DOC AIRBUS | AMM A320FInstallation of the Turbine Center Frame Accelerometer [CFML]
TASK 77-31-05-400-801-A
Installation of the Turbine Center Frame Accelerometer
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Consumable Materials
C. Work Zones and Access Panels
D. Referenced Information
3. Job Set-up
Subtask 77-31-05-941-051-A
Subtask 77-31-05-420-051-A
Subtask 77-31-05-410-052-A
[Rev.10 from 2021]
2026.04.02 07:41:41 UTC
Installation of the Turbine Center Frame Accelerometer
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: 4187KS
1. Reason for the JobSelf explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Consumable Materials
| REFERENCE | DESIGNATION |
|---|---|
| (Material No.CP2442) | engine oil |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENGINE 1) | |
| 437AL, 438AR, 451AL, 452AR | |
| FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENGINE 2) | |
| 447AL, 448AR, 461AL, 462AR | |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 36-11-49-400-827-A | Installation of the Environmental Control System (ECS) Ducts from the Engine Case Ports to the Pylon Connections |
| 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 73-29-00-710-802-A | FADEC 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 |
Turbine Center Frame Accelerometer (PRE SB 72-0036)Subtask 77-31-05-941-051-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:
(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 77-31-05-010-052-A (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.
(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).
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 77-31-05-040-051-A (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.
C. Deactivation of the Thrust Reverser System for Maintenance
Subtask 77-31-05-010-053-A 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). D. Get Access
(1) Make sure that the thrust reverser cowl-doors are open (Ref. AMM TASK 78-36-00-010-806):
(a) FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENGINE 1)
451AL 452AR
(b) FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENGINE 2)
461AL 462AR
4. Procedure(1) Make sure that the thrust reverser cowl-doors are open (Ref. AMM TASK 78-36-00-010-806):
(a) FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENGINE 1)
451AL 452AR
(b) FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENGINE 2)
461AL 462AR
Subtask 77-31-05-420-051-A
A. Installation of the Turbine Center Frame Accelerometer (PRE SB 72-0036)
(2) Put the turbine center frame accelerometer (2) and accelerometer mount (3) in position on the engine.
(3) Apply engine oil (Material No.CP2442) on the threads of the three bolts (1).
(4) Install the three bolts (1) that attach the turbine center frame accelerometer (2), accelerometer mount (3) and support bracket (5) to the fourth stage air manifold (4).
(5) Apply engine oil (Material No.CP2442) on the threads of the two bolts (23).
(6) Install the two bolts (23) that attach the turbine center frame accelerometer (2) to the support bracket (24).
(7) Install the turbine center frame accelerometer (2) cable loop clamps as follows:
(a) Apply engine oil (Material No.CP2442) on the threads of the bolt (7), bolt (9), bolt (11), bolt (15), bolt (17) and bolt (19).
(b) Install the bolt (19) that attaches the loop clamp (21) and turbine center frame accelerometer (2) cable to the support bracket (20) and tighten it with your hand.
(c) Install the bolt (17) that attaches the loop clamp (16) and turbine center frame accelerometer (2) cable to the support bracket (18) and tighten it with your hand.
(d) Install the bolt (15) that attaches the loop clamp (14) and turbine center frame accelerometer (2) cable to the support bracket (13) and tighten it with your hand.
(e) Install the bolt (11) that attaches the loop clamp (12) and turbine center frame accelerometer (2) cable to the support bracket (13) and tighten it with your hand.
(f) Install the bolt (9) that attaches the loop clamp (10) and turbine center frame accelerometer (2) cable to the support bracket (8) and tighten it with your hand.
(g) Install the bolt (7) that attaches the loop clamp (6) and turbine center frame accelerometer (2) cable to the support bracket (5) and tighten it with your hand.
(8) TORQUE the three bolts (1) that attach the turbine center frame accelerometer (2), accelerometer mount (3) and support bracket (5) to the fourth stage air manifold (4) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN )
.
(9) TORQUE the two bolts (23) that attach the turbine center frame accelerometer (2) to the support bracket (24) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN ).
(10) Connect the electrical connector (22) to the turbine center frame accelerometer (2). Tighten the coupling. Use PLIERS - JAWED, SOFT if necessary.
