W DOC AIRBUS | AMM A320F

Removal of the CJ12L Harness [CFMB]


TASK 73-21-50-000-027-A
Removal of the CJ12L Harness


FIN: 1000EM1 ** ON A/C NOT FOR ALL
FIN: 1000EM2 ** ON A/C NOT FOR ALL
1. Reason for the Job
This TASK is applicable for NON /P engines.
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
AR
CAP - BLANKING
No specific
AR
PLIERS - CONNECTOR, JAW, SOFT
No specific
AR
WARNING NOTICE(S)
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
FOR [1000EM1] (ENGINE-1)
437AL, 438AR, 451AL
FOR [1000EM2] (ENGINE-2)
447AL, 448AR, 461AL
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 71-13-00-010-040-B
Opening of the Fan Cowl Doors
TASK 78-30-00-481-041-B
Make the Thrust Reverser Unserviceable for Maintenance
TASK 78-36-00-010-040-B
Opening of the Thrust Reverser Doors
3. Job Set-up
Subtask 73-21-50-941-077-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 73-21-50-010-097-A ** ON A/C NOT FOR ALL
B. Open the fan cowl doors (Ref. AMM TASK 71-13-00-010-040):
   (1) FOR [1000EM1] (ENGINE-1)
437AL 438AR
   (2) FOR [1000EM2] (ENGINE-2)
447AL 448AR
Subtask 73-21-50-040-108-A ** ON A/C NOT FOR ALL
C. Make the thrust reverser unserviceable (Ref. AMM TASK 78-30-00-481-041).
Subtask 73-21-50-010-114-A ** ON A/C NOT FOR ALL
D. Open the left thrust reverser door (Ref. AMM TASK 78-36-00-010-040):
   (1) FOR [1000EM1] (ENGINE-1)
451AL
   (2) FOR [1000EM2] (ENGINE-2)
461AL
4. Procedure
Subtask 73-21-50-020-065-A ** ON A/C NOT FOR ALL
A. Removal of the CJ12L Harness
   (1) Disconnect the CJ12L harness (10) from the VBV position sensor CH. B, the VSV position sensor CH. B and the RACSB valve position sensor CH. B. Use PLIERS - CONNECTOR, JAW, SOFT only if necessary.
   (2) Disconnect the HJ12 harness from the CJ12L harness receptacle in the 6 o'clock junction box, left-hand side (ALF). Use PLIERS - CONNECTOR, JAW, SOFT only if necessary.
   (3) Cut and remove the lockwire which safeties the CJ12L bulkhead connector nut (130) in the 6 o'clock junction box.
   (4) Remove the nut (130) and disengage the CJ12L harness bulkhead connector from the 6 o'clock junction box (Detail B).
   (5) Put the CAP-BLANKING on each disconnected electrical connector and receptacle.
   (6) Remove the parts which attach the CJ12L harness as follows:
REMOVE
FROM
NOTE
Bolt (30)
Clamp (20) on
CJ12L harness and
fan frame
At the 7:45 o'clock position
(Detail C)
Bolt (100)
Bracket (110)
At the 8:30 o'clock position
(Detail D)
Bolt (50)
Clamp (40) on
bracket (60) on
the VBV fuel gear
motor
At the 9 o'clock position
(Detail E)
Bolt (90)
Clamp (70) on
CJ12L harness and
bracket (80)
At the 7:30 o'clock position
(Detail F)
Clamps (20), (40)
and (70)
CJ12L harness (10)
(Details C, E and F)
   (7) Remove the CJ12L harness (10) from the engine.
[Rev.10 from 2021] 2026.04.01 02:58:41 UTC