DOC AIRBUS | AMM A320FInstallation of the Static Discharger Retainer
TASK 23-61-42-400-001-A
Installation of the Static Discharger Retainer
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Consumable Materials
C. Work Zones and Access Panels
D. Expendable Parts
E. Referenced Information
3. Job Set-up
Subtask 23-61-42-941-052-A
Subtask 23-61-42-560-050-M ** ON A/C NOT FOR ALL
Subtask 23-61-42-410-050-A
[Rev.10 from 2021]
2026.04.02 06:12:17 UTC
Installation of the Static Discharger Retainer
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:
BEFORE YOU START WORK, YOU MUST PUT ON A SAFETY HARNESS AND ATTACH IT TO THE ACCESS PLATFORM. WITHOUT A SAFETY HARNESS, YOU CAN FALL. THIS CAN KILL YOU OR CAUSE YOU INJURY.
WARNING:
BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
1. Reason for the JobSelf explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | ACCESS PLATFORM 12M (40 FT) - ADJUSTABLE |
| No specific | AR | SAFETY BARRIER(S) |
| No specific | AR | WARNING NOTICE(S) |
| REFERENCE | DESIGNATION |
|---|---|
| (Material No.06ABA1) | Polysulfide Sealant-Fuel Tank Brushable - |
| (Material No.06ABB1) | Polysulfide Sealant-Fuel Tank Fillet - |
| (Material No.08BAA9) | Non Aqueous Cleaner-General - - |
| (Material No.08BBE1) | Non Aqueous Cleaner-- Methyl Alcohol - |
| (Material No.14SBA1) | Textile-Lint free Cotton - |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 324 | VERTICAL STABILIZER TIP |
| 326 | RUDDER |
| 330 | THS LH AND LH ELEVATOR |
| 340 | THS RH AND RH ELEVATOR |
| 530 | L WG FLAP TAB, FLAP TRACK FAIR & WG TIP |
| 590 | AILERON |
| 630 | RIGHT WING FLAP TRACK FAIR AND WING TIP |
| 690 | AILERON |
E. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| TASK 20-28-00-912-803-A | Bonding Surface Preparation |
| 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 |
| TASK 23-61-41-000-001-A | Removal of the Static Discharger |
| TASK 23-61-41-400-001-A | Installation of the Static Discharger |
| TASK 55-44-11-400-001-A | Installation of the Rudder Tip |
| TASK 57-55-11-400-001-A | Installation of the Flap Track Fairings Nos. 2, 3 and 4 |
| TASK 57-55-11-400-004-A | Installation of the Flap Track Fairings Nos. 2, 3 and 4 |
| SRM 553411 | |
Subtask 23-61-42-941-052-A
A. Safety Precautions
(1) Make sure that the SAFETY BARRIER(S) is(are) in position.
(2) Make sure that the WARNING NOTICE(S) is(are) in position to tell persons not to operate the flight controls.
Subtask 23-61-42-865-051-A (1) Make sure that the SAFETY BARRIER(S) is(are) in position.
(2) Make sure that the WARNING NOTICE(S) is(are) in position to tell persons not to operate the flight controls.
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
Subtask 23-61-42-860-051-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/ELAC1/NORM/SPLY | 15CE1 | B11 |
| 49VU | FLIGHT CONTROLS/THS/ACTR/MOT2 | 19CE2 | B09 |
| 49VU | FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 | 6CV | B07 |
| 49VU | AUTO FLT/FAC1/28VDC | 5CC1 | B04 |
| 49VU | AUTO FLT/FAC1/26VAC | 14CC1 | B03 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/ELAC1/NORM/SPLY | 15CE1 | B06 |
| 49VU | FLIGHT CONTROLS/THS/ACTR/MOT2 | 19CE2 | B04 |
| 49VU | FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 | 6CV | B02 |
| 49VU | AUTO FLT/FAC1/28VDC | 5CC1 | H10 |
| 49VU | AUTO FLT/FAC1/26VAC | 14CC1 | H09 |
| ** ON A/C ALL | |||
| 105VU | FLIGHT CONTROLS/ELAC2/STBY SPLY | 16CE2 | A02 |
| 105VU | FLT CTL/ELAC1/STBY SPLY | 16CE1 | A01 |
| 121VU | AUTO FLT/FAC2/28VDC | 5CC2 | M19 |
| 121VU | AUTO FLT/FAC2/26VAC | 14CC2 | M18 |
| 121VU | FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 | 8CV | Q21 |
| 121VU | FLIGHT CONTROLS/THS ACTR/MOT3 | 19CE3 | Q17 |
| 121VU | FLIGHT CONTROLS/THS ACTR/MOT1 | 19CE1 | Q16 |
| 121VU | FLIGHT CONTROLS/ELAC2/NORM/SPLY | 15CE2 | R20 |
C. Aircraft Maintenance Configuration
(1) Make sure that the ACCESS PLATFORM 12M (40 FT) - ADJUSTABLE is in position below the applicable static discharge retainer.
(2) Make sure that the applicable static discharger is removed (Ref. AMM TASK 23-61-41-000-001).
4. Procedure(1) Make sure that the ACCESS PLATFORM 12M (40 FT) - ADJUSTABLE is in position below the applicable static discharge retainer.
(2) Make sure that the applicable static discharger is removed (Ref. AMM TASK 23-61-41-000-001).
Subtask 23-61-42-560-050-M ** ON A/C NOT FOR ALL
A. Preparation for Installation
(1) For the static discharger retainers at zone 324 (vertical stabilizer tip):
(a) Prepare the electrical bonding of the static discharger retainer (3) (Ref. AMM TASK 20-28-00-912-803).
(b) Replace the static discharger retainer without removal of the lightning protection strip SRM 553411.
(2) For the static discharger retainers at zone 326 (rudder):
(a) Prepare the electrical bonding of the static discharger retainer (1) (Ref. AMM TASK 20-28-00-912-803).
(b) Put the static discharger retainer (1) in the correct position on the aircraft structure.
(c) Drill the holes in the static discharger retainer (1).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(d) Prepare the electrical bonding of the static discharger retainer (3) (Ref. AMM TASK 20-28-00-912-803).
(e) Put the static discharger retainer (3) in the correct position on the aircraft structure.
(f) Drill the holes in the static discharger retainers.
1 Make sure that the holes of the retainers and the related holes in the rudder tip are aligned.
(3) For the static discharger retainers at zone 330 (340) (THS):
(a) Put the adapter (9) in the correct position on the aircraft structure.
(b) Drill the holes in the adapter (9).
1 Make sure that the holes of the adapter and the related holes in the aircraft structure are aligned.
(c) Put the adapter (5) and the static discharger retainer (7) in the correct position on the aircraft structure.
(d) Drill the holes in the adapter (5) and the static discharger retainer (7).
1 Make sure that the holes of the retainer and the related holes in the adapter are aligned.
(e) Put the static discharger retainers (10) and (13) in the correct position on the aircraft structure.
(f) Drill the holes in the static discharger retainers (10) and (13).
1 Make sure that the holes of the retainers and the related holes in the aircraft structure are aligned.
(g) Put the shim (18) in the correct position on the aircraft structure.
(h) Drill the holes in the shim (18).
1 Make sure that the holes of the shim and the related holes in the aircraft structure are aligned.
(i) Put the static discharger retainer (15) in the correct position on the aircraft structure.
(j) Drill the holes in the static discharger retainer (15).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(4) For the static discharger retainers at zone 470 (480) (engine pylon) (if applicable):
Static Discharger Retainers - Engine Pylon and Flap Track Fairings ** ON A/C NOT FOR ALL
Static Discharger Retainers - Flap Track Fairings ** ON A/C NOT FOR ALL
(a) Put the static discharger retainer (10) in the correct position on the aircraft structure.