(11) TORQUE the turbine center frame accelerometer (2) cable loop clamp bolt (19), bolt (17), bolt (15), bolt (11), bolt (9) and bolt (7) to between 38 and 32 lbf.in (0.43 and 0.36 m.daN ).
Subtask 77-31-05-420-053-A WARNING:
USE PERSONAL PROTECTION EQUIPMENT. USE THE ENGINE OIL IN A WELL-VENTILATED AREA. ENGINE OIL IS TOXIC.
(1) Remove all protective COVER - PROTECTION and CAP - PROTECTION from the openings, tubes, hoses and connectors. (2) Put the turbine center frame accelerometer (2) and accelerometer mount (3) in position on the engine.
(3) Apply engine oil (Material No.CP2442) on the threads of the three bolts (1).
(4) Install the three bolts (1) that attach the turbine center frame accelerometer (2), accelerometer mount (3) and support bracket (5) to the fourth stage air manifold (4).
(5) Apply engine oil (Material No.CP2442) on the threads of the two bolts (23).
(6) Install the two bolts (23) that attach the turbine center frame accelerometer (2) to the support bracket (24).
(7) Install the turbine center frame accelerometer (2) cable loop clamps as follows:
(a) Apply engine oil (Material No.CP2442) on the threads of the bolt (7), bolt (9), bolt (11), bolt (15), bolt (17) and bolt (19).
(b) Install the bolt (19) that attaches the loop clamp (21) and turbine center frame accelerometer (2) cable to the support bracket (20) and tighten it with your hand.
(c) Install the bolt (17) that attaches the loop clamp (16) and turbine center frame accelerometer (2) cable to the support bracket (18) and tighten it with your hand.
(d) Install the bolt (15) that attaches the loop clamp (14) and turbine center frame accelerometer (2) cable to the support bracket (13) and tighten it with your hand.
(e) Install the bolt (11) that attaches the loop clamp (12) and turbine center frame accelerometer (2) cable to the support bracket (13) and tighten it with your hand.
(f) Install the bolt (9) that attaches the loop clamp (10) and turbine center frame accelerometer (2) cable to the support bracket (8) and tighten it with your hand.
(g) Install the bolt (7) that attaches the loop clamp (6) and turbine center frame accelerometer (2) cable to the support bracket (5) and tighten it with your hand.
(8) TORQUE the three bolts (1) that attach the turbine center frame accelerometer (2), accelerometer mount (3) and support bracket (5) to the fourth stage air manifold (4) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN )
. (9) TORQUE the two bolts (23) that attach the turbine center frame accelerometer (2) to the support bracket (24) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN )
. (10) Connect the electrical connector (22) to the turbine center frame accelerometer (2). Tighten the coupling. Use PLIERS - JAWED, SOFT if necessary.
(11) TORQUE the turbine center frame accelerometer (2) cable loop clamp bolt (19), bolt (17), bolt (15), bolt (11), bolt (9) and bolt (7) to between 38 and 32 lbf.in (0.43 and 0.36 m.daN )
. B. Installation of the Turbine Center Frame Accelerometer (POST SB 72-0036)
(2) Put the turbine center frame accelerometer (2) and accelerometer mount (3) in position on the engine.
(3) Apply engine oil (Material No.CP2442) on the threads of the three bolts (1).
(4) Install the three bolts (1) that attach the turbine center frame accelerometer (2), accelerometer mount (3) and support bracket (5) to the fourth stage air manifold (4).
(5) Apply engine oil (Material No.CP2442) on the threads of the two bolts (21).
(6) Install the two bolts (21) that attach the turbine center frame accelerometer (2) to the support bracket (22).
(7) Install the turbine center frame accelerometer (2) cable loop clamps as follows:
(a) Apply engine oil (Material No.CP2442) on the threads of the bolt (7), bolt (9), bolts (11), bolt (15) and bolt (18).
(b) Install the two bolts (18) that attaches the two loop clamps (19) and the turbine center frame accelerometer (2) cable to the support bracket (17).
(c) Install the bolt (15) that attaches the loop clamp (14) and turbine center frame accelerometer (2) cable to the support bracket (16) and tighten it with your hand.
(d) Install the two bolts (11) that attaches the two loop clamps (12) and the turbine center frame accelerometer (2) cable to the support bracket (13).
