W DOC AIRBUS | AMM A320F

Installation of the High Pressure Compressor (HPC) Bleed Valve Air Pressure Sensor (Passive) [PW11]


TASK 75-32-21-400-801-A
Installation of the High Pressure Compressor (HPC) Bleed Valve Air Pressure Sensor (Passive)


WARNING: BE CAREFUL WHEN YOU DO WORK ON THE ENGINE AND THE ADJACENT COMPONENTS AFTER ENGINE SHUTDOWN. THE ENGINE, THE ENGINE OIL AND THE ADJACENT COMPONENTS CAN STAY HOT FOR A LONG TIME. IF YOU DO NOT OBEY THIS INSTRUCTION, INJURY CAN OCCUR.
FIN: 4058KS ** ON A/C NOT FOR ALL
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 1M(3 FT)
No specific
1
PLIERS - JAWED, SOFT
No specific
Torque wrench: range to between 100 and 90 lbf.in (1.13 and 1.02 m.daN ) T
No specific
Torque wrench: range to between 110 and 100 lbf.in (1.24 and 1.13 m.daN ) T
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENG 1)
437AL, 438AR, 451AL
FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENG 2)
447AL, 448AR, 461AL
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 71-00-00-860-832-A
Procedure to Prevent Engine Motoring and to Stop the Electrical Supply to the EEC
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 73-21-00-710-807-A
Test No.6 - EEC Operation Test (Idle Test)
TASK 73-25-34-400-802-A
Installation of the Engine Interface Unit (EIU)
TASK 78-30-00-040-805-A
Deactivation of the Thrust Reverser System for Ground Maintenance
TASK 78-30-00-440-805-A
Reactivation of the Thrust Reverser System after Ground Maintenance
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
3. Job Set-up
Subtask 75-32-21-941-051-A ** ON A/C NOT FOR ALL
A. Safety Precautions
   (1) Make sure that you did the procedure to prevent engine motoring and to stop the electrical supply to the Electronic Engine Control (EEC)
(Ref. AMM TASK 71-00-00-860-832).
Subtask 75-32-21-010-052-A ** ON A/C NOT FOR ALL
B. Get Access
   (1) Make sure that the fan cowl doors are open (Ref. AMM TASK 71-13-00-010-802):
     (a) FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENG 1)
437AL, 438AR
     (b) FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENG 2)
447AL, 448AR
Subtask 75-32-21-040-051-A ** ON A/C NOT FOR ALL
C. Deactivation of the Thrust Reverser System for Ground Maintenance
WARNING: YOU MUST DEACTIVATE THE THRUST REVERSER BEFORE YOU DO WORK ON OR AROUND IT. IF YOU DO NOT, THE THRUST REVERSER CAN OPERATE ACCIDENTALLY AND CAUSE AN INJURY AND/OR DAMAGE.
   (1) Make sure that you did the deactivation of the thrust reverser system for ground maintenance (Ref. AMM TASK 78-30-00-040-805).
Subtask 75-32-21-010-053-A ** ON A/C NOT FOR ALL
D. Get Access
   (1) Make sure that the left thrust reverser cowl-door is open (Ref. AMM TASK 78-36-00-010-802):
     (a) FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENG 1)
451AL
     (b) FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENG 2)
461AL
   (2) Make sure that the ACCESS PLATFORM 1M(3 FT) is in position.
4. Procedure
CAUTION: WIPE CLEAN ALL PARTS AND TOOLS AS NECESSARY TO REMOVE UNWANTED DEBRIS AND PREVENT DAMAGE TO THE ENGINE.
Subtask 75-32-21-420-050-A ** ON A/C NOT FOR ALL
A. Installation of the High Pressure Compressor (HPC) Bleed Valve Air Pressure Sensor (Passive)
   (1) Removal of the protection covers
CAUTION: REMOVE THE PROTECTION COVERS FROM THE OPENINGS AS NECESSARY TO PREVENT ENGINE DAMAGE.
     (a) Make sure that you remove all the necessary COVER - PROTECTION to prevent damage to the engine.
   (2) Install the HPC bleed valve air pressure sensor (passive) (2) on the Compressor Intermediate Case (CIC) firewall at approximately the 10 o'clock position as follows:
     (a) Install the sensor (2) onto the CIC firewall bracket with the two bolts (1).
     (b) TORQUE the two bolts (1) to between 100 and 90 lbf.in (1.13 and 1.02 m.daN ) T.
     (c) Connect the (AS33) manifold B-nut to the sensor (2).
CAUTION: USE A SECOND WRENCH TO HOLD THE MATING PARTS WHEN YOU LOOSEN OR TIGHTEN THE TUBE OR HOSE NUTS. IF YOU DO NOT OBEY THIS CAUTION, YOU CAN TWIST OR CAUSE DAMAGE TO THE TUBES OR HOSES.
       1 TORQUE the (AS33) manifold B-nut to between 110 and 100 lbf.in (1.24 and 1.13 m.daN )
T.
   (3) Connect the (WC10) wiring harness connector (P53) to the sensor (2) receptacle (J56) as follows:
     (a) Examine, align and engage the connector.
     (b) Push lightly inward on the connector while you tighten the coupling ring.
     (c) Use the PLIERS - JAWED, SOFT and tighten the connector against the receptacle.
     (d) Make sure that you can feel the ratchet feature.
     (e) While you tighten, push the connector in and from side to side.
     (f) Tighten the connector until the PLIERS - JAWED, SOFT slip on the connector ring.
   (4) Examine the assembly for foreign objects, damage, and correct assembly.
5. Close-up
Subtask 75-32-21-410-050-A ** ON A/C NOT FOR ALL
Subtask 75-32-21-440-050-A ** ON A/C NOT FOR ALL
B. Do the reactivation of the thrust reverser system after ground maintenance (Ref. AMM TASK 78-30-00-440-805).
Subtask 75-32-21-410-051-A ** ON A/C NOT FOR ALL
C. Close Access
   (1) Close the fan cowl doors (Ref. AMM TASK 71-13-00-410-802):
     (a) FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENG 1)
437AL 438AR
     (b) FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENG 2)
447AL 448AR
   (2) Remove the access platform(s).
   (3) Remove the WARNING NOTICE(S).
   (4) Make sure that all the circuit breakers shown in the paragraph Procedure of the engine interface unit installation are closed. If they are not, close them in the recommended sequence
(Ref. AMM TASK 73-25-34-400-802).
Subtask 75-32-21-720-050-A ** ON A/C NOT FOR ALL
D. Test
   (1) Do the test No. 6 - EEC - Idle test (Ref. AMM TASK 73-21-00-710-807).
[Rev.10 from 2021] 2026.04.01 03:13:51 UTC