(b) Drill the holes in the static discharger retainer (10).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(5) For the static discharger retainers at zones 531 (631), 532 (632) and 533 (633) (flap track fairings):
Static Discharger Retainers - Engine Pylon and Flap Track Fairings ** ON A/C NOT FOR ALL
Static Discharger Retainers - Flap Track Fairings ** ON A/C NOT FOR ALL
(a) Put the static discharger retainer (4) in the correct position on the aircraft structure.
(b) Drill the holes in the static discharger retainer (4).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(c) Put the bonding plate (9) in the correct position on the aircraft structure.
(d) Drill the holes in the bonding plate (9).
1 Make sure that the holes of the bonding plate and the related holes in the aircraft structure are aligned.
(6) For the static discharger retainers at zone 590 (690) (ailerons):
(a) Put the static discharger retainers (10) and (14) in the correct position on the aircraft structure.
(b) Drill the holes in the static discharger retainers (10) and (14).
1 Make sure that the holes of the retainers and the related holes in the aircraft structure are aligned.
(7) For the static discharger retainer at zone 534 (634) (wing tip):
(a) Put the static discharger retainer (2) in the correct position on the aircraft structure.
(b) Drill the holes in the static discharger retainer (2).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(8) For the static discharger retainers at zone 534 (634) (wing tip fence):
(a) Put the packer (4) in the correct position on the aircraft structure.
(b) Drill the holes in the packer (4).
1 Make sure that the holes of the packer and the related holes in the aircraft structure are aligned.
(c) Put the static discharger retainer (3) in the correct position on the aircraft structure.
(d) Drill the holes in the static discharger retainer (3).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(e) Put the static discharger retainers (5) in the correct position on the aircraft structure.
(f) Drill the holes in the static discharger retainer (5).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(g) Put the packer (7) in the correct position on the aircraft structure.
(h) Drill the holes in the packer (7).
1 Make sure that the holes of the packer and the related holes in the aircraft structure are aligned.
(i) Put the static discharger retainer (9) in the correct position on the aircraft structure.
(j) Drill the holes in the static discharger retainer (9).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
Subtask 23-61-42-560-050-O ** ON A/C NOT FOR ALL (1) For the static discharger retainers at zone 324 (vertical stabilizer tip):
(a) Prepare the electrical bonding of the static discharger retainer (3) (Ref. AMM TASK 20-28-00-912-803).
(b) Replace the static discharger retainer without removal of the lightning protection strip SRM 553411.
(2) For the static discharger retainers at zone 326 (rudder):
(a) Prepare the electrical bonding of the static discharger retainer (1) (Ref. AMM TASK 20-28-00-912-803).
(b) Put the static discharger retainer (1) in the correct position on the aircraft structure.
(c) Drill the holes in the static discharger retainer (1).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(d) Prepare the electrical bonding of the static discharger retainer (3) (Ref. AMM TASK 20-28-00-912-803).
(e) Put the static discharger retainer (3) in the correct position on the aircraft structure.
(f) Drill the holes in the static discharger retainers.
1 Make sure that the holes of the retainers and the related holes in the rudder tip are aligned.
(3) For the static discharger retainers at zone 330 (340) (THS):
(a) Put the adapter (9) in the correct position on the aircraft structure.
(b) Drill the holes in the adapter (9).
1 Make sure that the holes of the adapter and the related holes in the aircraft structure are aligned.
(c) Put the adapter (5) and the static discharger retainer (7) in the correct position on the aircraft structure.
(d) Drill the holes in the adapter (5) and the static discharger retainer (7).
1 Make sure that the holes of the retainer and the related holes in the adapter are aligned.
(e) Put the static discharger retainers (10) and (13) in the correct position on the aircraft structure.
(f) Drill the holes in the static discharger retainers (10) and (13).
1 Make sure that the holes of the retainers and the related holes in the aircraft structure are aligned.
(g) Put the shim (18) in the correct position on the aircraft structure.
(h) Drill the holes in the shim (18).
1 Make sure that the holes of the shim and the related holes in the aircraft structure are aligned.
(i) Put the static discharger retainer (15) in the correct position on the aircraft structure.
(j) Drill the holes in the static discharger retainer (15).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(4) For the static discharger retainers at zone 470 (480) (engine pylon) (if applicable):
Static Discharger Retainers - Engine Pylon and Flap Track Fairings ** ON A/C NOT FOR ALL Static Discharger Retainers - Flap Track Fairings ** ON A/C NOT FOR ALL (b) Drill the holes in the static discharger retainer (10).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(5) For the static discharger retainers at zones 531 (631), 532 (632) and 533 (633) (flap track fairings):
Static Discharger Retainers - Engine Pylon and Flap Track Fairings ** ON A/C NOT FOR ALL Static Discharger Retainers - Flap Track Fairings ** ON A/C NOT FOR ALL (b) Drill the holes in the static discharger retainer (4).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(c) Put the bonding plate (9) in the correct position on the aircraft structure.
(d) Drill the holes in the bonding plate (9).
1 Make sure that the holes of the bonding plate and the related holes in the aircraft structure are aligned.
(6) For the static discharger retainers at zone 590 (690) (ailerons):
(a) Put the static discharger retainers (10) and (14) in the correct position on the aircraft structure.
(b) Drill the holes in the static discharger retainers (10) and (14).
1 Make sure that the holes of the retainers and the related holes in the aircraft structure are aligned.
(7) For the static discharger retainer at zone 534 (634) (wing tip):
(a) Put the static discharger retainer (2) in the correct position on the aircraft structure.
(b) Drill the holes in the static discharger retainer (2).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(8) For the static discharger retainers at zone 534 (634) (wing tip fence):
(a) Put the packer (4) in the correct position on the aircraft structure.
(b) Drill the holes in the packer (4).
1 Make sure that the holes of the packer and the related holes in the aircraft structure are aligned.
(c) Put the static discharger retainer (3) in the correct position on the aircraft structure.
(d) Drill the holes in the static discharger retainer (3).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(e) Put the static discharger retainers (5) in the correct position on the aircraft structure.
(f) Drill the holes in the static discharger retainer (5).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(g) Put the packer (7) in the correct position on the aircraft structure.
(h) Drill the holes in the packer (7).
1 Make sure that the holes of the packer and the related holes in the aircraft structure are aligned.
(i) Put the static discharger retainer (9) in the correct position on the aircraft structure.
(j) Drill the holes in the static discharger retainer (9).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
A. Preparation for Installation
(1) For the static discharger retainers at zone 324 (vertical stabilizer tip):
(a) Prepare the electrical bonding of the static discharger retainer (3) (Ref. AMM TASK 20-28-00-912-803).
(b) Replace the static discharger retainer without removal of the lightning protection strip SRM 553411.
(2) For the static discharger retainers at zone 326 (rudder):
(a) Prepare the electrical bonding of the static discharger retainer (1) (Ref. AMM TASK 20-28-00-912-803).
(b) Put the static discharger retainer (1) in the correct position on the aircraft structure.
(c) Drill the holes in the static discharger retainer (1).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(d) Prepare the electrical bonding of the static discharger retainer (3) (Ref. AMM TASK 20-28-00-912-803).
(e) Put the static discharger retainer (3) in the correct position on the rudder tip.
(f) Drill the holes in the static discharger retainer (3).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(3) For the static discharger retainers at zone 330 (340) (THS):
(a) Put the adapter (9) in the correct position on the aircraft structure.
