W DOC AIRBUS | AMM A320F

Reactivation of the HP Bleed Valve

TASK 36-11-00-440-803-A
Reactivation of the HP Bleed Valve

WARNING: MAKE SURE THAT THE PNEUMATIC SYSTEM IS DEPRESSURIZED BEFORE YOU START WORK. PRESSURIZED AIR CAN CAUSE INJURY TO PERSONNEL.
WARNING: PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU START A TASK ON OR NEAR:
  • THE FLIGHT CONTROLS
  • THE FLIGHT CONTROL SURFACES
  • THE LANDING GEAR AND THE RELATED DOORS
  • COMPONENTS THAT MOVE.
MOVEMENT OF COMPONENTS CAN KILL OR CAUSE INJURY TO PERSONS AND/OR CAN CAUSE DAMAGE TO THE EQUIPMENT.
WARNING: BE CAREFUL WHEN YOU DO WORK ON THE ENGINE PARTS AFTER THE ENGINE SHUTDOWN. USE APPLICABLE THERMAL GLOVES. THE ENGINE PARTS CAN STAY HOT FOR ONE HOUR AFTER SHUTDOWN AND CAN BURN YOU.
WARNING: YOU MUST NOT TOUCH HOT PARTS WITHOUT APPLICABLE GLOVES. HOT PARTS CAN CAUSE AN INJURY.
WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
1. Reason for the Job
MMEL 36-11-07B
ENGINE BLEED HP VALVE
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
1
ACCESS PLATFORM 1M(3 FT)
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
No specific
AR
WARNING NOTICE(S)
No specific
1
WRENCH - HEXAGONAL
No specific
Torque wrench: range to between 0.5 and 0.4 m.daN (44.25 and 35.40 lbf.in ) T
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
FOR [1000EM1] (ENGINE-1)
437AL, 438AR, 452AR
FOR [1000EM2] (ENGINE-2)
447AL, 448AR, 462AR
 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 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 31-60-00-860-001-A
EIS Start Procedure
TASK 31-60-00-860-002-A
EIS Stop Procedure
TASK 71-13-00-010-802-A
Opening of the Fan Cowl Doors
TASK 71-13-00-410-802-A
Closing of the Fan Cowl Doors
TASK 78-36-00-010-802-A
Opening of the Thrust Reverser Cowl-Doors
TASK 78-36-00-410-802-A
Closing of the Thrust Reverser Cowl-Doors
F High Pressure Regulator Valve
3. Job Set-up
Subtask 36-11-00-861-130-A ** ON A/C NOT FOR ALL
A. Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
Subtask 36-11-00-860-150-A ** ON A/C NOT FOR ALL
B. Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) (Ref. AMM TASK 31-60-00-860-001).
Subtask 36-11-00-941-133-A ** ON A/C NOT FOR ALL
C. Safety Precautions
   (1) Make sure that the engine 1(2) shutdown occurred not less than five minutes before you do this procedure.
   (2) On the AIR COND panel 30VU:
  • Make sure that the ENG 1(2) BLEED pushbutton switch is released (the OFF legend is on)
  • Make sure that the APU BLEED pushbutton switch is released (the ON legend is off)
  • Put a WARNING NOTICE(S) to tell persons not to operate the pneumatic system.
   (3) On the ENG panel 115VU:
  • Put a WARNING NOTICE(S) to tell persons not to start the engine 1(2).
   (4) ON the HP ground connector:
  • Put a WARNING NOTICE(S) to tell persons not to pressurize the pneumatic system.
   (5) 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) to tell persons not to energize the FADEC 1(2).
Subtask 36-11-00-865-105-A ** ON A/C NOT FOR ALL
D. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
FOR FIN: 1000EM1 (ENGINE1)
49VUAIR BLEED/APU BLEED VLV CTL/BMC1 OVRD11HVD14
49VUAIR BLEED/X FEED/VALVE/BAT2HVD13
49VUAIR BLEED/ENG 1/CTL2HA1D11
122VUAIR BLEED/ENG 1/MONG3HA1Z23
122VUAIR BLEED/X FEED VALVE/NORM1HVZ20
122VUAIR BLEED/APU BLEED VLV CTL/BMC2 OVRD12HVZ19
FOR FIN: 1000EM2 (ENGINE2)
49VUAIR BLEED/APU BLEED VLV CTL/BMC1 OVRD11HVD14
49VUAIR BLEED/X FEED/VALVE/BAT2HVD13
