W DOC AIRBUS | TSM A320F

Bleed Pressure-Regulator Valve of the Engine 2 Blocked in the Closed Position or Regulation Too Low


TASK 36-11-00-810-810-A
Bleed Pressure-Regulator Valve of the Engine 2 Blocked in the Closed Position or Regulation Too Low


1. Possible Causes
  • BMC-2 [1HA2]
  • VALVE-BLEED PRESS REG [4001HA]
  • sense line between the bleed-pressure regulator valve (4001HA) and the solenoid (10HA2)
  • O-RING
  • SOLENOID-BLEED PRESS REG V CTL, ENG 2 [10HA2]
  • XDCR-BLEED REGULATED PRESS, ENG 2 [8HA2]
  • XDCR-BLEED TRANSFER PRESS, ENG 2 [7HA2]
  • VALVE-HP BLEED [4000HA]
  • P/BSW-ENG 2 BLEED [4HA2]
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
1
CAP - BLANKING
 B. Referenced Information
REFERENCE
DESIGNATION
ESPM 204511
AMM 36-11-00-720-007
Functional Test of the Sense Lines Connected to the Bleed Pressure-Regulator Valve with the Bleed Test Set P/N 98D36003000000
AMM 36-11-00-740-001
BITE Test of the BMC 1(2)
AIPC 36110606
AMM 36-11-15-000-001
Removal of the Bleed Transferred Pressure-Transducer
AMM 36-11-15-400-001
Installation of the Bleed Transferred Pressure-Transducer
AMM 36-11-16-000-001
Removal of the Bleed Regulated Pressure-Transducer
AMM 36-11-16-400-001
Installation of the Bleed Regulated Pressure-Transducer
AMM 36-11-49-000-029
Removal of the Pneumatic Sense Lines in the Pylon
AMM 36-11-49-000-820
Removal of the Pneumatic Sense Lines in the Pylon
AMM 36-11-49-400-029
Installation of the Pneumatic Sense Lines in the Pylon
AMM 36-11-49-400-820
Installation of the Pneumatic Sense Lines in the Pylon
AMM 36-11-51-000-040
Removal of the High Pressure Bleed Valve
AMM 36-11-51-000-042
Removal of the High Pressure Bleed Valve
AMM 36-11-51-400-040
Installation of the High Pressure Bleed Valve
AMM 36-11-51-400-042
Installation of the High Pressure Bleed Valve
AMM 36-11-52-000-040
Removal of the Bleed Pressure-Regulator Valve
AMM 36-11-52-000-042
Removal of the Bleed Pressure Regulator Valve
AMM 36-11-52-400-040
Installation of the Bleed Pressure-Regulator Valve
AMM 36-11-52-400-042
Installation of the Bleed Pressure Regulator Valve
AMM 36-11-52-720-001
Functional Test of the Opening of the Bleed-Pressure Regulator Valve (PRV) with the Bleed Test Set P/N 98D36003000000
AMM 36-11-55-000-001
Removal of the Bleed-Pressure-Regulator Valve Control-Solenoid
AMM 36-11-55-400-001
Installation of the Bleed-Pressure-Regulator Valve Control-Solenoid
AMM 36-11-58-100-803
Cleaning of the Sense Line between the HP Bleed-Override Solenoid and the Pressure Regulating Valve (PRV)
3. Fault Confirmation
Subtask 36-11-00-710-052-A ** ON A/C NOT FOR ALL
A. Test
   (1) Do the BITE test of the BMC2 AMM 36-11-00-740-001.
4. Fault Isolation
CAUTION: BE CAREFUL WITH THE SEMI-FLEXIBLE SENSE LINE. DEFORMATION OF THE RIGID PART OR LARGE DEFORMATION OF THE FLEXIBLE PART CAN QUICKLY CAUSE LEAKAGE.
CAUTION: USE TWO WRENCHES DURING DISCONNECTION OF THE SENSE LINE, ONE TO MAINTAIN THE FIXED NUT AND THE SECOND ONE TO LOOSEN/TIGHTEN THE SENSE LINE COUPLING.
Subtask 36-11-00-810-266-A ** ON A/C NOT FOR ALL
A. If the BITE test gives a fault message related to the BMC-2 [1HA2]
  • Do the related trouble shooting procedure.
Subtask 36-11-00-810-051-H ** ON A/C NOT FOR ALL
DELETED
Subtask 36-11-00-810-051-I ** ON A/C NOT FOR ALL
B. If the test do not give a fault message related to the BMC2 and if the fault is identified by the maintenance message
PRESS REG-V 4001HA2 OR SOL 10HA2 OR SENSE LINE:
  • Do a check of the sense line unions and the clamps between the bleed- pressure regulator valve (4001HA) and the solenoid (10HA2).
   (1) If the unions are loose:
  • Tighten them.
   (2) If the unions are correctly tightened:
     (a) If the bleed-pressure regulator valve does not open:
     (b) If the bleed-pressure regulator valve opens:
  • Do a leakage check of the sense line between the bleed-pressure regulator valve and the control solenoid of the bleed-pressure regulator valve AMM 36-11-00-720-007.
       1 If the pressure decreases very slowly:
       2 If the pressure decreases to 0 bar (0 psi) in less than 20 seconds:
  • Do an internal leak check of the control solenoid bleed-pressure regulator valve.