(b) Drill the holes in the adapter (9).
1 Make sure that the holes of the adapter and the related holes in the aircraft structure are aligned.
(c) Put the adapter (5) and the static discharger retainer (7) in the correct position on the aircraft structure.
(d) Drill the holes in the adapter (5) and the static discharger retainer (7).
1 Make sure that the holes of the retainer and the related holes in the adapter are aligned.
(e) Put the static discharger retainers (10) and (13) in the correct position on the aircraft structure.
(f) Drill the holes in the static discharger retainers (10) and (13).
1 Make sure that the holes of the retainers and the related hole in the aircraft structure are aligned.
(g) Put the shim (18) in the correct position on the aircraft structure.
(h) Drill the holes in the shim (18).
1 Make sure that the holes of the shim and the related holes in the aircraft structure are aligned.
(i) Put the static discharger retainer (15) in the correct position on the aircraft structure.
(j) Drill the holes in the static discharger retainer (15).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(4) For the static discharger retainers at zone 470 (480) (engine pylon) (if applicable):
(a) Put the static discharger retainer (10) in the correct position on the aircraft structure.
(b) Drill the holes in the static discharger retainer (10).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(5) For the static discharger retainers at zones 531 (631), 532 (632) and 533 (633) (flap track fairings) (if applicable):
(a) Put the static discharger retainer (4) in the correct position on the aircraft structure.
(b) Drill the holes in the static discharger retainer (4).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(c) Put the bonding plate (9) in the correct position on the aircraft structure.
(d) Drill the holes in the bonding plate (9).
1 Make sure that the holes of the bonding plate and the related holes in the aircraft structure are aligned.
(6) For the static discharger retainers at zone 590 (690) (ailerons):
(a) Put the static discharger retainer (2) in the correct position on the aircraft structure.
(b) Drill the holes in the static discharger retainer (2).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(7) For the static discharger retainer at zone 534 (634) (wing tip):
(a) Put the static discharger retainer (2) in the correct position on the aircraft structure.
(b) Drill the holes in the static discharger retainer (2).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(8) For the static discharger retainers at zone 534 (634) (wing tip fence):
(a) Put the packer (3) in the correct position on the aircraft structure.
(b) Drill the holes in the packer (3).
1 Make sure that the holes of the packer and the related holes in the aircraft structure are aligned.
(c) Put the static discharger retainer (2) in the correct position on the aircraft structure.
(d) Drill the holes in the static discharger retainer (2).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(e) Put the static discharger retainers (5) and (7) in the correct position on the aircraft structure.
(f) Drill the holes in the static discharger retainers (5) and (7).
1 Make sure that the holes of the retainers and the related holes in the aircraft structure are aligned.
Subtask 23-61-42-560-050-P ** ON A/C NOT FOR ALL (1) For the static discharger retainers at zone 324 (vertical stabilizer tip):
(a) Prepare the electrical bonding of the static discharger retainer (3) (Ref. AMM TASK 20-28-00-912-803).
(b) Replace the static discharger retainer without removal of the lightning protection strip SRM 553411.
(2) For the static discharger retainers at zone 326 (rudder):
(a) Prepare the electrical bonding of the static discharger retainer (1) (Ref. AMM TASK 20-28-00-912-803).
(b) Put the static discharger retainer (1) in the correct position on the aircraft structure.
(c) Drill the holes in the static discharger retainer (1).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(d) Prepare the electrical bonding of the static discharger retainer (3) (Ref. AMM TASK 20-28-00-912-803).
(e) Put the static discharger retainer (3) in the correct position on the rudder tip.
(f) Drill the holes in the static discharger retainer (3).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(3) For the static discharger retainers at zone 330 (340) (THS):
(a) Put the adapter (9) in the correct position on the aircraft structure.
(b) Drill the holes in the adapter (9).
1 Make sure that the holes of the adapter and the related holes in the aircraft structure are aligned.
(c) Put the adapter (5) and the static discharger retainer (7) in the correct position on the aircraft structure.
(d) Drill the holes in the adapter (5) and the static discharger retainer (7).
1 Make sure that the holes of the retainer and the related holes in the adapter are aligned.
(e) Put the static discharger retainers (10) and (13) in the correct position on the aircraft structure.
(f) Drill the holes in the static discharger retainers (10) and (13).
1 Make sure that the holes of the retainers and the related hole in the aircraft structure are aligned.
(g) Put the shim (18) in the correct position on the aircraft structure.
(h) Drill the holes in the shim (18).
1 Make sure that the holes of the shim and the related holes in the aircraft structure are aligned.
(i) Put the static discharger retainer (15) in the correct position on the aircraft structure.
(j) Drill the holes in the static discharger retainer (15).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(4) For the static discharger retainers at zone 470 (480) (engine pylon) (if applicable):
(a) Put the static discharger retainer (10) in the correct position on the aircraft structure.
(b) Drill the holes in the static discharger retainer (10).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(5) For the static discharger retainers at zones 531 (631), 532 (632) and 533 (633) (flap track fairings) (if applicable):
(a) Put the static discharger retainer (4) in the correct position on the aircraft structure.
(b) Drill the holes in the static discharger retainer (4).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(c) Put the bonding plate (9) in the correct position on the aircraft structure.
(d) Drill the holes in the bonding plate (9).
1 Make sure that the holes of the bonding plate and the related holes in the aircraft structure are aligned.
(6) For the static discharger retainers at zone 590 (690) (ailerons):
(a) Put the static discharger retainer (2) in the correct position on the aircraft structure.
(b) Drill the holes in the static discharger retainer (2).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(7) For the static discharger retainer at zone 534 (634) (wing tip):
(a) Put the static discharger retainer (2) in the correct position on the aircraft structure.
(b) Drill the holes in the static discharger retainer (2).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(8) For the static discharger retainers at zone 534 (634) (wing tip fence):
(a) Put the packer (3) in the correct position on the aircraft structure.
(b) Drill the holes in the packer (3).
1 Make sure that the holes of the packer and the related holes in the aircraft structure are aligned.
(c) Put the static discharger retainer (2) in the correct position on the aircraft structure.
(d) Drill the holes in the static discharger retainer (2).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(e) Put the static discharger retainers (5) and (7) in the correct position on the aircraft structure.
(f) Drill the holes in the static discharger retainers (5) and (7).
1 Make sure that the holes of the retainers and the related holes in the aircraft structure are aligned.
A. Preparation for Installation
(1) For the static discharger retainers at zone 324 (vertical stabilizer tip):
(a) Prepare the electrical bonding of the static discharger retainer (3) (Ref. AMM TASK 20-28-00-912-803).
(b) Replace the static discharger retainer without removal of the lightning protection strip SRM 553411.
(2) For the static discharger retainers at zone 326 (rudder):
(a) Prepare the electrical bonding of the static discharger retainer (1) (Ref. AMM TASK 20-28-00-912-803).
(b) Put the static discharger retainer (1) in the correct position on the aircraft structure.
(c) Drill the holes in the static discharger retainer (1).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(d) Prepare the electrical bonding of the static discharger retainer (3) (Ref. AMM TASK 20-28-00-912-803).
(e) Put the static discharger retainer (3) in the correct position on the rudder tip.
(f) Drill the holes in the static discharger retainer (3).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(3) For the static discharger retainers at zone 330 (340) (THS):
(a) Put the adapter (9) in the correct position on the aircraft structure.
(b) Drill the holes in the adapter (9).
1 Make sure that the holes of the adapter and the related holes in the aircraft structure are aligned.
(c) Put the adapter (5) and the static discharger retainer (7) in the correct position on the aircraft structure.
