W DOC AIRBUS | AMM A320F

Reactivation of the Bleed Pressure Regulator Valve


TASK 36-11-00-440-001-A
Reactivation of the Bleed Pressure Regulator Valve


WARNING: MAKE SURE THAT THE PNEUMATIC SYSTEM IS DEPRESSURIZED BEFORE YOU START WORK. PRESSURIZED AIR CAN CAUSE INJURY TO PERSONNEL.
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: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
FIN: 1000EM1 ** ON A/C NOT FOR ALL
FIN: 1000EM2 ** ON A/C NOT FOR ALL
FIN: 4001HA ** ON A/C NOT FOR ALL
1. Reason for the Job
MMEL 36-11-02A
ENGINE BLEED VALVE (PRV)
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
AR
ACCESS PLATFORM 1M (3 FT)-ADJUSTABLE
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
No specific
AR
WARNING NOTICE(S)
No specific
Torque wrench: range to between 0.6 and 0.4 m.daN (53.10 and 35.40 lbf.in ) T
No specific
Torque wrench: range to between 0.7 and 0.6 m.daN (61.95 and 53.10 lbf.in ) T
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.14QEB1)
Wire-Locking Dia: 0.6 mm CRES Nickel Alloy -
(Material No.357500)
NEVERSEEZ REGULAR GRADE
(Material No.357700)
NEVER-SEEZ PURE NICKEL SPECIAL
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
FOR [1000EM1] (ENGINE-1)
437AL, 438AR, 451AL
452AR
FOR [1000EM2] (ENGINE-2)
447AL, 448AR, 461AL
462AR
 D. Expendable Parts
FIG.ITEM
DESIGNATION
IPC-CSN
2
PACKING
AIPC 36-11-52-01-030
3
PACKING
AIPC 36-11-52-01-150
 E. 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 71-13-00-010-010-A
Opening of the Fan Cowls 437AL(447AL),438AR(448AR)
TASK 71-13-00-010-040-A
Opening of the Fan Cowl Doors
TASK 71-13-00-010-040-B
Opening of the Fan Cowl Doors
TASK 71-13-00-410-010-A
Closing of the Fan Cowls 437AL(447AL),438AR(448AR)
TASK 71-13-00-410-040-A
Closing of the Fan Cowl Doors
TASK 71-13-00-410-040-B
Closing of the Fan Cowl Doors
TASK 78-30-00-040-012-A
Deactivation of the Thrust Reverser Hydraulic Control Unit (HCU) for Ground Maintenance
TASK 78-30-00-081-041-A
Make the Thrust Reverser Serviceable after Maintenance
TASK 78-30-00-081-041-B
Make the Thrust Reverser Serviceable after Maintenance
TASK 78-30-00-440-012-A
Re-activation of the Thrust Reverser Hydraulic Control Unit (HCU) after Ground Maintenance
TASK 78-30-00-481-041-A
Make the Thrust Reverser Unserviceable for Maintenance
TASK 78-30-00-481-041-B
Make the Thrust Reverser Unserviceable for Maintenance
TASK 78-32-00-010-010-A
Opening of the Thrust Reverser Halves
TASK 78-32-00-410-010-A
Closing of the Thrust Reverser Halves
TASK 78-36-00-010-040-A
Opening of the Thrust Reverser Doors
TASK 78-36-00-010-040-B
Opening of the Thrust Reverser Doors
TASK 78-36-00-410-040-A
Closing of the Thrust Reverser Doors
TASK 78-36-00-410-040-B
Closing of the Thrust Reverser Doors
F Bleed-Pressure Regulator Valve ** ON A/C NOT FOR ALL
F Bleed-Pressure Regulator Valve ** ON A/C NOT FOR ALL
3. Job Set-up
Subtask 36-11-00-861-068-A ** ON A/C NOT FOR ALL
A. Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
Subtask 36-11-00-941-054-A ** ON A/C NOT FOR ALL
B. Safety Precautions
   (1) Make sure that the engine 1(2) is shut down occurred not less than 5 minutes.
   (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 36-11-00-865-065-A ** ON A/C NOT FOR ALL
C. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUAIR BLEED/ENG 1/CTL3HA1D12
49VUAIR BLEED/ENG 1/MONG2HA1D11
122VUAIR BLEED/ENG 2/CTL3HA2Z23
122VUAIR BLEED/ENG 2/MONG2HA2Z22
Subtask 36-11-00-010-051-A ** ON A/C NOT FOR ALL
D. Get Access
   (1) Open the fan cowl doors (Ref. AMM TASK 71-13-00-010-040):
     (a) FOR [1000EM1] (ENGINE-1)
437AL 438AR
     (b) FOR [1000EM2] (ENGINE-2)
447AL 448AR
   (2) Put the ACCESS PLATFORM 1M (3 FT)-ADJUSTABLE in position below the engine.
