W DOC AIRBUS | AMM A320F

Removal of the Pressure Relief Valve Hose/Tube


TASK 29-13-49-000-006-A
Removal of the Pressure Relief Valve Hose/Tube


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.
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
CONTAINER 5 L (1.32 USGAL)
No specific
AR
COVER - PROTECTION
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
No specific
AR
WARNING NOTICE(S)
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
447AL
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 71-13-00-010-040-B
Opening of the Fan Cowl Doors
3. Job Set-up
Subtask 29-13-49-860-079-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
   (1) Make sure that the Yellow hydraulic system is depressurized and put it in the maintenance configuration.
(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 29-13-49-941-073-A ** ON A/C NOT FOR ALL
B. Safety Precautions
   (1) On the center pedestal, on the ENG panel 115VU:
  • put WARNING NOTICE(S) 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 WARNING NOTICE(S) in position to tell persons not to pressurize the Yellow hydraulic system:
  • in the cockpit, on the HYD section of the overhead panel 40VU.
   (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.
   (5) Put WARNING NOTICE(S) to tell persons not to energize the FADEC 1(2).
   (6) Put a CONTAINER 5 L (1.32 USGAL) below the higher pressure relief valve hose/tube (25) to collect the remaining fluid.
Subtask 29-13-49-010-068-A ** ON A/C NOT FOR ALL
C. Get Access
   (1) Open the left fan-cowl door (Ref. AMM TASK 71-13-00-010-040):
     (a) FOR [1000EM2] (ENGINE-2)
open the door 447AL.
   (2) Put the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE in position at the left fan-cowl door 447AL.
Subtask 29-13-49-865-061-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/Y HYD/PUMP ENG2/MONG3700GDQ37
4. Procedure
Subtask 29-13-49-020-067-A ** ON A/C NOT FOR ALL
A. Removal of the Pressure Relief Valve Hose/Tube
   (1) Disconnect the higher pressure relief valve hose/tube (25) from the lower pressure relief valve tube (30) and let the fluid flow in the container.
NOTE: Use a second wrench to hold the lower pressure relief valve tube when you loosen the coupling nut on the higher pressure relief valve tube.
   (2) Disconnect the pressure relief valve hose/tube (25) from the pressure relief valve interface.
   (3) Remove the bolts (5), the washers (10), the nuts (15) and the clamps (20) that attach the pressure relief valve hose/tube (25) to the engine brackets at the flange STA.199(A2).
   (4) Remove the pressure relief valve hose/tube (25) from the engine.
   (5) Put COVER - PROTECTION on the pressure relief valve tube (30), the fitting on the top case drain hose/tube and the pressure relief valve hose/tube (25).
   (6) Put a CONTAINER 5 L (1.32 USGAL) below the lower pressure relief valve tube (30) to collect the remaining fluid.
   (7) Disconnect the lower pressure relief valve tube (30) from the top case drain hose/tube and let the fluid flow in the container.
NOTE: Use a second wrench to hold the fitting on the case drain tube when you loosen the coupling nut on the pressure relief valve tube.
   (8) If not done before, disconnect the lower pressure relief valve tube (30) from the upper pressure relief valve hose/tube (25).
NOTE: Use a second wrench to hold the lower pressure relief valve tube when you loosen the coupling nut on the higher pressure relief valve tube.
   (9) Remove the bolt (5), the washer (10), the nut (15) and the clamp (20) that attach the lower pressure relief valve tube to the engine bracket at the flange STA.199(A2).
   (10) Remove the bolt (5), the washer (10), the nut (15) and the clamp (20) that attach the lower pressure relief valve tube to the engine bracket at flange STA.185(B5).
   (11) Remove the lower pressure relief valve tube (30) from the engine.
   (12) Put COVER - PROTECTION on the lower pressure relief valve tube (30), the fitting on the top case drain hose/tube and the higher pressure relief valve hose/tube (25).
[Rev.10 from 2021] 2026.04.01 00:22:36 UTC