(d) Drill the holes in the adapter (5) and the static discharger retainer (7).
1 Make sure that the holes of the retainer and the related holes in the adapter are aligned.
(e) Put the static discharger retainers (10) and (13) in the correct position on the aircraft structure.
(f) Drill the holes in the static discharger retainers (10) and (13).
1 Make sure that the holes of the retainers and the related hole in the aircraft structure are aligned.
(g) Put the shim (18) in the correct position on the aircraft structure.
(h) Drill the holes in the shim (18).
1 Make sure that the holes of the shim and the related holes in the aircraft structure are aligned.
(i) Put the static discharger retainer (15) in the correct position on the aircraft structure.
(j) Drill the holes in the static discharger retainer (15).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(4) For the static discharger retainers at zone 470 (480) (engine pylon) (if applicable):
(a) Put the static discharger retainer (10) in the correct position on the aircraft structure.
(b) Drill the holes in the static discharger retainer (10).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(5) For the static discharger retainers at zones 531 (631), 532 (632) and 533 (633) (flap track fairings) (if applicable):
(a) Put the static discharger retainer (4) in the correct position on the aircraft structure.
(b) Drill the holes in the static discharger retainer (4).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(c) Put the bonding plate (9) in the correct position on the aircraft structure.
(d) Drill the holes in the bonding plate (9).
1 Make sure that the holes of the bonding plate and the related holes in the aircraft structure are aligned.
(6) For the static discharger retainers at zone 590 (690) (ailerons):
(a) Put the static discharger retainer (2) in the correct position on the aircraft structure.
(b) Drill the holes in the static discharger retainer (2).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(7) For the static discharger retainers at zone 534 (634) (sharklet):
(a) Put the static discharger retainers (2), (7), (11), (17) and (22) in the correct position on the aircraft structure.
(b) Drill the holes in the static discharger retainers (2), (7), (11), (17) and (22).
1 Make sure that the holes of the retainers and the related holes in the aircraft structure are aligned.
Subtask 23-61-42-560-050-Q ** ON A/C NOT FOR ALL (1) For the static discharger retainers at zone 324 (vertical stabilizer tip):
(a) Prepare the electrical bonding of the static discharger retainer (3) (Ref. AMM TASK 20-28-00-912-803).
(b) Replace the static discharger retainer without removal of the lightning protection strip SRM 553411.
(2) For the static discharger retainers at zone 326 (rudder):
(a) Prepare the electrical bonding of the static discharger retainer (1) (Ref. AMM TASK 20-28-00-912-803).
(b) Put the static discharger retainer (1) in the correct position on the aircraft structure.
(c) Drill the holes in the static discharger retainer (1).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(d) Prepare the electrical bonding of the static discharger retainer (3) (Ref. AMM TASK 20-28-00-912-803).
(e) Put the static discharger retainer (3) in the correct position on the rudder tip.
(f) Drill the holes in the static discharger retainer (3).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(3) For the static discharger retainers at zone 330 (340) (THS):
(a) Put the adapter (9) in the correct position on the aircraft structure.
(b) Drill the holes in the adapter (9).
1 Make sure that the holes of the adapter and the related holes in the aircraft structure are aligned.
(c) Put the adapter (5) and the static discharger retainer (7) in the correct position on the aircraft structure.
(d) Drill the holes in the adapter (5) and the static discharger retainer (7).
1 Make sure that the holes of the retainer and the related holes in the adapter are aligned.
(e) Put the static discharger retainers (10) and (13) in the correct position on the aircraft structure.
(f) Drill the holes in the static discharger retainers (10) and (13).
1 Make sure that the holes of the retainers and the related hole in the aircraft structure are aligned.
(g) Put the shim (18) in the correct position on the aircraft structure.
(h) Drill the holes in the shim (18).
1 Make sure that the holes of the shim and the related holes in the aircraft structure are aligned.
(i) Put the static discharger retainer (15) in the correct position on the aircraft structure.
(j) Drill the holes in the static discharger retainer (15).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(4) For the static discharger retainers at zone 470 (480) (engine pylon) (if applicable):
(a) Put the static discharger retainer (10) in the correct position on the aircraft structure.
(b) Drill the holes in the static discharger retainer (10).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(5) For the static discharger retainers at zones 531 (631), 532 (632) and 533 (633) (flap track fairings) (if applicable):
(a) Put the static discharger retainer (4) in the correct position on the aircraft structure.
(b) Drill the holes in the static discharger retainer (4).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(c) Put the bonding plate (9) in the correct position on the aircraft structure.
(d) Drill the holes in the bonding plate (9).
1 Make sure that the holes of the bonding plate and the related holes in the aircraft structure are aligned.
(6) For the static discharger retainers at zone 590 (690) (ailerons):
(a) Put the static discharger retainer (2) in the correct position on the aircraft structure.
(b) Drill the holes in the static discharger retainer (2).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(7) For the static discharger retainers at zone 534 (634) (sharklet):
(a) Put the static discharger retainers (2), (7), (11), (17) and (22) in the correct position on the aircraft structure.
(b) Drill the holes in the static discharger retainers (2), (7), (11), (17) and (22).
1 Make sure that the holes of the retainers and the related holes in the aircraft structure are aligned.
A. Preparation for Installation
(1) For the static discharger retainers at zone 324 (vertical stabilizer tip):
(a) Prepare the electrical bonding of the static discharger retainer (3) (Ref. AMM TASK 20-28-00-912-803).
(b) Replace the static discharger retainer without removal of the lightning protection strip SRM 553411.
(2) For the static discharger retainers at zone 326 (rudder):
(a) Prepare the electrical bonding of the static discharger retainer (1) (Ref. AMM TASK 20-28-00-912-803).
(b) Put the static discharger retainer (1) in the correct position on the aircraft structure.
(c) Drill the holes in the static discharger retainer (1).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(d) Prepare the electrical bonding of the static discharger retainer (3) (Ref. AMM TASK 20-28-00-912-803).
(e) Put the static discharger retainer (3) in the correct position on the rudder tip.
(f) Drill the holes in the static discharger retainer (3).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(3) For the static discharger retainers at zone 330 (340) (THS):
(a) Put the adapter (9) in the correct position on the aircraft structure.
(b) Drill the holes in the adapter (9).
1 Make sure that the holes of the adapter and the related holes in the aircraft structure are aligned.
(c) Put the adapter (5) and the static discharger retainer (7) in the correct position on the aircraft structure.
(d) Drill the holes in the adapter (5) and the static discharger retainer (7).
1 Make sure that the holes of the retainer and the related holes in the adapter are aligned.
(e) Put the static discharger retainers (10) and (13) in the correct position on the aircraft structure.
(f) Drill the holes in the static discharger retainers (10) and (13).
1 Make sure that the holes of the retainers and the related holes in the aircraft structure are aligned.
(g) Put the shim (18) in the correct position on the aircraft structure.
(h) Drill the holes in the shim (18).
1 Make sure that the holes of the shim and the related holes in the aircraft structure are aligned.
(i) Put the static discharger retainer (15) in the correct position on the aircraft structure.
(j) Drill the holes in the static discharger retainer (15).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(4) For the static discharger retainers at zone 470 (480) (engine pylon) (if applicable):
(a) Put the static discharger retainer (10) in the correct position on the aircraft structure.
(b) Drill the holes in the static discharger retainer (10).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(5) For the static discharger retainers at zones 531 (631), 532 (632) and 533 (633) (flap track fairings) (if applicable):
(a) Put the static discharger retainer (4) in the correct position on the aircraft structure.
