W DOC AIRBUS | AMM A320F

Removal of the Static Discharger

TASK 23-61-41-000-001-A
Removal of the Static Discharger

WARNING: PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU START A TASK ON OR NEAR:
  • THE FLIGHT CONTROLS
  • THE FLIGHT CONTROL SURFACES
  • THE LANDING GEAR AND THE RELATED DOORS
  • COMPONENTS THAT MOVE.
MOVEMENT OF COMPONENTS CAN KILL OR CAUSE INJURY TO PERSONS AND/OR CAN CAUSE DAMAGE TO THE EQUIPMENT.
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.
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
AR
SAFETY CLIP - CIRCUIT BREAKER
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
300
STABILIZERS AND TAIL UNIT
500
LEFT WING
600
RIGHT WING
 C. Referenced Information
REFERENCE
DESIGNATION
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 23-61-41-941-050-A
A. Safety Precautions
   (1) Put the SAFETY BARRIER(S) in position.
   (2) Put the ACCESS PLATFORM 12M (40 FT) - ADJUSTABLE adjacent to the applicable static discharger.
Subtask 23-61-41-865-050-A
B. Open, safety and tag 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
4. Procedure
Subtask 23-61-41-020-050-A
A. Removal of the Static Discharger
   (1) Loosen the grub screw (2) and remove the static discharger (1) from the static discharger retainer (3).
[Rev.10 from 2021] 2026.04.01 04:01:44 UTC
"Aviabrain" 2025