  • The FWD and aft cargo-compartment doors 825 and 826 are closed
  • All the other hydraulically controlled systems are in the normal position.
   (3) Make sure that the hydraulic systems are depressurized and put them in the maintenance configuration
(Ref. AMM TASK 29-00-00-864-001).
NOTE: Do not depressurize the system reservoirs.
   (4) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
Subtask 12-12-29-010-054-A
B. Get Access
   (1) Open the left and right Main Landing Gear (MLG) doors (Ref. AMM TASK 32-12-00-010-001).
   (2) Open the access panels 197CB, 198CB and 197EB.
   (3) Put the ACCESS PLATFORM 2M (6 FT) in position.
Subtask 12-12-29-210-052-A
C. Inspection of the Pressure Values
   (1) Make sure that the nitrogen fill pressure of the brake accumulator 2582GM is correct (Ref. AMM TASK 32-44-11-200-001).
   (2) Make sure that the hydraulic accumulators 1070GM, 2070GM and 3070GM have a nitrogen pressure of 130 bar (1885.4901 psi) at 20 deg.C (68.00 deg.F).
If necessary, adjust the nitrogen pressure (Ref. AMM TASK 12-14-29-614-001).
   (3) Make sure that the pressure on the indicator of the related reservoir is 3.5 -0 bar or +0.3 bar (50.7632 -0 psi or +4.3511 psi). If necessary, pressurize the reservoir (Ref. AMM TASK 29-14-00-614-002).
NOTE: If you pressurize the Hydraulic Reservoir with the APU, the Hydraulic Reservoir pressure will be approximately 1.65 bar (24 psi).
Subtask 12-12-29-863-050-A
D. Pressurization of the Auxiliary Braking System
   (1) Pressurize the Yellow hydraulic system with the Yellow E-pump (Ref. AMM TASK 29-24-00-863-001) to pressurize the brake accumulator system to 206 bar (2987.7766 psi).
   (2) On the panel 110VU, put the parking brake control switch 73GG to the ON position.
   (3) Make sure that the pressure on the triple indicator 60GG shows the left and right pressure values.
   (4) Close the left and right MLG doors (Ref. AMM TASK 32-12-00-410-001).
   (5) Depressurize the Yellow hydraulic system (Ref. AMM TASK 29-24-00-864-001).
NOTE: Do not depressurize the alternate braking system.
   (6) Put the WARNING NOTICE(S) on the panel 40VU in the cockpit to tell persons not to pressurize the hydraulic systems.
4. Procedure
Subtask 12-12-29-611-052-A
A. Fill the Hydraulic Reservoirs (Refer to the Tables)
   (1) Remove the hand pump lever 3270GM from the service panel of the Yellow hydraulic system.
   (2) On the service panel of the Green hydraulic system, connect the hand pump lever 3270GM to the shaft of the hand pump 1009GM.
   (3) Remove the flexible hose 1699GM from the service panel compartment of the Green hydraulic system.
   (4) Remove the blanking cap and connect the flexible hose to the fill valve 1698GM. Put the other end in the CONTAINER - HYDRAULIC FLUID RESISTANT with the Phosphate Ester Hydraulic Fluid-General Power - - (Material No.02ABA1) .
NOTE: Do not use the Phosphate Ester Hydraulic Fluid-General Power - - (Material No.02ABA1) for outside air temperature on ground below -40 deg.C (-40 deg.F).
NOTE: It is not permitted to use high-density fluid Skydrol 500B-4 for A320NEO family.
   (5) Turn the selector 1134GQ to the position that is correct for the system you will fill.
   (6) Make sure that on the quantity indicator 1834GQ the colored light of the related system comes on.
   (7) Get the reservoir temperature using one of the methods:
     (a) Read out reservoir temperature through ACMS RTM (Real Time Monitoring) and use the related AIDS label call-up:
       1 For the reservoir of the Green hydraulic system - 029/1/172/01/08,
       2 For the reservoir of the Yellow hydraulic system - 029/1/172/10/08,
       3 For the reservoir of the Blue hydraulic system - 029/1/172/11/08.
Refer to (Ref. AMM TASK 31-36-00-740-008) to get access to the parameter call-up menus.
     (b) As an alternative to previous method, use the THERMOMETER-INFRARED to record the hydraulic fluid temperature.
NOTE: Measure the temperature on the lower part of the reservoir in the range of the fluid level.
     (c) As different alternative use the OAT (Outside Air Temperature), if the aircraft was parked for last 3h before servicing.
   (8) Fill the hydraulic reservoir:
CAUTION: MAKE SURE THAT YOU DO NOT PUT TOO MUCH FLUID IN THE RESERVOIR. IF THE RESERVOIR IS TOO FULL, YOU CANNOT PRESSURIZE IT SUFFICIENTLY. LOW AIR PRESSURE CAN CAUSE THE MESSAGE "RSVR LO AIR PR" TO SHOW IN FLIGHT ON THE UPPER AND LOWER ECAM DISPLAY UNITS.
     (a) Operate the hand pump 1009GM.
     (b) Monitor the increase of the fluid level of the related system on the quantity indicator and do these steps:
       1 Stop the flow of the hydraulic fluid when the pointer is almost to the fill level given in the table 2 (HYDRAULIC RESERVOIR FILLING CAPACITIES).
       2 Slowly continue to fill again, until the pointer shows almost to the fill level given in the table 2 (HYDRAULIC RESERVOIR FILLING CAPACITIES).
NOTE: Each open MLG door decreases the volume in the green reservoir by 0.25 l (0.0660 USgal).
NOTE: Each open cargo door decreases the volume in the yellow reservoir by 0.2 l (0.0528 USgal).
NOTE: After servicing of the reservoir with the temperature adjustment instruction, the cockpit reservoir filling level is permitted to be above the normal filling range, if the reservoir gauge on the ground service panel is in permitted range.
NOTE: The temperature of the hydraulic fluid can change when you use different method of measurement. The differences agree with the tolerance.
HYDRAULIC RESERVOIR CAPACITIES
SYSTEM/RESERVOIR
QUANTITY LITERS
QUANTITY US GAL
REMARKS
GREEN SYSTEM