Subtask 36-11-00-040-051-A ** ON A/C NOT FOR ALL
E. Make the thrust reverser unserviceable (Ref. AMM TASK 78-30-00-481-041).
Subtask 36-11-00-010-072-A ** ON A/C NOT FOR ALL
F. Open the left thrust-reverser cowl door (Ref. AMM TASK 78-36-00-010-040):
   (1) FOR [1000EM1] (ENGINE-1)
451AL
   (2) FOR [1000EM2] (ENGINE-2)
461AL
Subtask 36-11-00-010-051-B ** ON A/C NOT FOR ALL
G. Get Access
   (1) Open the fan cowls (Ref. AMM TASK 71-13-00-010-010):
     (a) FOR [1000EM1] (ENGINE-1)
437AL 438AR
     (b) FOR [1000EM2] (ENGINE-2)
447AL 448AR
   (2) Put the ACCESS PLATFORM 1M (3 FT)-ADJUSTABLE in to position below the engine.
Subtask 36-11-00-040-051-B ** ON A/C NOT FOR ALL
H. Deactivate the Thrust Reverser
WARNING: MAKE SURE THAT THE THRUST REVERSER HYDRAULIC CONTROL UNIT (HCU) IS DEACTIVATED BEFORE YOU DO WORK ON OR AROUND THE THRUST REVERSER. IF THE HCU IS NOT DEACTIVATED, THERE IS A RISK OF UNWANTED THRUST REVERSER OPERATION WHICH CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT.
   (1) Deactivate the thrust reverser Hydraulic Control Unit (HCU) (Ref. AMM TASK 78-30-00-040-012).
Subtask 36-11-00-010-072-B ** ON A/C NOT FOR ALL
I. Open the thrust reverser halves (Ref. AMM TASK 78-32-00-010-010):
   (1) FOR [1000EM1] (ENGINE-1)
451AL 452AR
   (2) FOR [1000EM2] (ENGINE-2)
461AL 462AR
Subtask 36-11-00-010-051-C ** ON A/C NOT FOR ALL
J. Get Access
   (1) Open the fan cowl doors (Ref. AMM TASK 71-13-00-010-040):
     (a) FOR [1000EM1] (ENGINE-1)
437AL 438AR
     (b) FOR [1000EM2] (ENGINE-2)
447AL 448AR.
   (2) Put the ACCESS PLATFORM 1M (3 FT)-ADJUSTABLE in position below the engine.
Subtask 36-11-00-040-051-C ** ON A/C NOT FOR ALL
K. Make the thrust reverser unserviceable (Ref. AMM TASK 78-30-00-481-041).
Subtask 36-11-00-010-072-C ** ON A/C NOT FOR ALL
L. Open the left thrust-reverser cowl door (Ref. AMM TASK 78-36-00-010-040):
   (1) FOR [1000EM1] (ENGINE-1)
451AL
   (2) FOR [1000EM2] (ENGINE-2)
461AL.
4. Procedure
Subtask 36-11-00-440-057-A ** ON A/C NOT FOR ALL
A. Reactivation of the Bleed Pressure Regulator Valve
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 bleed-pressure regulator valve P/N 6774B02 and 6714D01 to 6714D06:
F Bleed-Pressure Regulator Valve ** ON A/C NOT FOR ALL
F Bleed-Pressure Regulator Valve ** ON A/C NOT FOR ALL
     (a) Remove the knurled screw (1) from the override control to unlock the valve.
     (b) Install the washer (2) on the knurled screw (1).
     (c) Install the knurled screw (1) as follows:
CAUTION: BEFORE YOU INSTALL THE LOCKING PIN OR SAFETY SCREW OR SPECIAL SCREW OR KNURLED SCREW, YOU MUST APPLY NEVER-SEEZ REGULAR GRADE. IF YOU DO NOT APPLY IT, YOU CAN CAUSE DAMAGE TO THE MANUAL OVERRIDE CONTROL OF THE VALVE.
       1 Apply NEVERSEEZ REGULAR GRADE (Material No.357500) or NEVER-SEEZ PURE NICKEL SPECIAL (Material No.357700) on the knurled screw (1).