(b) Drill the holes in the static discharger retainer (4).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(c) Put the bonding plate (9) in the correct position on the aircraft structure.
(d) Drill the holes in the bonding plate (9).
1 Make sure that the holes of the bonding plate and the related holes in the aircraft structure are aligned.
(6) For the static discharger retainers at zone 590 (690) (ailerons):
(a) Put the static discharger retainer (2) in the correct position on the aircraft structure.
(b) Drill the holes in the static discharger retainer (2).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(7) For the static discharger retainer at zone 534 (634) (wing-tip):
(a) Put the static discharger retainer (2) in the correct position on the aircraft structure.
(b) Drill the holes in the static discharger retainer (2).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(8) For the static discharger retainer at zone 534 (634) (wing tip fence):
(a) Put the packer (4) in the correct position on the aircraft structure.
(b) Drill the holes in the packer (4).
1 Make sure that the holes of the packer and the related holes in the aircraft structure are aligned.
(c) Put the static discharger retainer (3) in the correct position on the aircraft structure.
(d) Drill the holes in the static discharger retainer (3).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(e) Put the static discharger retainers (5) in the correct position on the aircraft structure.
(f) Drill the holes in the static discharger retainers (5).
1 Make sure that the holes of the retainers and the related holes in the aircraft structure are aligned.
(g) Put the packer (7) in the correct position on the aircraft structure.
(h) Drill the holes in the packer (7).
1 Make sure that the holes of the packer and the related holes in the aircraft structure are aligned.
(i) Put the static discharger retainer (9) in the correct position on the aircraft structure.
(j) Drill the holes in the static discharger retainer (9).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
Subtask 23-61-42-560-050-R (1) For the static discharger retainers at zone 324 (vertical stabilizer tip):
(a) Prepare the electrical bonding of the static discharger retainer (3) (Ref. AMM TASK 20-28-00-912-803).
(b) Replace the static discharger retainer without removal of the lightning protection strip SRM 553411.
(2) For the static discharger retainers at zone 326 (rudder):
(a) Prepare the electrical bonding of the static discharger retainer (1) (Ref. AMM TASK 20-28-00-912-803).
(b) Put the static discharger retainer (1) in the correct position on the aircraft structure.
(c) Drill the holes in the static discharger retainer (1).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(d) Prepare the electrical bonding of the static discharger retainer (3) (Ref. AMM TASK 20-28-00-912-803).
(e) Put the static discharger retainer (3) in the correct position on the rudder tip.
(f) Drill the holes in the static discharger retainer (3).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(3) For the static discharger retainers at zone 330 (340) (THS):
(a) Put the adapter (9) in the correct position on the aircraft structure.
(b) Drill the holes in the adapter (9).
1 Make sure that the holes of the adapter and the related holes in the aircraft structure are aligned.
(c) Put the adapter (5) and the static discharger retainer (7) in the correct position on the aircraft structure.
(d) Drill the holes in the adapter (5) and the static discharger retainer (7).
1 Make sure that the holes of the retainer and the related holes in the adapter are aligned.
(e) Put the static discharger retainers (10) and (13) in the correct position on the aircraft structure.
(f) Drill the holes in the static discharger retainers (10) and (13).
1 Make sure that the holes of the retainers and the related holes in the aircraft structure are aligned.
(g) Put the shim (18) in the correct position on the aircraft structure.
(h) Drill the holes in the shim (18).
1 Make sure that the holes of the shim and the related holes in the aircraft structure are aligned.
(i) Put the static discharger retainer (15) in the correct position on the aircraft structure.
(j) Drill the holes in the static discharger retainer (15).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(4) For the static discharger retainers at zone 470 (480) (engine pylon) (if applicable):
(a) Put the static discharger retainer (10) in the correct position on the aircraft structure.
(b) Drill the holes in the static discharger retainer (10).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(5) For the static discharger retainers at zones 531 (631), 532 (632) and 533 (633) (flap track fairings) (if applicable):
(a) Put the static discharger retainer (4) in the correct position on the aircraft structure.
(b) Drill the holes in the static discharger retainer (4).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(c) Put the bonding plate (9) in the correct position on the aircraft structure.
(d) Drill the holes in the bonding plate (9).
1 Make sure that the holes of the bonding plate and the related holes in the aircraft structure are aligned.
(6) For the static discharger retainers at zone 590 (690) (ailerons):
(a) Put the static discharger retainer (2) in the correct position on the aircraft structure.
(b) Drill the holes in the static discharger retainer (2).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(7) For the static discharger retainer at zone 534 (634) (wing-tip):
(a) Put the static discharger retainer (2) in the correct position on the aircraft structure.
(b) Drill the holes in the static discharger retainer (2).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(8) For the static discharger retainer at zone 534 (634) (wing tip fence):
(a) Put the packer (4) in the correct position on the aircraft structure.
(b) Drill the holes in the packer (4).
1 Make sure that the holes of the packer and the related holes in the aircraft structure are aligned.
(c) Put the static discharger retainer (3) in the correct position on the aircraft structure.
(d) Drill the holes in the static discharger retainer (3).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(e) Put the static discharger retainers (5) in the correct position on the aircraft structure.
(f) Drill the holes in the static discharger retainers (5).
1 Make sure that the holes of the retainers and the related holes in the aircraft structure are aligned.
(g) Put the packer (7) in the correct position on the aircraft structure.
(h) Drill the holes in the packer (7).
1 Make sure that the holes of the packer and the related holes in the aircraft structure are aligned.
(i) Put the static discharger retainer (9) in the correct position on the aircraft structure.
(j) Drill the holes in the static discharger retainer (9).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
A. Preparation for Installation
(1) For the static discharger retainers at zone 324 (vertical stabilizer tip):
(a) Prepare the electrical bonding of the static discharger retainer (3) (Ref. AMM TASK 20-28-00-912-803).
(b) Replace the static discharger retainer without removal of the lightning protection strip SRM 553411.
(2) For the static discharger retainers at zone 326 (rudder):
(a) Prepare the electrical bonding of the static discharger retainer (1) (Ref. AMM TASK 20-28-00-912-803).
(b) Put the static discharger retainer (1) in the correct position on the aircraft structure.
(c) Drill the holes in the static discharger retainer (1).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(d) Prepare the electrical bonding of the static discharger retainer (3) (Ref. AMM TASK 20-28-00-912-803).
(e) Put the static discharger retainer (3) in the correct position on the rudder tip.
(f) Drill the holes in the static discharger retainer (3).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(3) For the static discharger retainers at zone 330 (340) (THS):
(a) Put the adapter (9) in the correct position on the aircraft structure.
(b) Drill the holes in the adapter (9).
1 Make sure that the holes of the adapter and the related holes in the aircraft structure are aligned.
(c) Put the adapter (5) and the static discharger retainer (7) in the correct position on the aircraft structure.
(d) Drill the holes in the adapter (5) and the static discharger retainer (7).
1 Make sure that the holes of the retainer and the related holes in the adapter are aligned.
(e) Put the static discharger retainers (10) and (13) in the correct position on the aircraft structure.
(f) Drill the holes in the static discharger retainers (10) and (13).
1 Make sure that the holes of the retainers and the related holes in the aircraft structure are aligned.
(g) Put the shim (18) in the correct position on the aircraft structure.
(h) Drill the holes in the shim (18).
1 Make sure that the holes of the shim and the related holes in the aircraft structure are aligned.
(i) Put the static discharger retainer (15) in the correct position on the aircraft structure.
