W DOC AIRBUS | AMM A320F

Installation of the HPC Bleed Valve [PW11]


TASK 75-32-02-400-801-A
Installation of the HPC Bleed Valve


WARNING: BE CAREFUL WHEN YOU DO WORK ON THE ENGINE AFTER SHUTDOWN. THE ENGINE CAN STAY HOT FOR A LONG TIME. IF YOU DO NOT OBEY THIS INSTRUCTION, INJURY CAN OCCUR.
WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
FIN: 4102JM ** ON A/C NOT FOR ALL
1. Reason for the Job
Use this procedure to install the High Pressure Compressor (HPC) bleed 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
Torque wrench: range to between 70 and 60 lbf.in (0.79 and 0.68 m.daN ) T
No specific
Torque wrench: range to between 225 and 200 lbf.in (2.54 and 2.26 m.daN ) T
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.P05-395)
beeswax
(Material No.P05-396)
Paraffin wax blend (PMC 9462)
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENG 1)
437AL, 438AR, 451AL, 452AR
FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENG 2)
447AL, 448AR, 461AL, 462AR
 D. Expendable Parts
FIG.ITEM
DESIGNATION
IPC-CSN
2
GASKET
EIPC 75-32-02-01-090
 E. Referenced Information
REFERENCE
DESIGNATION
TASK 71-00-00-720-811-A
Test No. 3A - Idle Power Test
TASK 71-00-00-860-833-A
Procedure to Prevent Engine Motoring
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 78-30-00-040-805-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 75-32-02-941-051-A ** ON A/C NOT FOR ALL
A. Safety Precautions
   (1) Make sure that you did the procedure to prevent engine motoring
(Ref. AMM TASK 71-00-00-860-833)
Subtask 75-32-02-010-052-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
   (2) Make sure that the ACCESS PLATFORM 1M(3 FT) is in position.
Subtask 75-32-02-040-051-A ** ON A/C NOT FOR ALL
C. Deactivation of the Thrust Reverser System for 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 maintenance (Ref. AMM TASK 78-30-00-040-805).
Subtask 75-32-02-010-053-A ** ON A/C NOT FOR ALL
D. Get Access
   (1) Make sure that the thrust reverser cowl-doors are open (Ref. AMM TASK 78-36-00-010-802):
     (a) FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENG 1)
451AL, 452AR
     (b) FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENG 2)
461AL, 462AR
4. Procedure
Subtask 75-32-02-420-050-A ** ON A/C NOT FOR ALL
A. Installation of the HPC Bleed Valve
CAUTION: WIPE CLEAN ALL PARTS AND TOOLS AS NECESSARY TO REMOVE UNWANTED DEBRIS AND PREVENT DAMAGE TO THE ENGINE.
   (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 COVER - PROTECTION as necessary to prevent damage to the engine.
   (2) Install the bleed valve (1) as follows:
     (a) Apply P05-396Paraffin wax blend (PMC 9462) or beeswax (Material No.P05-395) to a new EIPC 75-32-02-01-090 GASKET (2).
     (b) Install the gasket (2) on the diffuser case boss.
     (c) Align and install the valve (1) on the diffuser case.
     (d) TORQUE the four captive bolts to between 70 and 60 lbf.in (0.79 and 0.68 m.daN )
T equally in an opposite pattern until the same torque indication holds.
   (3) Connection of the air sense tube (AS33) to the valve (1) as follows:
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.
     (a) Connect the air sense tube (AS33) to the HPC bleed valve (1) as follows:
       1 Connect the B-nut to the HPC bleed valve (1).
       2 TORQUE the B-nut to between 225 and 200 lbf.in (2.54 and 2.26 m.daN )
T. Do not loosen the B-nut.
       3 TORQUE the B-nut again to between 225 and 200 lbf.in (2.54 and 2.26 m.daN )
T.
   (4) Examine the assembly for foreign objects, damage and correct assembly.
5. Close-up
Subtask 75-32-02-410-050-A ** ON A/C NOT FOR ALL
Subtask 75-32-02-440-050-A ** ON A/C NOT FOR ALL
B. Do the reactivation of the thrust reverser system after maintenance (Ref. AMM TASK 78-30-00-440-805).
Subtask 75-32-02-410-051-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).
Subtask 75-32-02-720-050-A ** ON A/C NOT FOR ALL
D. Test
   (1) Do a test No. 3 - Power Plant - Operation Test (Idle Power Test) (Ref. AMM TASK 71-00-00-720-811).
[Rev.10 from 2021] 2026.04.01 03:13:44 UTC