W DOC AIRBUS | AMM A320F

Installation of the Beam Electrical Harness [CFMI]


TASK 78-31-17-400-041-A
Installation of the Beam Electrical Harness


FIN: 4103KS1 ** ON A/C NOT FOR ALL
FIN: 4103KS2 ** 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
AR
ACCESS PLATFORM 1M(3 FT)
No specific
AR
PLIERS - NOSE, SOFT, LONG
No specific
AR
WARNING NOTICE(S)
No specific
Torque wrench: range to between 45 and 35 lbf.in (0.51 and 0.40 m.daN ) T
No specific
Torque wrench: range to between 80 and 70 lbf.in (0.90 and 0.79 m.daN ) T
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.CP2318)
blindexite RT 342-2
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
FOR [1000EM1] (ENGINE-1)
437AL, 438AR, 451AL, 452AR
FOR [1000EM2] (ENGINE-2)
447AL, 448AR, 461AL, 462AR
 D. Referenced Information
REFERENCE
DESIGNATION
TASK 71-13-00-010-040-A
Opening of the Fan Cowl Doors
TASK 71-13-00-410-040-A
Closing of the Fan Cowl Doors
TASK 78-30-00-081-041-A
Make the Thrust Reverser Serviceable after Maintenance
TASK 78-30-00-481-041-A
Make the Thrust Reverser Unserviceable for Maintenance
TASK 78-31-00-710-040-A-01
Operational Test of the Thrust Reverser without CFDS - Engine not Running
TASK 78-31-00-710-040-A-02
Operational Test of the Thrust Reverser without CFDS - Engine Running
TASK 78-31-00-710-040-A
Operational Test of the Thrust Reverser System
TASK 78-31-00-710-040-A-01
Operational Test of the Thrust Reverser without CFDS - Engine not Running
TASK 78-31-00-710-040-A-02
Operational Test of the Thrust Reverser without CFDS - Engine Running
TASK 78-36-00-010-040-A
Opening of the Thrust Reverser Doors
TASK 78-36-00-410-040-A
Closing of the Thrust Reverser Doors
3. Job Set-up
Subtask 78-31-17-860-051-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
   (1) On the center pedestal, on the ENG panel 115VU, make sure that a WARNING NOTICE(S) is in position to tell persons not to start the engine.
   (2) On the overhead maintenance panel 50VU, make sure that the ON legend of the ENG/FADEC GND PWR/1(2) pushbutton switch is off. Make sure that a WARNING NOTICE(S) is in position to tell persons not to energize the FADEC 1(2).
   (3) Make sure that the ACCESS PLATFORM 1M(3 FT) is in position.
Subtask 78-31-17-010-071-A ** ON A/C NOT FOR ALL
B. Get Access
   (1) Make sure that the fan cowl doors are open (Ref. AMM TASK 71-13-00-010-040):
     (a) FOR [1000EM1] (ENGINE-1)
437AL 438AR
     (b) FOR [1000EM2] (ENGINE-2)
447AL 448AR
   (2) Make sure that the thrust reverser doors are open (Ref. AMM TASK 78-36-00-010-040):
     (a) FOR [1000EM1] (ENGINE-1)
451AL 452AR
     (b) FOR [1000EM2] (ENGINE-2)
461AL 462AR
Subtask 78-31-17-040-062-A ** ON A/C NOT FOR ALL
C. Make sure that the thrust reverser is unserviceable (Ref. AMM TASK 78-30-00-481-041).
4. Procedure
Subtask 78-31-17-420-054-A ** ON A/C NOT FOR ALL
A. Installation of the Beam Electrical Harness
WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
   (1) Apply a layer of blindexite RT 342-2 (Material No.CP2318) on the harness surface in contact with the forward frame.
   (2) Install the beam electrical harness.
   (3) Connect the electrical harness to the blocker door deploy switch.
   (4) Tighten the coupling nuts of the deploy switch connectors with PLIERS - NOSE, SOFT, LONG.
   (5) Install the three bolts which attach the harness.
   (6) TORQUE the bolts to between 80 and 70 lbf.in (0.90 and 0.79 m.daN ) T.
   (7) Connect the forward frame electrical harness on to the beam harness connector.
   (8) Install the deploy switch access door.
   (9) Install the three screws.
   (10) TORQUE the screws to between 45 and 35 lbf.in (0.51 and 0.40 m.daN )
T.
5. Close-up
Subtask 78-31-17-410-059-A ** ON A/C NOT FOR ALL
Subtask 78-31-17-440-055-A ** ON A/C NOT FOR ALL
B. Make the thrust reverser serviceable (Ref. AMM TASK 78-30-00-081-041).
Subtask 78-31-17-410-060-A ** ON A/C NOT FOR ALL
C. Close Access
   (1) Close the fan cowl doors (Ref. AMM TASK 71-13-00-410-040):
     (a) FOR [1000EM1] (ENGINE-1)
437AL 438AR
     (b) FOR [1000EM2] (ENGINE-2)
447AL 448AR
   (2) Remove the WARNING NOTICE(S).
   (3) Remove the access platform(s).
Subtask 78-31-17-710-054-A ** ON A/C NOT FOR ALL
D. Do an operational test of the thrust reverser system from the CFDS (Ref. AMM TASK 78-31-00-710-040).
NOTE: As an alternative procedure, you can do this operational test without the CFDS:
[Rev.10 from 2021] 2026.04.02 07:41:51 UTC