At 20.0 deg.C (68 deg.F).
Total Capacity
23
6.1

Max. Capacity shown on the Gage
18
4.8

Fill Level
14
3.7
See the table - HYDRAULIC RESERVOIR FILLING CAPACITIES.
Low Level Warning
3
0.8

BLUE SYSTEM


At 20.0 deg.C (68 deg.F).
Total Capacity
10
2.6

Max. Capacity shown on the Gage
8
2.1

Fill Level
6
1.6
See the table - HYDRAULIC RESERVOIR FILLING CAPACITIES.
Low Level Warning
2
0.5

YELLOW SYSTEM


At 20.0 deg.C (68 deg.F).
With the normal nitrogen precharging pressure in the brake accumulator 2582GM and the auxiliary brake system pressurized.
Total Capacity
20
5.3

Max. Capacity shown on the Gage
18
4.8

Fill Level
12
3.2
See the table - HYDRAULIC RESERVOIR FILLING CAPACITIES.
Low Level Warning
3
0.8


HYDRAULIC RESERVOIR FILLING CAPACITIES
SYSTEM/RESERVOIR
RESERVOIR TEMPERATURE (deg.C/deg.F)
QUANTITY LITERS
QUANTITY US GAL
GREEN SYSTEM
-20 deg.C (-4 deg.F) or less
12.00
3.2

-10 deg.C (14 deg.F)
12.50
3.3

0 deg.C (32 deg.F)
13.00
3.4

10 deg.C (50 deg.F)
13.50
3.6

20 deg.C (68 deg.F)
14.00
3.7

30 deg.C (86 deg.F)
14.50
3.8

40 deg.C (104 deg.F)
15.00
4.0

50 deg.C (122 deg.F) or more
15.50
4.1
BLUE SYSTEM
-20 deg.C (-4 deg.F) or less
5.25
1.4

-10 deg.C (14 deg.F)
5.50
1.5

0 deg.C (32 deg.F)
5.50
1.5

10 deg.C (50 deg.F)
5.75
1.5

20 deg.C (68 deg.F)
6.00
1.6

30 deg.C (86 deg.F)
6.25
1.7

40 deg.C (104 deg.F)
6.50
1.7

50 deg.C (122 deg.F) or more
6.50
1.7
YELLOW SYSTEM
-20 deg.C (-4 deg.F) or less
11.00
2.9

-10 deg.C (14 deg.F)
11.25
3.0

0 deg.C (32 deg.F)
11.50
3.0

10 deg.C (50 deg.F)
11.75
3.1

20 deg.C (68 deg.F)
12.00
3.2

30 deg.C (86 deg.F)
12.25
3.2

40 deg.C (104 deg.F)
12.50
3.3

50 deg.C (122 deg.F) or more
12.75
3.4
       3 After servicing of the reservoir, refer to previous work step:
  • The cockpit reservoir full level is permitted to be above the normal full limit, if the reservoir level has been adjusted before or the reservoir gauge on the ground service panel is according to the table 2 (HYDRAULIC RESERVOIR FILLING CAPACITIES).
   (9) If a reservoir is filled too much, drain the unwanted hydraulic fluid:
   (10) Turn the selector 1134GQ to the NEUTRAL position.
   (11) Make sure that the colored light on the quantity indicator 1834GQ goes off.
   (12) Remove the flexible hose and install the blanking cap on the pump.
   (13) Put the flexible hose back in position in the service panel compartment of the Green hydraulic system.
   (14) Remove the hand pump lever 3270GM from the hand pump 1009GM. Then put the hand pump lever in position on the service panel of the Yellow hydraulic system.
   (15) If you filled the hydraulic reservoir after:
  • Maintenance
  • Removal/installation of hydraulic components
  • Hydraulic fluid low level (loss of the hydraulic system)
  • High loss of hydraulic fluid:
     (a) Use the related bleeding procedure as follows:
5. Close-up
Subtask 12-12-29-410-054-A
A. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Close the access panels 197CB 198CB and if necessary 197EB.
Subtask 12-12-29-860-050-A
B. Put the aircraft back to its initial configuration.
   (1) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
   (2) Remove the WARNING NOTICE(S).
   (3) Remove the access platform(s).
[Rev.10 from 2021] 2026.04.01 03:56:14 UTC