(e) Install the bolt (9) that attaches the loop clamp (10) and turbine center frame accelerometer (2) cable to the support bracket (8) and tighten it with your hand.
(f) Install the bolt (7) that attaches the loop clamp (6) and turbine center frame accelerometer (2) cable to the support bracket (5) and tighten it with your hand.
(8) TORQUE the three bolts (1) that attach the turbine center frame accelerometer (2), accelerometer mount (3) and support bracket (5) to the fourth stage air manifold (4) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN ).
(9) TORQUE the two bolts (21) that attach the turbine center frame accelerometer (2) to the support bracket (22) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN ).
(10) Connect the electrical connector (20) to the turbine center frame accelerometer (2). Tighten the coupling. Use PLIERS - JAWED, SOFT if necessary.
(11) TORQUE the turbine center frame accelerometer (2) cable loop clamp bolt (18), bolt (15), bolt (11), bolt (9) and bolt (7) to between 38 and 32 lbf.in (0.43 and 0.36 m.daN ).
Subtask 77-31-05-420-052-A WARNING:
USE PERSONAL PROTECTION EQUIPMENT. USE THE ENGINE OIL IN A WELL-VENTILATED AREA. ENGINE OIL IS TOXIC.
(1) Remove all protective COVER - PROTECTION and CAP - PROTECTION from the openings, tubes, hoses and connectors. (2) Put the turbine center frame accelerometer (2) and accelerometer mount (3) in position on the engine.
(3) Apply engine oil (Material No.CP2442) on the threads of the three bolts (1).
(4) Install the three bolts (1) that attach the turbine center frame accelerometer (2), accelerometer mount (3) and support bracket (5) to the fourth stage air manifold (4).
(5) Apply engine oil (Material No.CP2442) on the threads of the two bolts (21).
(6) Install the two bolts (21) that attach the turbine center frame accelerometer (2) to the support bracket (22).
(7) Install the turbine center frame accelerometer (2) cable loop clamps as follows:
(a) Apply engine oil (Material No.CP2442) on the threads of the bolt (7), bolt (9), bolts (11), bolt (15) and bolt (18).
(b) Install the two bolts (18) that attaches the two loop clamps (19) and the turbine center frame accelerometer (2) cable to the support bracket (17).
(c) Install the bolt (15) that attaches the loop clamp (14) and turbine center frame accelerometer (2) cable to the support bracket (16) and tighten it with your hand.
(d) Install the two bolts (11) that attaches the two loop clamps (12) and the turbine center frame accelerometer (2) cable to the support bracket (13).
(e) Install the bolt (9) that attaches the loop clamp (10) and turbine center frame accelerometer (2) cable to the support bracket (8) and tighten it with your hand.
(f) Install the bolt (7) that attaches the loop clamp (6) and turbine center frame accelerometer (2) cable to the support bracket (5) and tighten it with your hand.
(8) TORQUE the three bolts (1) that attach the turbine center frame accelerometer (2), accelerometer mount (3) and support bracket (5) to the fourth stage air manifold (4) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN )
.(9) TORQUE the two bolts (21) that attach the turbine center frame accelerometer (2) to the support bracket (22) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN )
.(10) Connect the electrical connector (20) to the turbine center frame accelerometer (2). Tighten the coupling. Use PLIERS - JAWED, SOFT if necessary.
(11) TORQUE the turbine center frame accelerometer (2) cable loop clamp bolt (18), bolt (15), bolt (11), bolt (9) and bolt (7) to between 38 and 32 lbf.in (0.43 and 0.36 m.daN )
.C. Installation of the Environmental Control System (ECS) Upper Duct
(1) If necessary, install the ECS upper duct (Ref. AMM TASK 36-11-49-400-827).
Subtask 77-31-05-710-050-A 5. Close-up(1) If necessary, install the ECS upper duct (Ref. AMM TASK 36-11-49-400-827).
Subtask 77-31-05-410-052-A
A. 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 78-36-00-410-806)
(a) FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENGINE 1)
451AL 452AR
(b) FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENGINE 2)
461AL 462AR
Subtask 77-31-05-440-051-A Subtask 77-31-05-410-053-A (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 78-36-00-410-806)
(a) FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENGINE 1)
451AL 452AR
(b) FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENGINE 2)
461AL 462AR