W DOC AIRBUS | AMM A320F

Removal of the Igniter Plug [IAE]


TASK 74-21-41-000-010-A
Removal of the Igniter Plug


WARNING: DO NOT TOUCH THE HIGH TENSION LEADS OF THE IGNITOR PLUGS FOR AT LEAST ONE MINUTE AFTER THE APPLICABLE CIRCUIT BREAKERS ARE OPEN. THE ELECTRICAL DISCHARGE OF THE HIGH ENERGY UNIT IS DANGEROUS AND CAN KILL.
CAUTION: DO NOT BEND THE ELECTRICAL CABLE CONDUIT TOO MUCH WHEN YOU DISCONNECT THE ELECTRICAL CONNECTOR. THE CONDUIT CAN BE DAMAGED AND CAN CAUSE ELECTRICAL CIRCUIT DEFECTS.
FIN: 4001JH1 ** ON A/C NOT FOR ALL
FIN: 4001JH2 ** ON A/C NOT FOR ALL
1. Reason for the Job
There are two ignitor plugs on each engine. This TASK gives the procedure to remove one ignitor plug. Use the same procedure to remove the second ignitor plug.
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, 452AR
FOR [1000EM2] (ENGINE-2)
447AL, 448AR, 462AR
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 71-13-00-010-010-A
Opening of the Fan Cowls 437AL(447AL),438AR(448AR)
TASK 74-21-41-200-010-A
Inspection of the Ignitor Plug
TASK 78-30-00-040-012-A
Deactivation of the Thrust Reverser Hydraulic Control Unit (HCU) for Ground Maintenance
TASK 78-32-00-010-010-A
Opening of the Thrust Reverser Halves
TSM 74-00-00-810-811
Failure of the Ignition System A on Engine 1
TSM 74-00-00-810-812
Failure of the Ignition System A on Engine 2
TSM 74-00-00-810-813
Failure of the Ignition System B on Engine 1
TSM 74-00-00-810-814
Failure of the Ignition System B on Engine 2
TSM 74-00-00-810-815
Failure of the Ignition Systems A and B on Engine 1
TSM 74-00-00-810-816
Failure of the Ignition Systems A and B on Engine 2
3. Job Set-up
Subtask 74-21-41-941-050-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 74-21-41-865-050-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/1 AND 2/IGN/SYS A1JHA03
FOR FIN: 1000EM1 (ENGINE1)
121VUENGINE/IGN/ENG1/SYS B3JH1P41
121VUENGINE/IGN/ENG1/SYS A BAT2JH1P39
FOR FIN: 1000EM2 (ENGINE2)
121VUENGINE/IGN/ENG2/SYS B3JH2P42
121VUENGINE/IGN/ENG2/SYS A BAT2JH2P40
Subtask 74-21-41-010-050-A ** ON A/C NOT FOR ALL
C. Get Access
   (1) Open the fan cowls (Ref. AMM TASK 71-13-00-010-010):
     (a) FOR [1000EM1] (ENGINE-1)
437AL 438AR
     (b) FOR [1000EM2] (ENGINE-2)
447AL 448AR
   (2) Put the ACCESS PLATFORM 1M(3 FT) in position.
Subtask 74-21-41-040-050-A ** ON A/C NOT FOR ALL
D. Deactivate the thrust reverser Hydraulic Control Unit (HCU) (Ref. AMM TASK 78-30-00-040-012).
Subtask 74-21-41-010-054-A ** ON A/C NOT FOR ALL
E. Open the right thrust reverser half (Ref. AMM TASK 78-32-00-010-010):
   (1) FOR [1000EM1] (ENGINE-1)
452AR
   (2) FOR [1000EM2] (ENGINE-2)
462AR
4. Procedure
Subtask 74-21-41-020-050-A ** ON A/C NOT FOR ALL
A. Removal of the Igniter Plug (4001JH1,4001JH2)
   (1) Disconnect the ignition lead.
F Igniter Plug ** ON A/C NOT FOR ALL
F Clip Points ** ON A/C NOT FOR ALL
     (a) Loosen the clamps (2) and (6) and move them away from the cooling shrouds (1) and (5).
     (b) Remove the cooling shrouds (1) and (5).
     (c) Remove the bolt (10), the washer (9) and the clip (8) from the clip point at Detail C.
     (d) Remove the bolt (18), the washers (19) and (23), the clips (20) and (22), the spacer (21) and the nut (24) from the clip point at Detail E.
     (e) Remove the bolt (17), the washers (12) and (16), the clips (13) and (15), the spacer (14) and the nut (11) from the clip point at Detail D.
     (f) Disconnect the ignition lead (4).
     (g) Remove and discard the grommet (3) from the ignition lead (4).
   (2) Remove the igniter plug.
F Igniter Plug ** ON A/C NOT FOR ALL
NOTE: Replace igniter plug only if one or more of the following conditions are met:
     (a) Remove the lockwire from the igniter threaded insert.
     (b) Hold the threaded insert with a wrench so it will not turn.
     (c) Loosen the igniter plug (7) with a wrench to remove it from the threaded insert.
     (d) Remove the igniter plug.
     (e) Do the procedure again to remove the remaining igniter.
   (3) Install COVER - PROTECTION to all exposed openings.
[Rev.10 from 2021] 2026.04.01 13:00:36 UTC