W DOC AIRBUS | AMM A320F

Removal of the Vibration Sensor Harness [CFMB]


TASK 71-51-43-000-048-A
Removal of the Vibration Sensor Harness


FIN: 4201KS ** 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
COVER - PROTECTION
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
No specific
AR
WARNING NOTICE(S)
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
FOR [1000EM1] (ENGINE-1)
437AL, 438AR
FOR [1000EM2] (ENGINE-2)
447AL, 448AR
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 71-13-00-010-040-B
Opening of the Fan Cowl Doors
3. Job Set-up
Subtask 71-51-43-941-058-A ** ON A/C NOT FOR ALL
A. Safety Precautions
   (1) On the center pedestal, on the ENG panel 115VU:
     (a) Put a WARNING NOTICE(S) to tell persons not to start the engine.
   (2) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure.
   (3) On the overhead maintenance panel 50VU:
     (a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2) pushbutton switch is off.
     (b) Put a WARNING NOTICE(S) to tell persons not to energize the FADEC 1(2).
Subtask 71-51-43-865-074-A ** ON A/C NOT FOR ALL
WARNING: OPEN THE PROBE HEATER CIRCUIT-BREAKERS 1DA1(2), 3DA1(2,3), 4DA1(2,3) AND 5DA1(2,3) BEFORE ENG1(2)FADEC A and EIU 1(2) C/B'S 2KS1 AND 2KS2. IF YOU DO NOT OBEY THIS SEQUENCE:
  • THE PROBES WILL BECOME TOO HOT.
  • THIS CAN CAUSE DAMAGE TO EQUIPMENT AND INJURY TO MAINTENANCE PERSONNEL.
B. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUCOM/CVR/SPLY2RKE14
49VUCOM/CVR/CTL4RKE13
** ON A/C NOT FOR ALL
49VUENGINE/1 AND 2/IGN/SYS A1JHA03
49VUANTI ICE/PROBES/AOA/14DA1D04
49VUANTI ICE/PROBES/PITOT/13DA1D02
** ON A/C NOT FOR ALL
49VUANTI ICE/RAIN/RPLNT/CAPT1DB1D01
** ON A/C NOT FOR ALL
49VUCOM/CVR/SPLY23RKE14
49VUCOM/CVR/CTL26RKE13
** ON A/C NOT FOR ALL
121VURCDR/DFDR7TUK16
121VUHYDRAULIC/HYD POWER/Y3803GXN30
122VUANTI ICE/WINDOWS/R4DG2W14
122VUANTI ICE/WINDOWS/L4DG1X14
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
** ON A/C NOT FOR ALL
122VUANTI ICE/RAIN/RPLNT/F/O1DB2W11
** ON A/C NOT FOR ALL
123VUY HYD/ELEC/PUMP3802GXAB06
123VUY HYD/ELEC/ELEC PUMP/NORM3801GXAB03
FOR FIN: 1000EM1 (ENGINE1)
49VUENGINE/1/FIRE DET/LOOP A7WD1A06
49VUENGINE/1/FADEC A/AND EIU 12KS1A04
121VUENGINE/IGN/ENG1/SYS B3JH1P41
121VUENGINE/IGN/ENG1/SYS A BAT2JH1P39
121VUENGINE/ENG1 AND 2 FIRE EXTIG/BTL1/SQUIB/B2WE1Q44
121VUENGINE/ENG1 AND 2 FIRE EXTIG/BTL1/SQUIB/A1WE1Q43
121VUENGINE/ENG1/FIRE DET/LOOP B8WD1Q38
121VUENGINE/ENG1/FADEC B/AND EIU 14KS1R41
122VUELEC/GCU/12XU1T26
FOR FIN: 1000EM2 (ENGINE2)
49VUENGINE/2/FIRE DET/LOOP B8WD2A07
49VUENGINE/2/FADEC A/AND EIU 22KS2A05
121VUENGINE/IGN/ENG2/SYS B3JH2P42
121VUENGINE/IGN/ENG2/SYS A BAT2JH2P40
121VUENGINE/ENG1 AND 2 FIRE EXTIG/BTL2/SQUIB/B2WE2Q42
121VUENGINE/ENG1 AND 2 FIRE EXTIG/BTL2/SQUIB/A1WE2Q41
121VUENGINE/ENG2/FADEC B4KS2Q40
121VUENGINE/ENG2/FIRE DET/LOOP A7WD2Q39
122VUELEC/GCU/22XU2T27
Subtask 71-51-43-010-061-A ** ON A/C NOT FOR ALL
C. Get Access
   (1) Open the fan cowls: (Ref. AMM TASK 71-13-00-010-040)
   (2) FOR [1000EM1] (ENGINE-1)
437AL 438AR
   (3) FOR [1000EM2] (ENGINE-2)
447AL 448AR
   (4) Put the ACCESS PLATFORM 1M(3 FT) in position.
4. Procedure
Subtask 71-51-43-020-058-A ** ON A/C NOT FOR ALL
A. Removal of the Vibration Sensor Harness
NOTE: To open the flip-lock clamps and line blocks, turn the captive screws or captive bolts 1/4 turn counterclockwise to disengage the cam nuts.
NOTE: Loosely attach the clamp(s), anti-rotation lug(s) if applicable, and bolt(s) to the brackets from which they were removed to make it easier for installation.
   (1) Disconnect the electrical connector 448VC-A from the pylon junction box.
   (2) Open the flip-lock clamp (25) and remove the electrical harness (5).

BEFORE SPIB NO. CFM02255MW1

   (3) Open the 3 line blocks (10) attached to the brackets at station 167.
   (4) Open the line block (15) attached to the bracket at station 174.
   (5) Open the 3 line blocks (20) attached to the brackets at station 176, 185 and 191.
   (6) If necessary, remove the rubber supports from the line blocks. Remove the harness (5) from the rubber supports.

AFTER SPIB NO. CFM02255MW1

   (7) Remove the clamps and bolts (12) that attach the harness (5) to the brackets at station 167.
   (8) Remove the clamps, bolt and anti-rotation lug (13) that attach the harness (5) to the brackets at station 167.
   (9) Remove the clamps and bolt (17) that attach the harness (5) to the bracket at station 174.
   (10) Remove the clamps, bolts and anti-rotation lugs (22) that attach the harness (5) to the brackets at station 176 and 185.
   (11) Remove the clamps and bolts (23) that attach the harness (5) to the bracket at station 191.

END SPIB NO. CFM02255MW1

   (12) Disconnect the electrical connector 4002EV-A from the No. 1 bearing vibration accelerometer.
   (13) Remove the electrical harness (5) from the engine.
   (14) Put COVER - PROTECTION on the electrical connectors.
[Rev.10 from 2021] 2026.04.02 07:30:19 UTC