49VUAIR BLEED/ENG 2/MONG3HA2D12
122VUAIR BLEED/ENG 2/CTL2HA2Z22
122VUAIR BLEED/X FEED VALVE/NORM1HVZ20
122VUAIR BLEED/APU BLEED VLV CTL/BMC2 OVRD12HVZ19
Subtask 36-11-00-010-158-A ** ON A/C NOT FOR ALL
E. Get Access
   (1) Open the fan cowl doors (Ref. AMM TASK 71-13-00-010-802):
     (a) FOR [1000EM1] (ENGINE-1)
437AL 438AR
     (b) FOR [1000EM2] (ENGINE-2)
447AL 448AR.
   (2) Put in position a ACCESS PLATFORM 1M(3 FT).
Subtask 36-11-00-010-159-A ** ON A/C NOT FOR ALL
F. Open the right thrust-reverser cowl door (Ref. AMM TASK 78-36-00-010-802):
   (1) FOR [1000EM1] (ENGINE-1)
452AR
   (2) FOR [1000EM2] (ENGINE-2)
462AR.
4. Procedure
Subtask 36-11-00-440-094-A ** ON A/C NOT FOR ALL
A. Reactivation of the HP Bleed Valve (HPV) (4000HA)
CAUTION: MAKE SURE THAT THE PACKING IS IN POSITION WHEN YOU INSTALL THE LOCKING PIN ON ITS SUPPORT. THIS WILL PREVENT VENTING OF THE VALVE REGULATOR.
   (1) On the HPV (4000HA):
     (a) Use a WRENCH - HEXAGONAL to remove the locking pin from the override control in the HPV (4000HA).
     (b) Remove the locking pin from the override control to unlock the HPV (4000HA).
     (c) Install the locking pin on its storage position on the HPV (4000HA).
     (d) Use a WRENCH - HEXAGONAL to install the locking pin on the HPV (4000HA).
     (e) TORQUE the locking pin to between 0.5 and 0.4 m.daN (44.25 and 35.40 lbf.in ) T.
5. Close-up
Subtask 36-11-00-410-151-A ** ON A/C NOT FOR ALL
A. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Close the right thrust reverser cowl door (Ref. AMM TASK 78-36-00-410-802).
     (a) FOR [1000EM1] (ENGINE-1)
452AR
     (b) FOR [1000EM2] (ENGINE-2)
462AR.
Subtask 36-11-00-410-152-A ** ON A/C NOT FOR ALL
B. Close Access
   (1) Remove the access platform(s).
   (2) Close the fan cowl doors (Ref. AMM TASK 71-13-00-410-802):
     (a) FOR [1000EM1] (ENGINE-1)
437AL 438AR
     (b) FOR [1000EM2] (ENGINE-2)
447AL 448AR.
   (3) Remove the WARNING NOTICE(S).
Subtask 36-11-00-865-107-A ** ON A/C NOT FOR ALL
C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
FOR FIN: 1000EM1 (ENGINE1)
49VUAIR BLEED/APU BLEED VLV CTL/BMC1 OVRD11HVD14
49VUAIR BLEED/X FEED/VALVE/BAT2HVD13
49VUAIR BLEED/ENG 1/CTL2HA1D11
122VUAIR BLEED/ENG 1/MONG3HA1Z23
122VUAIR BLEED/X FEED VALVE/NORM1HVZ20
122VUAIR BLEED/APU BLEED VLV CTL/BMC2 OVRD12HVZ19
FOR FIN: 1000EM2 (ENGINE2)
49VUAIR BLEED/APU BLEED VLV CTL/BMC1 OVRD11HVD14
49VUAIR BLEED/X FEED/VALVE/BAT2HVD13
49VUAIR BLEED/ENG 2/MONG3HA2D12
122VUAIR BLEED/ENG 2/CTL2HA2Z22
122VUAIR BLEED/X FEED VALVE/NORM1HVZ20
122VUAIR BLEED/APU BLEED VLV CTL/BMC2 OVRD12HVZ19
Subtask 36-11-00-440-106-A ** ON A/C NOT FOR ALL
D. Reactivation of the HP Bleed Valve
   (1) On the ECAM control panel, push the BLEED key (on the lower ECAM DU, the BLEED page comes into view).
     (a) On the lower ECAM DU, on the BLEED page:
  • Make sure that the related HP bleed-valve symbol shows closed in green.
Subtask 36-11-00-860-151-A ** ON A/C NOT FOR ALL
E. Do the EIS stop procedure
(Ref. AMM TASK 31-60-00-860-002).
Subtask 36-11-00-869-121-A ** ON A/C NOT FOR ALL
F. Aircraft Maintenance Configuration
   (1) On the AIR COND panel 30VU:
  • Push the ENG 1(2) BLEED pushbutton switch (the OFF legend is off).
Subtask 36-11-00-862-116-A ** ON A/C NOT FOR ALL
G. De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
[Rev.10 from 2021] 2026.04.01 01:06:32 UTC
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