W DOC AIRBUS | AMM A320F

Installation of the Static Discharger

TASK 23-61-41-400-001-A
Installation of the Static Discharger

WARNING: MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING NOTICES ARE IN POSITION.
WARNING: MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING GEAR. THIS WILL PREVENT UNWANTED MOVEMENT OF THE LANDING GEAR, AND THUS POSSIBLE INJURY TO PERSONS AND DAMAGE TO THE AIRCRAFT AND/OR EQUIPMENT.
WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
ZONE: 300
ZONE: 500
ZONE: 600
1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
1
ACCESS PLATFORM 12M (40 FT) - ADJUSTABLE
No specific
AR
SAFETY BARRIER(S)
No specific
Torque wrench: range to between 0.21 and 0.19 m.daN (18.58 and 16.81 lbf.in ) T
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.08BAA9)
Non Aqueous Cleaner-General - -
(Material No.14SBA1)
Textile-Lint free Cotton -
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
300
STABILIZERS AND TAIL UNIT
500
LEFT WING
600
RIGHT WING
 D. Referenced Information
REFERENCE
DESIGNATION
TASK 23-61-00-200-001-A
Resistance Check from the Tip to the Retainer and Bonding Check from the Retainer to the Aircraft Structure
F Static Discharger - Location and Detail ** ON A/C NOT FOR ALL
F Static Discharger - Location and Detail ** ON A/C NOT FOR ALL
F Static Discharger - Location and Detail ** ON A/C NOT FOR ALL
F Static Discharger - Location and Detail ** ON A/C NOT FOR ALL
3. Job Set-up
Subtask 23-61-41-941-051-A
A. Safety Precautions
   (1) Make sure that the SAFETY BARRIER(S) are in position.
Subtask 23-61-41-860-050-A
B. Aircraft Maintenance Configuration
   (1) Make sure that the ACCESS PLATFORM 12M (40 FT) - ADJUSTABLE is in position.
Subtask 23-61-41-865-052-A
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/ELAC1/NORM/SPLY15CE1B11
49VUFLIGHT CONTROLS/THS/ACTR/MOT219CE2B09
49VUFLIGHT CONTROLS/FLP/CTL AND MONG/SYS16CVB07
49VUAUTO FLT/FAC1/28VDC5CC1B04
49VUAUTO FLT/FAC1/26VAC14CC1B03
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/ELAC1/NORM/SPLY15CE1B06
49VUFLIGHT CONTROLS/THS/ACTR/MOT219CE2B04
49VUFLIGHT CONTROLS/FLP/CTL AND MONG/SYS16CVB02
49VUAUTO FLT/FAC1/28VDC5CC1H10
49VUAUTO FLT/FAC1/26VAC14CC1H09
** ON A/C ALL
105VUFLIGHT CONTROLS/ELAC2/STBY SPLY16CE2A02
105VUFLT CTL/ELAC1/STBY SPLY16CE1A01
121VUAUTO FLT/FAC2/28VDC5CC2M19
121VUAUTO FLT/FAC2/26VAC14CC2M18
121VUFLIGHT CONTROLS/FLP/CTL AND/MONG/SYS28CVQ21
121VUFLIGHT CONTROLS/THS ACTR/MOT319CE3Q17
121VUFLIGHT CONTROLS/THS ACTR/MOT119CE1Q16
121VUFLIGHT CONTROLS/ELAC2/NORM/SPLY15CE2R20
4. Procedure
Subtask 23-61-41-420-051-A ** ON A/C NOT FOR ALL
A. Preparation for Installation
   (1) Clean the component interface and the adjacent area with a clean Textile-Lint free Cotton - (Material No.14SBA1) and Non Aqueous Cleaner-General - - (Material No.08BAA9) .
   (2) Do an inspection of the component interfaces and the adjacent area.
   (3) Make sure that the parts retained from the removed component are clean and in the correct condition.
Subtask 23-61-41-420-051-C ** ON A/C NOT FOR ALL
A. Preparation for Installation
   (1) Clean the component interface and the adjacent area with a clean Textile-Lint free Cotton - (Material No.14SBA1) and Non Aqueous Cleaner-General - - (Material No.08BAA9) .
   (2) Do an inspection of the component interfaces and the adjacent area.
   (3) Make sure that the parts retained from the removed component are clean and in the correct condition.
Subtask 23-61-41-420-050-A
B. Installation of the Static Discharger
   (1) Install the static discharger (1) in the static discharger retainer (3).
   (2) TORQUE the grub screw (2) to between 0.21 and 0.19 m.daN (18.58 and 16.81 lbf.in ) T.
Subtask 23-61-41-750-050-A
C. Test
   (1) Do a resistance test between the static discharger (1) and the static discharger retainer (3) (Ref. AMM TASK 23-61-00-200-001).
5. Close-up
Subtask 23-61-41-410-051-A
A. Close Access
   (1) Remove the access platform(s).
Subtask 23-61-41-865-051-A
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/ELAC1/NORM/SPLY15CE1B11
49VUFLIGHT CONTROLS/THS/ACTR/MOT219CE2B09
49VUFLIGHT CONTROLS/FLP/CTL AND MONG/SYS16CVB07
49VUAUTO FLT/FAC1/28VDC5CC1B04
49VUAUTO FLT/FAC1/26VAC14CC1B03
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/ELAC1/NORM/SPLY15CE1B06
49VUFLIGHT CONTROLS/THS/ACTR/MOT219CE2B04
49VUFLIGHT CONTROLS/FLP/CTL AND MONG/SYS16CVB02
49VUAUTO FLT/FAC1/28VDC5CC1H10
49VUAUTO FLT/FAC1/26VAC14CC1H09
** ON A/C ALL
105VUFLIGHT CONTROLS/ELAC2/STBY SPLY16CE2A02
105VUFLT CTL/ELAC1/STBY SPLY16CE1A01
121VUAUTO FLT/FAC2/28VDC5CC2M19
121VUAUTO FLT/FAC2/26VAC14CC2M18
121VUFLIGHT CONTROLS/FLP/CTL AND/MONG/SYS28CVQ21
121VUFLIGHT CONTROLS/THS ACTR/MOT319CE3Q17
121VUFLIGHT CONTROLS/THS ACTR/MOT119CE1Q16
121VUFLIGHT CONTROLS/ELAC2/NORM/SPLY15CE2R20
Subtask 23-61-41-942-050-A
C. Remove the Equipment
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Remove the SAFETY BARRIER(S).
   (3) Remove the WARNING NOTICE(S).
   (4) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
[Rev.10 from 2021] 2026.04.01 04:01:45 UTC
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