W DOC AIRBUS | AMM A320F

Removal of the Core Fire Detector Channel B Wire Harness [CFMI]


TASK 71-52-43-000-002-A
Removal of the Core Fire Detector Channel B Wire Harness


FIN: 1000EM1 ** ON A/C NOT FOR ALL
FIN: 1000EM2 ** 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 2M (6 FT) - ADJUSTABLE
No specific
AR
CAP - BLANKING
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, 451AL, 452AR
FOR [1000EM2] (ENGINE-2)
447AL, 448AR, 461AL, 462AR
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 71-13-00-010-040-A
Opening of the Fan Cowl Doors
TASK 78-30-00-481-041-A
Make the Thrust Reverser Unserviceable for Maintenance
TASK 78-36-00-010-040-A
Opening of the Thrust Reverser Doors
3. Job Set-up
Subtask 71-52-43-860-065-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 71-52-43-865-072-A ** ON A/C NOT FOR ALL
B. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUENGINE/2/FIRE DET/LOOP B8WD2A07
49VUENGINE/1/FIRE DET/LOOP A7WD1A06
49VUENGINE/2/FADEC A/AND EIU 22KS2A05
49VUENGINE/1/FADEC A/AND EIU 12KS1A04
49VUENGINE/1 AND 2/IGN/SYS A1JHA03
49VUANTI ICE/PROBES/AOA/14DA1D04
49VUANTI ICE/PROBES/PHC/12DA1D03
49VUANTI ICE/PROBES/PITOT/13DA1D02
49VUCOM/CVR/SPLY2RKE14
49VUCOM/CVR/CTL4RKE13
49VUNAV PROBES/ADIRU 1/AND AOA 1/26VAC5FP1F07
49VUNAV PROBES/ADIRU1/115VAC4FP1F06
105VUADIRS/ADIRU1/28VDC6FP1C02
121VURCDR/DFDR7TUK16
121VUENGINE/ENG2/OIL/PRESS2EN2N42
121VUENGINE/ENG2/OIL/QTY1EN2N41
121VUENGINE/ENG1/OIL/PRESS2EN1N40
121VUENGINE/ENG1/OIL/QTY1EN1N39
121VUADIRS/ADIRU/2/26VAC AND AOA5FP2N08
121VUADIRS/ADIRU/3/26VAC AND AOA5FP3N07
121VUADIRS/ADIRU/2/115VAC4FP2N06
121VUADIRS/ADIRU/3/115VAC4FP3N05
121VUADIRS/ADIRU/2/28VDC6FP2N04
121VUADIRS/ADIRU/3/28VDC6FP3N03
121VUENGINE/IGN/ENG2/SYS B3JH2P42
121VUENGINE/IGN/ENG1/SYS B3JH1P41
121VUENGINE/IGN/ENG2/SYS A BAT2JH2P40
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 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
121VUENGINE/ENG1/FIRE DET/LOOP B8WD1Q38
121VUENGINE/ENG1/FADEC B/AND EIU 14KS1R41
122VUELEC/GCU/22XU2T27
122VUELEC/GCU/12XU1T26
122VUANTI ICE/WINDOWS/R4DG2W14
122VUANTI ICE/WINDOWS/L4DG1X14
122VUANTI ICE/PROBES/PHC/32DA3Y16
122VUANTI ICE/PROBES/2/TAT1DA2Y15
122VUANTI ICE/PROBES/2/PITOT3DA2Y14
122VUANTI ICE/PROBES/2/AOA4DA2Y13
122VUANTI ICE/PROBES/PHC/22DA2Y12
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
Subtask 71-52-43-010-073-A ** ON A/C NOT FOR ALL
C. Get Access
   (1) Open the fan cowl doors (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 2M (6 FT) - ADJUSTABLE in position.
Subtask 71-52-43-040-065-A ** ON A/C NOT FOR ALL
D. Make the thrust reverser unserviceable (Ref. AMM TASK 78-30-00-481-041).
Subtask 71-52-43-010-074-A ** ON A/C NOT FOR ALL
E. Open the thrust reverser doors (Ref. AMM TASK 78-36-00-010-040):
   (1) FOR [1000EM1] (ENGINE-1)
451AL 452AR
   (2) FOR [1000EM2] (ENGINE-2)
461AL 462AR
4. Procedure
Subtask 71-52-43-020-061-A ** ON A/C NOT FOR ALL
A. Removal of the Channel B Fire Detector Harness
   (1) Disconnect the electrical connector 454VC-A from the core junction box.
   (2) Remove the two bolts (5) and open the two clamps (10) that attach the harnesses to the pylon. Remove the harness from the clamps. Install the bolt (5) and tighten it with your hand.
   (3) Remove the screw (15) and washer (20). Open the clamp (25) that attaches the harness assemblies to the bracket and station 233. Remove harness from the clamp. Install the screw (15) and washer (20). Tighten the screw with your hand.
   (4) Remove the screw (30), spacer (35) and lug (40) that attach the clamp (45) to the bracket at the top of the engine.
(Ref. Detail B).
   (5) Remove the screw (50), washer (20) and nut (55) that attach the clamp (45) to the bracket at station 239.
   (6) Remove the screw (15), washer (20), spacer (35) and lug (40) that attach the clamp (45) to the bracket at station 239.
   (7) Remove the screw (15) and washer (20) that attach the clamp (45) to the bracket at station 239.
   (8) Cut the lockwire and remove the screws (75) and the clamp (70) that attach the harness to the fire detector element 4001WD2-A.
   (9) Remove the nut (60) that attaches the wire (65) to terminal A of the fire detector.
   (10) Remove the nut (90) that attaches the wire (85) to terminal C of the fire detector.
   (11) Remove the screw (95) and the washer (20) that attach the ground wire (80) to the bracket.
   (12) Remove the fire detector channel B harness from the engine.
   (13) Put CAP - BLANKING on the disconnected electrical connectors.
[Rev.10 from 2021] 2026.04.01 02:23:28 UTC