       2 Install the knurled screw (1) on its storage port.
       3 Tighten the knurled screw (1) with your hand.
     (d) Install the lockwire as follows:
WARNING: USE PROTECTIVE GOGGLES AND GLOVES WHEN YOU REMOVE OR INSTALL LOCKWIRE. EACH TIME YOU CUT LOCKWIRE, REMOVE AND DISCARD IT IMMEDIATELY. LOOSE LOCKWIRE CAN CUT YOU OR MAKE YOU BLIND, AND/OR CAN CAUSE DAMAGE.
       1 Safety the knurled screw (1) with 14QEB1Wire-Locking Dia: 0.6 mm CRES Nickel Alloy -.
   (2) On bleed-pressure regulator valve P/N 6774B03 and 6714D07:
     (a) Remove the safety screw (1) from the override control to unlock the valve.
     (b) Install the washer (2) on the safety screw (1).
     (c) Install the safety screw (1) as follows:
CAUTION: BEFORE YOU INSTALL THE LOCKING PIN OR SAFETY SCREW OR SPECIAL SCREW OR KNURLED SCREW, YOU MUST APPLY NEVER-SEEZ REGULAR GRADE. IF YOU DO NOT APPLY IT, YOU CAN CAUSE DAMAGE TO THE MANUAL OVERRIDE CONTROL OF THE VALVE.
       1 Apply NEVERSEEZ REGULAR GRADE (Material No.357500) or NEVER-SEEZ PURE NICKEL SPECIAL (Material No.357700) on the safety screw (1).
       2 Install the safety screw (1) on its storage port.
       3 TORQUE the safety screw (1) to between 0.7 and 0.6 m.daN (61.95 and 53.10 lbf.in ) T.
     (d) Install the lockwire as follows:
WARNING: USE PROTECTIVE GOGGLES AND GLOVES WHEN YOU REMOVE OR INSTALL LOCKWIRE. EACH TIME YOU CUT LOCKWIRE, REMOVE AND DISCARD IT IMMEDIATELY. LOOSE LOCKWIRE CAN CUT YOU OR MAKE YOU BLIND, AND/OR CAN CAUSE DAMAGE.
       1 Safety the safety screw (1) with 14QEB1Wire-Locking Dia: 0.6 mm CRES Nickel Alloy -.
   (3) On bleed-pressure regulator valve P/N 6774E:
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.
     (a) Remove the special screw (1) from the override control to unlock the valve.
     (b) Install the washer (2) on the special screw (1).
     (c) Install a new AIPC 36-11-52-01-150 PACKING (3).
     (d) Install the special screw (1) as follows:
CAUTION: BEFORE YOU INSTALL THE LOCKING PIN OR SAFETY SCREW OR SPECIAL SCREW OR KNURLED SCREW, YOU MUST APPLY NEVER-SEEZ REGULAR GRADE. IF YOU DO NOT APPLY IT, YOU CAN CAUSE DAMAGE TO THE MANUAL OVERRIDE CONTROL OF THE VALVE.
       1 Apply NEVERSEEZ REGULAR GRADE (Material No.
357500) or NEVER-SEEZ PURE NICKEL SPECIAL (Material No.357700) on the special screw (1).
       2 Install the special screw (1) on its storage port with washer (2).
       3 Tighten the special screw (1) with your hand.
     (e) Install the lockwire as follows:
WARNING: USE PROTECTIVE GOGGLES AND GLOVES WHEN YOU REMOVE OR INSTALL LOCKWIRE. EACH TIME YOU CUT LOCKWIRE, REMOVE AND DISCARD IT IMMEDIATELY. LOOSE LOCKWIRE CAN CUT YOU OR MAKE YOU BLIND, AND/OR CAN CAUSE DAMAGE.
       1 Safety the special screw (1) with 14QEB1Wire-Locking Dia: 0.6 mm CRES Nickel Alloy -.
   (4) On bleed-pressure regulator valve P/N 6774F and P/N 6774G:
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.
     (a) Remove the safety screw (1) from the override control to unlock the valve.
     (b) Install a new AIPC 36-11-52-01-030 PACKING (2).
     (c) Install the safety screw (1) as follows:
CAUTION: BEFORE YOU INSTALL THE LOCKING PIN OR SAFETY SCREW OR SPECIAL SCREW OR KNURLED SCREW, YOU MUST APPLY NEVER-SEEZ REGULAR GRADE. IF YOU DO NOT APPLY IT, YOU CAN CAUSE DAMAGE TO THE MANUAL OVERRIDE CONTROL OF THE VALVE.