(j) Drill the holes in the static discharger retainer (15).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(4) For the static discharger retainers at zone 470 (480) (engine pylon) (if applicable):
(a) Put the static discharger retainer (10) in the correct position on the aircraft structure.
(b) Drill the holes in the static discharger retainer (10).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(5) For the static discharger retainers at zones 531 (631), 532 (632) and 533 (633) (flap track fairings) (if applicable):
(a) Put the static discharger retainer (4) in the correct position on the aircraft structure.
(b) Drill the holes in the static discharger retainer (4).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(c) Put the bonding plate (9) in the correct position on the aircraft structure.
(d) Drill the holes in the bonding plate (9).
1 Make sure that the holes of the bonding plate and the related holes in the aircraft structure are aligned.
(6) For the static discharger retainers at zone 590 (690) (ailerons):
(a) Put the static discharger retainer (2) in the correct position on the aircraft structure.
(b) Drill the holes in the static discharger retainer (2).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(7) For the static discharger retainer at zone 534 (634) (sharklet):
(a) Put the static discharger retainers (2), (7), (11), (17) and (22) in the correct position on the aircraft structure.
(b) Drill the holes in the static discharger retainers (2), (7), (11), (17) and (22).
1 Make sure that the holes of the retainers and the related holes in the aircraft structure are aligned.
Subtask 23-61-42-420-053-A (1) For the static discharger retainers at zone 324 (vertical stabilizer tip):
(a) Prepare the electrical bonding of the static discharger retainer (3) (Ref. AMM TASK 20-28-00-912-803).
(b) Replace the static discharger retainer without removal of the lightning protection strip SRM 553411.
(2) For the static discharger retainers at zone 326 (rudder):
(a) Prepare the electrical bonding of the static discharger retainer (1) (Ref. AMM TASK 20-28-00-912-803).
(b) Put the static discharger retainer (1) in the correct position on the aircraft structure.
(c) Drill the holes in the static discharger retainer (1).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(d) Prepare the electrical bonding of the static discharger retainer (3) (Ref. AMM TASK 20-28-00-912-803).
(e) Put the static discharger retainer (3) in the correct position on the rudder tip.
(f) Drill the holes in the static discharger retainer (3).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(3) For the static discharger retainers at zone 330 (340) (THS):
(a) Put the adapter (9) in the correct position on the aircraft structure.
(b) Drill the holes in the adapter (9).
1 Make sure that the holes of the adapter and the related holes in the aircraft structure are aligned.
(c) Put the adapter (5) and the static discharger retainer (7) in the correct position on the aircraft structure.
(d) Drill the holes in the adapter (5) and the static discharger retainer (7).
1 Make sure that the holes of the retainer and the related holes in the adapter are aligned.
(e) Put the static discharger retainers (10) and (13) in the correct position on the aircraft structure.
(f) Drill the holes in the static discharger retainers (10) and (13).
1 Make sure that the holes of the retainers and the related holes in the aircraft structure are aligned.
(g) Put the shim (18) in the correct position on the aircraft structure.
(h) Drill the holes in the shim (18).
1 Make sure that the holes of the shim and the related holes in the aircraft structure are aligned.
(i) Put the static discharger retainer (15) in the correct position on the aircraft structure.
(j) Drill the holes in the static discharger retainer (15).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(4) For the static discharger retainers at zone 470 (480) (engine pylon) (if applicable):
(a) Put the static discharger retainer (10) in the correct position on the aircraft structure.
(b) Drill the holes in the static discharger retainer (10).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(5) For the static discharger retainers at zones 531 (631), 532 (632) and 533 (633) (flap track fairings) (if applicable):
(a) Put the static discharger retainer (4) in the correct position on the aircraft structure.
(b) Drill the holes in the static discharger retainer (4).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(c) Put the bonding plate (9) in the correct position on the aircraft structure.
(d) Drill the holes in the bonding plate (9).
1 Make sure that the holes of the bonding plate and the related holes in the aircraft structure are aligned.
(6) For the static discharger retainers at zone 590 (690) (ailerons):
(a) Put the static discharger retainer (2) in the correct position on the aircraft structure.
(b) Drill the holes in the static discharger retainer (2).
1 Make sure that the holes of the retainer and the related holes in the aircraft structure are aligned.
(7) For the static discharger retainer at zone 534 (634) (sharklet):
(a) Put the static discharger retainers (2), (7), (11), (17) and (22) in the correct position on the aircraft structure.
(b) Drill the holes in the static discharger retainers (2), (7), (11), (17) and (22).
1 Make sure that the holes of the retainers and the related holes in the aircraft structure are aligned.
B. Preparation for Installation of the Static Discharger Retainers at Zones 324 (Vertical Stabilizer Tip) , 326 (Rudder) and 330 (340) (THS)
(1) Clean the applicable component interfaces and the adjacent area with a Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) .
(2) Make sure that the parts retained from the removed component are clean and in the correct condition.
(3) Do an inspection of the component interfaces and the adjacent area.
(4) Apply a layer of Polysulfide Sealant-Fuel Tank Fillet - (Material No.06ABB1) to the interface of the applicable static discharger retainer.
Subtask 23-61-42-420-054-C ** ON A/C NOT FOR ALL (1) Clean the applicable component interfaces and the adjacent area with a Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) .
(2) Make sure that the parts retained from the removed component are clean and in the correct condition.
(3) Do an inspection of the component interfaces and the adjacent area.
(4) Apply a layer of Polysulfide Sealant-Fuel Tank Fillet - (Material No.06ABB1) to the interface of the applicable static discharger retainer.
C. Preparation for Installation of the Static Discharger Retainers in Zones 470 (480) (Engine Pylon) and 531 (631), 532 (632) and 533 (633) (Flap Track Fairings)
(1) Clean the applicable component interfaces and the adjacent area with a Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) .
(2) Make sure that the parts retained from the removed component are clean and in the correct condition.
(3) Do an inspection of the component interfaces and the adjacent area.
(4) Apply a layer of Polysulfide Sealant-Fuel Tank Brushable - (Material No.06ABA1) to the interface of the bonding plate (9) and the static discharger retainer (4).
(5) Put the bonding plate (9) and the static discharger retainer (4) in position on the aircraft structure.
(6) Apply pressure to the bonding plate (9) and the static discharger retainer (4) to compress the sealant.
Subtask 23-61-42-420-054-D ** ON A/C NOT FOR ALL (1) Clean the applicable component interfaces and the adjacent area with a Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) .
(2) Make sure that the parts retained from the removed component are clean and in the correct condition.
(3) Do an inspection of the component interfaces and the adjacent area.
(4) Apply a layer of Polysulfide Sealant-Fuel Tank Brushable - (Material No.06ABA1) to the interface of the bonding plate (9) and the static discharger retainer (4).
(5) Put the bonding plate (9) and the static discharger retainer (4) in position on the aircraft structure.
(6) Apply pressure to the bonding plate (9) and the static discharger retainer (4) to compress the sealant.
NOTE: This lets the surface of the bonding plate (9) and the static discharger (4) to touch the anti-static paint surface.
(7) On the composite engine-pylon fairing, do not apply sealant to the static discharger retainer (10). NOTE: The correct bonding resistance is only possible when the retainer (10) touches the engine-pylon fairing.
C. Preparation for Installation of the Static Discharger Retainers in Zones 470 (480) (Engine Pylon) and 531 (631), 532 (632) and 533 (633) (Flap Track Fairings)
(1) Clean the applicable component interfaces and the adjacent area with a Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) .
(2) Make sure that the parts retained from the removed component are clean and in the correct condition.
(3) Do an inspection of the component interfaces and the adjacent area.