  • Disconnect the sense line at the control solenoid of the bleed-pressure regulator valve.
  • Put a CAP - BLANKING on the sense line.
  • Pressurize the sense line to 2.07 bar (30 psi), then close the shutoff valve of the pressure source.
         a If the pressure decreases:
         b If the pressure stays constant:
  • Remove the bleed-pressure-regulator valve control-solenoid AMM 36-11-55-000-001.
  • Do a visual inspection of the O-ring at the bottom of the bleed-pressure-regulator valve control-solenoid.
    * If the O-ring is damaged:
    ** Install a new O-RING AIPC 36110606.
    ** Install the bleed-pressure-regulator valve control-solenoid AMM 36-11-55-400-001.
    * If the O-ring has no damage:
    ** Install a new O-RING AIPC 36110606.
    ** Replace the SOLENOID-BLEED PRESS REG V CTL, ENG 2 [10HA2] AMM 36-11-55-400-001.
   (3) If the fault continues:
  • Do a check of the correct indication of the bleed-regulated pressure transducer (8HA2).
  • On the AIR control panel 30VU, push the APU BLEED pushbutton switch and set the X-BLEED selector switch to OPEN.
  • On the ECAM BLEED page, do a check of the pressure indications of the two systems.
     (a) If the pressure indication of the defective system is a minimum of 0.55 bar (8 psi) less than the indication of the opposite system:
       1 If the fault continues:
   (4) If the fault continues:
   (5) If the fault continues:
Subtask 36-11-00-810-051-L ** ON A/C NOT FOR ALL
B. If the test do not give a fault message related to the BMC2 and if the fault is identified by the maintenance message
PRESS REG-V 4001HA2 or SOL 10HA2 or SENSE LINE:
  • Do a check of the sense line unions and the clamps between the bleed-pressure regulator valve (4001HA) and the solenoid (10HA2).
   (1) If the unions are loose:
  • Tighten them.
   (2) If the unions are correctly tightened:
     (a) If the bleed-pressure regulator valve does not open:
  • Do the cleaning of the sense line between the HP bleed-override solenoid and the bleed-pressure regulator valve AMM 36-11-58-100-803.
  • Do a check of the opening of the bleed-pressure regulator valve AMM 36-11-52-720-001.
       1 If the bleed-pressure regulator valve does not open:
     (b) If the bleed-pressure regulator valve opens:
  • Do a leak check of the sense line between the bleed-pressure regulator valve and the control solenoid of the bleed-pressure regulator valve AMM 36-11-00-720-007.
       1 If the pressure decreases very slowly:
       2 If the pressure decreases to 0 bar (0 psi) in less than 20 seconds:
  • Do an internal leak check of the control solenoid of the bleed-pressure regulator valve.
  • Disconnect the sense line at the control solenoid of the bleed-pressure regulator valve.
  • Put a CAP - BLANKING on the sense line.
  • Pressurize the sense line to 2.07 bar (30 psi), then close the shutoff valve of the pressure source.
         a If the pressure decreases:
         b If the pressure stays constant:
  • Remove the bleed-pressure-regulator valve control-solenoid AMM 36-11-55-000-001.
  • Do a visual inspection of the O-ring at the bottom of the bleed-pressure-regulator valve control-solenoid.
    * If the O-ring is damaged:
    ** Install a new O-RING AIPC 36110606.
    ** Install the bleed-pressure-regulator valve control-solenoid AMM 36-11-55-400-001.
    * If the O-ring has no damage:
    ** Install a new O-RING AIPC 36110606.
    ** Replace the SOLENOID-BLEED PRESS REG V CTL, ENG 2 [10HA2] AMM 36-11-55-400-001.
   (3) If the fault continues:
  • Do a check of the correct indication of the bleed-regulated pressure transducer (8HA2).
  • On the AIR control panel 30VU, push the APU BLEED pusbhutton switch and set the X-BLEED selector switch to OPEN.
  • On the ECAM BLEED page, do a check of the pressure indications of the two systems.
     (a) If the pressure indication of the defective system is a minimum of 0.55 bar (8 psi) less than the indication of the opposite system:
       1 If the fault continues:
   (4) If the fault continues:
   (5) If the fault continues:
Subtask 36-11-00-710-053-A ** ON A/C NOT FOR ALL
C. After the subsequent flight, make sure that the fault does not continue.
[Rev.8 from Aug 2018] 2026.04.04 04:39:59 UTC