W DOC AIRBUS | AMM A320F

Installation of the High Pressure Turbine (HPT) Active Clearance Control (ACC) Valve [CFML]


TASK 75-21-05-400-801-A
Installation of the High Pressure Turbine (HPT) Active Clearance Control (ACC) Valve


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.
ZONE: 400
FIN: 4025KS
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 - CONNECTOR, JAW, SOFT
No specific
AR
WARNING NOTICE(S)
No specific
2
WRENCH - TORQUE
No specific
Torque wrench: range to between 38 and 32 lbf.in (0.43 and 0.36 m.daN ) T
No specific
Torque wrench: range to between 124 and 106 lbf.in (1.40 and 1.20 m.daN ) T
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.CP2442)
engine oil
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
400
POWER PLANT, NACELLES AND PYLONS
FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENGINE 1)
437AL, 438AR, 451AL
FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENGINE 2)
447AL, 448AR, 461AL
 D. Expendable Parts
FIG.ITEM
DESIGNATION
IPC-CSN
3
GASKET SEAL
EIPC 73-00-00-20-220
 E. Referenced Information
REFERENCE
DESIGNATION
TASK 71-13-00-010-803-A
Opening of the Fan Cowl Doors
TASK 71-13-00-410-803-A
Closing of the Fan Cowl Doors
TASK 73-29-00-740-803-A
Idle Test (Menu Mode)
TASK 78-30-00-040-809-A
Deactivation of the Thrust Reverser System for Ground Maintenance
TASK 78-30-00-440-809-A
Reactivation of the Thrust Reverser System after Ground Maintenance
TASK 78-36-00-010-806-A
Opening of the Thrust Reverser Cowl Doors
TASK 78-36-00-410-806-A
Closing of the Thrust Reverser Cowl Doors
3. Job Set-up
Subtask 75-21-05-941-051-A
A. Safety Precautions
   (1) On the center pedestal, on ENG panel 115VU:
     (a) Make sure that the ENG/MODE selector switch is in the NORM position.
     (b) Make sure that the ENG/MASTER 1(2) control switch was in the OFF position not less than five minutes before you do this procedure.
     (c) Make sure that the WARNING NOTICE(S) are in position to tell persons not to operate:
  • The ENG/MODE selector switch, and
  • The ENG/MASTER 1(2) control switch.
   (2) On the ENG section of maintenance panel 50VU:
     (a) Make sure that the ON legend of the FADEC GND PWR/1(2) pushbutton switch is off.
     (b) Make sure that the WARNING NOTICE(S) is in position to tell persons not to energize FADEC 1(2).
Subtask 75-21-05-010-051-A
B. Get Access
   (1) Make sure that the fan cowl doors are open (Ref. AMM TASK 71-13-00-010-803):
     (a) FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENGINE 1)
437AL 438AR
     (b) FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENGINE 2)
447AL 448AR
   (2) Make sure that the ACCESS PLATFORM 1M(3 FT) is in position.
Subtask 75-21-05-040-051-A
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 78-30-00-040-809).
Subtask 75-21-05-010-053-A
D. Get Access
   (1) Make sure that the left thrust reverser cowl-door is open (Ref. AMM TASK 78-36-00-010-806):
     (a) FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENGINE 1)
451AL
     (b) FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENGINE 2)
461AL
4. Procedure
Subtask 75-21-05-420-050-A
A. Installation of the HPT ACC Valve
   (1) Remove all the COVER - PROTECTION and the CAP - PROTECTION from the openings, tubes, hoses and connectors.
   (2) Put the HPT ACC valve (1) in position on the bracket (10), bracket (11) and bracket (14).
   (3) Apply engine oil (Material No.CP2442) on the threads of the two bolts (8) and the bolt (18).
   (4) Install the two bolts (8) and the two washers (21) that attach the HPT ACC valve (1) to the bracket (10) and the bracket (11). Do not tighten the two bolts (8).
   (5) Install the bolt (18) and the washer (20) that attach the HPT ACC valve (1) to the bracket (14).
   (6) TORQUE the two bolts (8) and the bolt (18) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN ) T.
   (7) Use the two WRENCH - TORQUE to connect the drain tube (4) B-nut to the HPT ACC valve (1) fitting.
   (8) TORQUE the drain tube (4) B-nut to 285 lbf.in (3.22 m.daN).
   (9) Install the ACC wye duct (17) as follows:
     (a) Put the ACC wye duct (17) in position between the HPT ACC valve (1), ACC inlet duct (16) and LPT ACC valve (12).
     (b) Loosely install the hose clamp (19) that attaches the ACC wye duct (17) to the HPT ACC valve (1).
     (c) Loosely install the hose clamp (13) that attaches the ACC wye duct (17) to the Low Pressure Turbine (LPT) ACC valve (12).
     (d) Loosely install the hose clamp (15) that attaches the ACC wye duct (17) and the ACC inlet duct (16) to the engine bracket.
     (e) TORQUE the hose clamp (13), hose clamp (15) and hose clamp (19) to between 38 and 32 lbf.in (0.43 and 0.36 m.daN )
T.
   (10) Loosely install the hose clamp (7) that attaches the HPT aft valve elbow duct (9) to the HPT ACC valve (1).
   (11) TORQUE the hose clamp (7) to between 38 and 32 lbf.in (0.43 and 0.36 m.daN )
T.
   (12) Apply the engine oil (Material No.
CP2442) on the threads of the four bolts (6).
   (13) Install a new EIPC 73-00-00-20-220 GASKET SEAL (3) between the MTC-ACC fuel HYDR manifold (5) and the HPT ACC valve (1).

POST SB LEAP-1A 72-0292
   (14) Install the bracket (22) on top of the MTC-ACC fuel HYDR manifold (5).

END OF POST SB LEAP-1A 72-0292
   (15) Install the four bolts (6) that attach the MTC-ACC fuel HYDR manifold (5) to the HPT ACC valve (1).
   (16) TORQUE the four bolts (6) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN )
T.
   (17) Connect the electrical connector (2) to the HPT ACC valve (1). Tighten the coupling ring. If necessary, use the PLIERS - CONNECTOR, JAW, SOFT.
5. Close-up
Subtask 75-21-05-410-051-A
Subtask 75-21-05-440-050-A
B. Do the reactivation of the thrust reverser system after maintenance (Ref. AMM TASK 78-30-00-440-809).
Subtask 75-21-05-710-050-A
C. Test
   (1) Do the idle test (menu mode) (Ref. AMM TASK 73-29-00-740-803).
Subtask 75-21-05-410-050-A
D. Close Access
   (1) Close the fan cowl doors (Ref. AMM TASK 71-13-00-410-803):
     (a) FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENGINE 1)
437AL 438AR
     (b) FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENGINE 2)
447AL 448AR
   (2) Remove the access platform(s).
   (3) Remove the WARNING NOTICE(S).
[Rev.10 from 2021] 2026.04.01 03:14:10 UTC