W DOC AIRBUS | AMM A320F

Installation of the EEC Wiring Harness (WF02) [PW11]


TASK 73-21-62-400-802-A
Installation of the EEC Wiring Harness (WF02)


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.
CAUTION: DO NOT BEND OR TWIST THE HARNESS TOO MUCH. IF YOU DO, DAMAGE TO THE HARNESS CAN OCCUR.
ZONE: 400
FIN: 4218KS ** ON A/C NOT FOR ALL
1. Reason for the Job
Use this procedure to install the harness (WF02).
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
1
ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE
No specific
1
PLIERS - JAWED, SOFT
No specific
Torque wrench: range to between 44 and 38 lbf.in (0.50 and 0.43 m.daN ) T
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.P06-054)
Antigalling Compound
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
400
POWER PLANT, NACELLES AND PYLONS
FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENG 1)
437AL, 438AR
FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENG 2)
447AL, 448AR
 D. Expendable Parts
FIG.ITEM
DESIGNATION
IPC-CSN
3
TAPE - PRESSURE SENSITIVE ADHESIVE
EIPC 73-21-62-01-340
 E. Referenced Information
REFERENCE
DESIGNATION
TASK 23-44-00-700-001-A
Operational Test of the Service Interphone
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 73-21-00-710-806-A
Test No.7 - EEC Operation Test (Self Test)
TASK 73-25-34-400-802-A
Installation of the Engine Interface Unit (EIU)
3. Job Set-up
Subtask 73-21-62-941-055-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).
   (2) On maintenance panel 80VU:
     (a) Make sure that ON legend on the SVCE INTERPHONE OVRD pushbutton switch is off.
Subtask 73-21-62-865-058-A ** ON A/C NOT FOR ALL
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUENGINE/1 AND 2/IGN/SYS A1JHA03
49VUANTI ICE/PROBES/AOA/14DA1D04
49VUANTI ICE/PROBES/PITOT/13DA1D02
49VUANTI ICE/RAIN/RPLNT/CAPT1DB1D01
49VUNAV PROBES/ADIRU 1/AND AOA 1/26VAC5FP1F07
105VUADIRS/ADIRU1/28VDC6FP1C02
122VUANTI ICE/WINDOWS/R4DG2W14
122VUANTI ICE/RAIN/RPLNT/F/O1DB2W11
122VUANTI ICE/WINDOWS/L4DG1X14
122VUANTI ICE/PROBES/2/TAT1DA2Y15
122VUANTI ICE/PROBES/2/PITOT3DA2Y14
122VUANTI ICE/PROBES/2/AOA4DA2Y13
122VUANTI ICE/PROBES/2/STATIC5DA2Y11
122VUANTI ICE/PROBES/3/PITOT3DA3Z16
122VUANTI ICE/PROBES/3/AOA4DA3Z15
122VUANTI ICE/PROBES/3/STATIC5DA3Z14
122VUANTI ICE/PROBES/1/STATIC5DA1Z13
122VUANTI ICE/PROBES/1/TAT1DA1Z12
** ON A/C NOT FOR ALL
FOR FIN: 4020KM1 (POWER PLANTDEMOUNTABLE, ENG 1)
121VUICU A/ENG1 PWR SUPPLY22KS1R39
** ON A/C NOT FOR ALL
121VUPHMU/ENG195KS1P44
** ON A/C NOT FOR ALL
121VUICU A/ENG1 PWR SUPPLY22KS1R38
** ON A/C NOT FOR ALL
FOR FIN: 4020KM2 (POWER PLANTDEMOUNTABLE, ENG 2)
121VUICU A/ENG2 PWR SUPPLY22KS2R40
** ON A/C NOT FOR ALL
121VUPHMU/ENG295KS2P45
** ON A/C NOT FOR ALL
121VUICU A/ENG2 PWR SUPPLY22KS2R39
Subtask 73-21-62-865-059-A ** ON A/C NOT FOR ALL
WARNING: MAKE SURE THAT THE PROBE HEATER AND WINDOW HEATER CIRCUIT-BREAKERS ARE OPEN BEFORE YOU OPEN THE PHC AND WHC CIRCUIT BREAKERS. IF YOU DO NOT OBEY THIS SEQUENCE:
  • THE PROBES WILL BECOME TOO HOT.
  • THIS CAN CAUSE INJURY TO MAINTENANCE PERSONNEL AND/OR DAMAGE TO EQUIPMENT.
WARNING: OPEN CIRCUIT BREAKERS 2KS1 AND 2KS2 AFTER YOU OPEN THE IGNITION CIRCUIT BREAKERS. IF YOU DO NOT, THE CONTINUOUS IGNITION SYSTEM WILL BE ACTIVATED.