(4) Apply a layer of Polysulfide Sealant-Fuel Tank Brushable - (Material No.06ABA1) to the interface of the plate (9) and the static discharger retainer (4).
(5) Put the plate (9) and the static discharger retainer (4) in position on the aircraft structure.
(6) Apply pressure to the bonding plate (9) and the static discharger retainer (4) to compress the sealant.
Subtask 23-61-42-420-055-A (1) Clean the applicable component interfaces and the adjacent area with a Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) .
(2) Make sure that the parts retained from the removed component are clean and in the correct condition.
(3) Do an inspection of the component interfaces and the adjacent area.
(4) Apply a layer of Polysulfide Sealant-Fuel Tank Brushable - (Material No.06ABA1) to the interface of the plate (9) and the static discharger retainer (4).
(5) Put the plate (9) and the static discharger retainer (4) in position on the aircraft structure.
(6) Apply pressure to the bonding plate (9) and the static discharger retainer (4) to compress the sealant.
NOTE: This lets the surface of the bonding plate (9) and the static discharger (4) to touch the anti-static paint surface.
D. Preparation for Installation of the Static Discharger Retainers at Zone 590 (690) (Aileron)
Static Discharger Retainers - Ailerons ** ON A/C NOT FOR ALL
Static Discharger Retainers - Ailerons ** ON A/C NOT FOR ALL
(1) Clean the applicable component interfaces and the adjacent area with a Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) .
(2) Make sure that the parts retained from the removed component are clean and in the correct condition.
(3) Do an inspection of the component interfaces and the adjacent area.
(4) Apply a layer of Polysulfide Sealant-Fuel Tank Fillet - (Material No.06ABB1) to the interface of the applicable static discharger retainer.
Subtask 23-61-42-420-056-B ** ON A/C NOT FOR ALL Static Discharger Retainers - Ailerons ** ON A/C NOT FOR ALL Static Discharger Retainers - Ailerons ** ON A/C NOT FOR ALL (2) Make sure that the parts retained from the removed component are clean and in the correct condition.
(3) Do an inspection of the component interfaces and the adjacent area.
(4) Apply a layer of Polysulfide Sealant-Fuel Tank Fillet - (Material No.06ABB1) to the interface of the applicable static discharger retainer.
E. Preparation for Installation of the Static Discharger Retainer at Zone 534 (634) (Wing-Tip)
(1) Clean the applicable component interfaces and the adjacent area with a Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) .
(2) Make sure that the parts retained from the removed component are clean and in the correct condition.
(3) Do an inspection of the component interfaces and the adjacent area.
(4) Apply a layer of Polysulfide Sealant-Fuel Tank Fillet - (Material No.06ABB1) to the interface of the applicable static discharger retainer.
Subtask 23-61-42-420-057-A ** ON A/C NOT FOR ALL (1) Clean the applicable component interfaces and the adjacent area with a Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) .
(2) Make sure that the parts retained from the removed component are clean and in the correct condition.
(3) Do an inspection of the component interfaces and the adjacent area.
(4) Apply a layer of Polysulfide Sealant-Fuel Tank Fillet - (Material No.06ABB1) to the interface of the applicable static discharger retainer.
F. Preparation for Installation of the Static Discharger Retainers at Zone 534 (634) (Wing-Tip Fence)
Static Discharger Retainers - Wing Tip Fences ** ON A/C NOT FOR ALL
Static Discharger Retainers - Wing Tip Fences ** ON A/C NOT FOR ALL
(1) Clean the applicable component interfaces and the adjacent area with a Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) .
(2) Make sure that the parts retained from the removed component are clean and in the correct condition.
(3) Do an inspection of the component interfaces and the adjacent area.
(4) Apply a layer of Polysulfide Sealant-Fuel Tank Fillet - (Material No.06ABB1) to the interface of the applicable static discharger retainer.
Subtask 23-61-42-420-063-A ** ON A/C NOT FOR ALL Static Discharger Retainers - Wing Tip Fences ** ON A/C NOT FOR ALL Static Discharger Retainers - Wing Tip Fences ** ON A/C NOT FOR ALL (2) Make sure that the parts retained from the removed component are clean and in the correct condition.
(3) Do an inspection of the component interfaces and the adjacent area.
(4) Apply a layer of Polysulfide Sealant-Fuel Tank Fillet - (Material No.06ABB1) to the interface of the applicable static discharger retainer.
G. Preparation for Installation of the Static Discharger Retainers at Zone 534 (634) (Sharklet)
(1) Clean the applicable component interfaces and the adjacent area with a Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) .
(2) Make sure that the parts retained from the removed component are clean and in the correct condition.
(3) Do an inspection of the component interfaces and the adjacent area.
(4) Apply a layer of Polysulfide Sealant-Fuel Tank Fillet - (Material No.06ABB1) to the interface of the applicable static discharger retainer.
Subtask 23-61-42-420-058-A (1) Clean the applicable component interfaces and the adjacent area with a Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) .
(2) Make sure that the parts retained from the removed component are clean and in the correct condition.
(3) Do an inspection of the component interfaces and the adjacent area.
(4) Apply a layer of Polysulfide Sealant-Fuel Tank Fillet - (Material No.06ABB1) to the interface of the applicable static discharger retainer.
H. Installation of the Static Discharger Retainers at Zones 326 (Rudder) and 330 (340) (THS)
(1) On the rudder trailing edge:
(a) Put the retainer (1) in position and install it with the AIPC 23-61-04-01-040 RIVETS (2) or AIPC 23-61-84-01-040 RIVETS (2) and the AIPC 23-61-04-01-041 RIVETS (2) or AIPC 23-61-84-01-040 RIVETS (2).
(2) On the rudder tip:
(a) Put the retainer (3) in position and install it with the AIPC 23-61-04-01-060 RIVETS (4) or AIPC 23-61-84-01-110 RIVETS (4), and AIPC 23-61-04-01-080 RIVETS (4) or AIPC 23-61-84-01-080 RIVETS (4).
(b) Install the rudder tip (Ref. AMM TASK 55-44-11-400-001).
(3) On the THS:
(a) Put the adapter (5) in position and install it with the AIPC 23-61-07-01-052 RIVETS (6) or AIPC 23-61-87-01-050 RIVETS (6).
(b) Put the retainer (7) in position and install it with the AIPC 23-61-07-01-051 RIVETS (8) or AIPC 23-61-87-01-050 RIVETS (8).
(c) Put the adapter (9) and the retainer (10) in position and install it with the AIPC 23-61-07-01-070 RIVETS (11) or AIPC 23-61-87-01-070 RIVETS (11) and the AIPC 23-61-07-01-060 RIVETS (12) or AIPC 23-61-87-01-060 RIVETS (12).
(d) Put the retainer (13) in position and install it with the AIPC 23-61-07-01-050 RIVETS (14) or AIPC 23-61-87-01-040 RIVETS (14).
(e) Put the retainer (15) in position with the shim (18) and install it with the AIPC 23-61-07-01-040 RIVETS (16) or AIPC 23-61-87-01-030 RIVETS (16) and the AIPC 23-61-07-01-130 RIVETS (17) or AIPC 23-61-87-01-030 RIVETS (17).
(4) Use a clean Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) to remove the unwanted sealant from around the applicable static discharger retainer.
Subtask 23-61-42-420-059-C ** ON A/C NOT FOR ALL (1) On the rudder trailing edge:
(a) Put the retainer (1) in position and install it with the AIPC 23-61-04-01-040 RIVETS (2) or AIPC 23-61-84-01-040 RIVETS (2) and the AIPC 23-61-04-01-041 RIVETS (2) or AIPC 23-61-84-01-040 RIVETS (2).