       1 Apply NEVERSEEZ REGULAR GRADE (Material No.
357500) or NEVER-SEEZ PURE NICKEL SPECIAL (Material No.357700) on the safety screw (1).
       2 Install the safety screw (1) on its storage port.
       3 TORQUE the safety screw (1) to between 0.6 and 0.4 m.daN (53.10 and 35.40 lbf.in ) T.
     (d) Install the lockwire as follows:
WARNING: USE PROTECTIVE GOGGLES AND GLOVES WHEN YOU REMOVE OR INSTALL LOCKWIRE. EACH TIME YOU CUT LOCKWIRE, REMOVE AND DISCARD IT IMMEDIATELY. LOOSE LOCKWIRE CAN CUT YOU OR MAKE YOU BLIND, AND/OR CAN CAUSE DAMAGE.
       1 Safety the safety screw (1) with 14QEB1Wire-Locking Dia: 0.6 mm CRES Nickel Alloy -.
   (5) On the AIR COND panel 30VU:
  • Push the ENG 1 (2) BLEED pushbutton switch (the OFF legend is off).
5. Close-up
Subtask 36-11-00-865-066-A ** ON A/C NOT FOR ALL
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUAIR BLEED/ENG 1/CTL3HA1D12
49VUAIR BLEED/ENG 1/MONG2HA1D11
122VUAIR BLEED/ENG 2/CTL3HA2Z23
122VUAIR BLEED/ENG 2/MONG2HA2Z22
Subtask 36-11-00-410-051-A ** ON A/C NOT FOR ALL
Subtask 36-11-00-440-051-A ** ON A/C NOT FOR ALL
C. Make the thrust reverser serviceable (Ref. AMM TASK 78-30-00-081-041).
Subtask 36-11-00-410-071-A ** ON A/C NOT FOR ALL
D. Close Access
   (1) Close the fan cowl doors (Ref. AMM TASK 71-13-00-410-040):
     (a) FOR [1000EM1] (ENGINE-1)
437AL 438AR
     (b) FOR [1000EM2] (ENGINE-2)
447AL 448AR
   (2) Remove the access platform(s).
   (3) Remove the WARNING NOTICE(S).
Subtask 36-11-00-410-051-B ** ON A/C NOT FOR ALL
E. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Close the thrust-reverser cowl doors (Ref. AMM TASK 78-32-00-410-010):
     (a) FOR [1000EM1] (ENGINE-1)
451AL 452AR
     (b) FOR [1000EM2] (ENGINE-2)
461AL 462AR
Subtask 36-11-00-440-051-B ** ON A/C NOT FOR ALL
F. Activate the thrust reverser HCU (Ref. AMM TASK 78-30-00-440-012).
Subtask 36-11-00-410-071-B ** ON A/C NOT FOR ALL
G. Close Access
   (1) Close the fan cowls (Ref. AMM TASK 71-13-00-410-010):
     (a) FOR [1000EM1] (ENGINE-1)
437AL 438AR
     (b) FOR [1000EM2] (ENGINE-2)
447AL 448AR
   (2) Remove the WARNING NOTICE(S).
   (3) Remove the access platform(s).
Subtask 36-11-00-410-051-C ** ON A/C NOT FOR ALL
H. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Close the left thrust-reverser cowl door (Ref. AMM TASK 78-36-00-410-040):
     (a) FOR [1000EM1] (ENGINE-1)
451AL
     (b) FOR [1000EM2] (ENGINE-2)
461AL.
Subtask 36-11-00-440-051-C ** ON A/C NOT FOR ALL
I. Make the thrust reverser serviceable (Ref. AMM TASK 78-30-00-081-041).
Subtask 36-11-00-410-071-C ** ON A/C NOT FOR ALL
J. Close Access
   (1) Close the fan cowl doors (Ref. AMM TASK 71-13-00-410-040):
     (a) FOR [1000EM1] (ENGINE-1)
437AL 438AR
     (b) FOR [1000EM2] (ENGINE-2)
447AL 448AR.
   (2) Remove the access platform(s).
   (3) Remove the WARNING NOTICE(S).
Subtask 36-11-00-862-068-A ** ON A/C NOT FOR ALL
K. De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
[Rev.10 from 2021] 2026.04.01 01:06:19 UTC