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUANTI ICE/PROBES/PHC/12DA1D03
122VUANTI ICE/WHC/25DG2W13
122VUANTI ICE/WHC/15DG1X13
122VUANTI ICE/PROBES/PHC/32DA3Y16
122VUANTI ICE/PROBES/PHC/22DA2Y12
FOR FIN: 4020KM1 (POWER PLANTDEMOUNTABLE, ENG 1)
49VUENGINE/1/FADEC A/AND EIU 12KS1A04
** ON A/C NOT FOR ALL
121VUENGINE/ENG1/FADEC B/AND EIU 14KS1R41
** ON A/C NOT FOR ALL
121VUENGINE/ENG1/FADEC B/AND EIU 14KS1R40
** ON A/C NOT FOR ALL
FOR FIN: 4020KM2 (POWER PLANTDEMOUNTABLE, ENG 2)
49VUENGINE/2/FADEC A/AND EIU 22KS2A05
** ON A/C NOT FOR ALL
121VUENGINE/ENG2/FADEC B/AND EIU24KS2Q40
** ON A/C NOT FOR ALL
121VUENGINE/ENG2/FADEC B/AND EIU24KS2R41
Subtask 73-21-62-010-059-A ** ON A/C NOT FOR ALL
D. 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 2M (6 FT) - ADJUSTABLE is in position.
4. Procedure
Subtask 73-21-62-420-052-A ** ON A/C NOT FOR ALL
A. Installation of the EEC Wiring Harness WF02
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) Route the harness (WF02) (1) along the engine. See the sheet 1 of the figure:
F EEC Wiring Harness WF02 ** ON A/C NOT FOR ALL
   (3) Connect the harness (WF02) (1) connectors to the engine as follows:
     (a) Connect the connector (P402) to the pylon receptacle (J402) as follows:
       1 Examine, align and engage the connector.
       2 Push lightly in on the connector while you tighten the coupling ring.
       3 Use the PLIERS - JAWED, SOFT to tighten the connector against the receptacle.
       4 Make sure that you can feel the ratchet feature.
       5 While you tighten, push the connector in and from side to side.
       6 Tighten the connector until the PLIERS - JAWED, SOFT slip on the connector ring.
     (b) Connect the connector (P406) to the pylon receptacle (J406) as follows:
       1 Examine, align and engage the connector.
       2 Push lightly in on the connector while you tighten the coupling ring.
       3 Use the PLIERS - JAWED, SOFT to tighten the connector against the receptacle.
       4 Make sure that you can feel the ratchet feature.
       5 While you tighten, push the connector in and from side to side.
       6 Tighten the connector until the PLIERS - JAWED, SOFT slip on the connector ring.
     (c) Connect the connector (P79) to the interphone jack receptacle (J79) as follows: See the sheet 2 of the figure:
F EEC Wiring Harness WF02 ** ON A/C NOT FOR ALL
       1 Examine, align and engage the connector.
       2 Push lightly in on the connector while you tighten the coupling ring.
       3 Use the PLIERS - JAWED, SOFT to tighten the connector against the receptacle.
       4 Make sure that you can feel the ratchet feature.
       5 While you tighten, push the connector in and from side to side.
       6 Tighten the connector until the PLIERS - JAWED, SOFT slip on the connector ring.
     (d) Apply Antigalling Compound (Material No.P06-054) to the threads of the four bolts (2).
NOTE: For new or refurbished bolts or nuts with baked on lubricant, do not do the wet application.
     (e) Install the harness (WF02) (1) to the bracket with the four bolts (2).
     (f) TORQUE the four bolts (2) to between 44 and 38 lbf.in (0.50 and 0.43 m.daN ) T.
     (g) Connect the harness (W04) connector (P102) to the harness (WF02) receptacle (J102) as follows:
       1 Examine, align and engage the connector.
       2 Push lightly in on the connector while you tighten the coupling ring.
       3 Use the PLIERS - JAWED, SOFT to tighten the connector against the receptacle.
       4 Make sure that you can feel the ratchet feature.
       5 While you tighten, push the connector in and from side to side.
       6 Tighten the connector until the PLIERS - JAWED, SOFT slip on the connector ring.
     (h) Connect the harness (WF01) connector (P103) to the harness (WF02) (1) receptacle (J103) as follows:
       1 Examine, align and engage the connector.
       2 Push lightly in on the connector while you tighten the coupling ring.
       3 Use the PLIERS - JAWED, SOFT to tighten the connector against the receptacle.
       4 Make sure that you can feel the ratchet feature.
       5 While you tighten, push the connector in and from side to side.
       6 Tighten the connector until the PLIERS - JAWED, SOFT slip on the connector ring.
     (i) Connect the connector (P122) to the T2 probe harness receptacle (J122) as follows: See the sheet 3 of the figure:
F EEC Wiring Harness WF02 ** ON A/C NOT FOR ALL
       1 Examine, align and engage the connector.
       2 Push lightly in on the connector while you tighten the coupling ring.
       3 Use the PLIERS - JAWED, SOFT to tighten the connector against the receptacle.
       4 Make sure that you can feel the ratchet feature.
       5 While you tighten, push the connector in and from side to side.
       6 Tighten the connector until the PLIERS - JAWED, SOFT slip on the connector ring.
     (j) Connect the connector (P1) to the EEC receptacle (J1) as follows: See the sheet 5 of the figure:
F EEC Wiring Harness WF02 ** ON A/C NOT FOR ALL
       1 Examine, align and engage the connector.
       2 Push lightly in on the connector while you tighten the coupling ring.
       3 Use the PLIERS - JAWED, SOFT to tighten the connector against the receptacle.
       4 Make sure that you can feel the ratchet feature.
       5 While you tighten, push the connector in and from side to side.
       6 Tighten the connector until the PLIERS - JAWED, SOFT slip on the connector ring.
     (k) Connect the connector (P9) to the Prognostics and Health Management Unit (PHMU) receptacle (J9) as follows:
       1 Examine, align and engage the connector.
       2 Push lightly in on the connector while you tighten the coupling ring.
       3 Use the PLIERS - JAWED, SOFT to tighten the connector against the receptacle.
       4 Make sure that you can feel the ratchet feature.
       5 While you tighten, push the connector in and from side to side.
       6 Tighten the connector until the PLIERS - JAWED, SOFT slip on the connector ring.
     (l) Install the harness (WF02) (1) to the bracket (14) as follows: See the sheet 6 of the figure:
F EEC Wiring Harness WF02 ** ON A/C NOT FOR ALL
       1 Apply Antigalling Compound (Material No.P06-054) to the threads of the bolt (12).
NOTE: For new or refurbished bolts or nuts with baked on lubricant, do not do the wet application.
       2 Install the harness (WF02) (1) to the bracket (14) with the bolt (12) and clamp (13).
       3 TORQUE the bolt (12) to between 44 and 38 lbf.in (0.50 and 0.43 m.daN ) T.

POST SB C-72-00-0105A: Harness Protection Method

     (m) Wrap the harness (WF02) (1) at the spring clip with
EIPC 73-21-62-01-340 TAPE - PRESSURE SENSITIVE ADHESIVE (3). See the sheets 1 and 3 of the figure:
F EEC Wiring Harness WF02 ** ON A/C NOT FOR ALL
       1 Tape - pressure sensitive adhesive must be in the center of the spring clip.
     (n) Wrap the harness (WF02) (1) at the spring clip with EIPC 73-21-62-01-340 TAPE - PRESSURE SENSITIVE ADHESIVE (3). See the sheets 1 and 7 of the figure:
F EEC Wiring Harness WF02 ** ON A/C NOT FOR ALL
       1 Tape - pressure sensitive adhesive must be in the center of the spring clip.

END OF POST SB C-72-00-0105A: Harness Protection Method

     (o) Install the harness (WF02) (1) to the ten spring clips as follows: See the sheets 1 and 4 of the figure:
F EEC Wiring Harness WF02 ** ON A/C NOT FOR ALL
       1 Start at the middle of the harness (WF02) (1).
       2 Position and push the harness (WF02) (1) into the ten spring clips.
       3 Make sure that all the spring clips engage with the harness (WF02) (1).
       4 Make sure that the tension in the harness (WF02) (1) is sufficient to prevent loose or tight conditions.
     (p) Examine the harness (WF02) (1) for contact with engine hardware which can cause chafing.
     (q) Examine the assembly for foreign objects, damage and correct assembly.
5. Close-up
Subtask 73-21-62-865-060-A ** ON A/C NOT FOR ALL
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUANTI ICE/PROBES/PHC/12DA1D03
122VUANTI ICE/WHC/25DG2W13
122VUANTI ICE/WHC/15DG1X13
122VUANTI ICE/PROBES/PHC/32DA3Y16
122VUANTI ICE/PROBES/PHC/22DA2Y12
FOR FIN: 4020KM1 (POWER PLANTDEMOUNTABLE, ENG 1)
49VUENGINE/1/FADEC A/AND EIU 12KS1A04
** ON A/C NOT FOR ALL
121VUENGINE/ENG1/FADEC B/AND EIU 14KS1R41
** ON A/C NOT FOR ALL
121VUENGINE/ENG1/FADEC B/AND EIU 14KS1R40
** ON A/C NOT FOR ALL
FOR FIN: 4020KM2 (POWER PLANTDEMOUNTABLE, ENG 2)
49VUENGINE/2/FADEC A/AND EIU 22KS2A05
** ON A/C NOT FOR ALL
121VUENGINE/ENG2/FADEC B/AND EIU24KS2Q40
** ON A/C NOT FOR ALL
121VUENGINE/ENG2/FADEC B/AND EIU24KS2R41
Subtask 73-21-62-865-061-A ** ON A/C NOT FOR ALL
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUENGINE/1 AND 2/IGN/SYS A1JHA03
49VUANTI ICE/PROBES/AOA/14DA1D04
49VUANTI ICE/PROBES/PITOT/13DA1D02
49VUANTI ICE/RAIN/RPLNT/CAPT1DB1D01
49VUNAV PROBES/ADIRU 1/AND AOA 1/26VAC5FP1F07
105VUADIRS/ADIRU1/28VDC6FP1C02
122VUANTI ICE/WINDOWS/R4DG2W14
122VUANTI ICE/RAIN/RPLNT/F/O1DB2W11
122VUANTI ICE/WINDOWS/L4DG1X14
122VUANTI ICE/PROBES/2/TAT1DA2Y15
122VUANTI ICE/PROBES/2/PITOT3DA2Y14
122VUANTI ICE/PROBES/2/AOA4DA2Y13
122VUANTI ICE/PROBES/2/STATIC5DA2Y11
122VUANTI ICE/PROBES/3/PITOT3DA3Z16
122VUANTI ICE/PROBES/3/AOA4DA3Z15
122VUANTI ICE/PROBES/3/STATIC5DA3Z14
122VUANTI ICE/PROBES/1/STATIC5DA1Z13
122VUANTI ICE/PROBES/1/TAT1DA1Z12
** ON A/C NOT FOR ALL
FOR FIN: 4020KM1 (POWER PLANTDEMOUNTABLE, ENG 1)
121VUICU A/ENG1 PWR SUPPLY22KS1R39
** ON A/C NOT FOR ALL
121VUPHMU/ENG195KS1P44
** ON A/C NOT FOR ALL
121VUICU A/ENG1 PWR SUPPLY22KS1R38
** ON A/C NOT FOR ALL
FOR FIN: 4020KM2 (POWER PLANTDEMOUNTABLE, ENG 2)
121VUICU A/ENG2 PWR SUPPLY22KS2R40
** ON A/C NOT FOR ALL
121VUPHMU/ENG295KS2P45
** ON A/C NOT FOR ALL
121VUICU A/ENG2 PWR SUPPLY22KS2R39
Subtask 73-21-62-860-054-A ** ON A/C NOT FOR ALL
C. Put the aircraft back to its initial configuration.
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Remove the WARNING NOTICE(S).
Subtask 73-21-62-710-050-A ** ON A/C NOT FOR ALL
D. Test(s)
   (1) 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).
   (2) Do the test No. 7 (Ref. AMM TASK 73-21-00-710-806).
Subtask 73-21-62-410-050-A ** ON A/C NOT FOR ALL
E. Close Access
   (1) Remove the access platform(s).
   (2) 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
Subtask 73-21-62-710-051-A ** ON A/C NOT FOR ALL
F. Do the operational test of the service interphone (Ref. AMM TASK 23-44-00-700-001)
[Rev.10 from 2021] 2026.04.01 13:06:42 UTC