(2) On the rudder tip:
(a) Put the retainer (3) in position and install it with the AIPC 23-61-04-01-060 RIVETS (4) or AIPC 23-61-84-01-110 RIVETS (4), and AIPC 23-61-04-01-080 RIVETS (4) or AIPC 23-61-84-01-080 RIVETS (4).
(b) Install the rudder tip (Ref. AMM TASK 55-44-11-400-001).
(3) On the THS:
(a) Put the adapter (5) in position and install it with the AIPC 23-61-07-01-052 RIVETS (6) or AIPC 23-61-87-01-050 RIVETS (6).
(b) Put the retainer (7) in position and install it with the AIPC 23-61-07-01-051 RIVETS (8) or AIPC 23-61-87-01-050 RIVETS (8).
(c) Put the adapter (9) and the retainer (10) in position and install it with the AIPC 23-61-07-01-070 RIVETS (11) or AIPC 23-61-87-01-070 RIVETS (11) and the AIPC 23-61-07-01-060 RIVETS (12) or AIPC 23-61-87-01-060 RIVETS (12).
(d) Put the retainer (13) in position and install it with the AIPC 23-61-07-01-050 RIVETS (14) or AIPC 23-61-87-01-040 RIVETS (14).
(e) Put the retainer (15) in position with the shim (18) and install it with the AIPC 23-61-07-01-040 RIVETS (16) or AIPC 23-61-87-01-030 RIVETS (16) and the AIPC 23-61-07-01-130 RIVETS (17) or AIPC 23-61-87-01-030 RIVETS (17).
(4) Use a clean Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) to remove the unwanted sealant from around the applicable static discharger retainer.
I. Installation of the Static Discharger Retainers at Zones 470 (480) (Engine Pylon), 531 (631), 532 (632) and 533 (633) (Flap Track Fairings)
(1) On the engine pylon:
Subtask 23-61-42-420-059-D ** ON A/C NOT FOR ALL (1) On the engine pylon:
- Put the retainer (10) in position and install it with the (6 off) AIPC 54-55-11-02-445 RIVETS (11).
- Use a clean Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) to remove the unwanted sealant from around the applicable static discharger retainer.
- Put the retainer (4) and the plate (9) in position and install it with the (4 off) AIPC 23-61-05-06-060 RIVETS (2) or AIPC 23-61-85-06-060 RIVETS (2) and the (2 off) AIPC 23-61-05-06-050 RIVETS (3) or AIPC 23-61-85-06-050 RIVETS (3).
- Use a clean Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) to remove the unwanted sealant from around the applicable static discharger retainer.
- Put the bonding lead (7) in position and install the bolt (8), the washer (6) and the nut (5).
- Tighten the nut (5).
- Install the top cover (1) on the flap track fairing (Ref. AMM TASK 57-55-11-400-001) or (Ref. AMM TASK 57-55-11-400-004).
- Put the retainer (4) and the plate (9) in position and install it with the (4 off) AIPC 23-61-05-05-060 RIVETS (2) or AIPC 23-61-85-05-060 RIVETS (2) and the (2 off) AIPC 23-61-05-05-050 RIVETS (3) or AIPC 23-61-85-05-050 RIVETS (3).
- Use a clean Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) to remove the unwanted sealant from around the applicable static discharger retainer.
- Put the bonding lead (7) in position and install the bolt (8), the washer (6) and the nut (5).
- Tighten the nut (5).
- Install the top cover (1) on the flap track fairing (Ref. AMM TASK 57-55-11-400-001) or (Ref. AMM TASK 57-55-11-400-004).
- Put the retainer (4) and the plate (9) in position and install it with the (4 off) AIPC 23-61-05-04-060 RIVETS (2) or AIPC 23-61-85-04-060 RIVETS (2) and the (2 off) AIPC 23-61-05-04-050 RIVETS (3) or AIPC 23-61-85-04-050 RIVETS (3).
- Use a clean Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) to remove the unwanted sealant from around the applicable static discharger retainer.
- Put the bonding lead (7) in position and install the bolt (8), the washer (6) and the nut (5).
- Tighten the nut (5).
- Install the top cover (1) on the flap track fairing (Ref. AMM TASK 57-55-11-400-001) or (Ref. AMM TASK 57-55-11-400-004).
I. Installation of the Static Discharger Retainers at Zones 531 (631), 532 (632) and 533 (633) (Flap Track Fairings)
(1) On flap-track fairing 2:
Subtask 23-61-42-420-060-A ** ON A/C NOT FOR ALL (1) On flap-track fairing 2:
- Put the retainer (4) and the plate (9) in position and install it with the (4 off) AIPC 23-61-05-06-060 RIVETS (2) or AIPC 23-61-85-06-060 RIVETS (2) and the (2 off) AIPC 23-61-05-06-050 RIVETS (3) or AIPC 23-61-85-06-050 RIVETS (3).
- Use a clean Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) to remove the unwanted sealant from around the applicable static discharger retainer.
- Put the bonding lead (7) in position and install the bolt (8), the washer (6) and the nut (5).
- Tighten the nut (5).
- Install the top cover (1) on the flap track fairing (Ref. AMM TASK 57-55-11-400-001) or (Ref. AMM TASK 57-55-11-400-004).
- Put the retainer (4) and the plate (9) in position and install it with the (4 off) AIPC 23-61-05-05-060 RIVETS (2) or AIPC 23-61-85-05-060 RIVETS (2) and the (2 off) AIPC 23-61-05-05-050 RIVETS (3) or AIPC 23-61-85-05-050 RIVETS (3).
- Use a clean Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) to remove the unwanted sealant from around the applicable static discharger retainer.
- Put the bonding lead (7) in position and install the bolt (8), the washer (6) and the nut (5).
- Tighten the nut (5).
- Install the top cover (1) on the flap track fairing (Ref. AMM TASK 57-55-11-400-001) or (Ref. AMM TASK 57-55-11-400-004).
- Put the retainer (4) and the plate (9) in position and install it with the (4 off) AIPC 23-61-05-04-060 RIVETS (2) or AIPC 23-61-85-04-060 RIVETS (2) and the (2 off) AIPC 23-61-05-04-050 RIVETS (3) or AIPC 23-61-85-04-050 RIVETS (3).
- Use a clean Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) to remove the unwanted sealant from around the applicable static discharger retainer.
- Put the bonding lead (7) in position and install the bolt (8), the washer (6) and the nut (5).
- Tighten the nut (5).
- Install the top cover (1) on the flap track fairing (Ref. AMM TASK 57-55-11-400-001) or (Ref. AMM TASK 57-55-11-400-004).
J. Installation of the Static Discharger Retainers at Zone 590 (690) (Ailerons)
(1) Put the retainer (10) and a new AIPC 23-61-05-01-065 WASHER (9) in position and install them with the (4 off) AIPC 23-61-05-01-010 RIVETS (7) and the (1 off) AIPC 23-61-05-01-020 RIVET (8).
(2) Put the retainer (14) and the new AIPC 23-61-05-01-065 WASHERS (13) in position and install them with the (4 off) AIPC 23-61-05-01-050 RIVETS (11) and the (2 off) AIPC 23-61-05-01-060 RIVETS (12).
(3) Use a clean Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) to remove the unwanted sealant from around the applicable static discharger retainer.
Subtask 23-61-42-420-060-B ** ON A/C NOT FOR ALL (1) Put the retainer (10) and a new AIPC 23-61-05-01-065 WASHER (9) in position and install them with the (4 off) AIPC 23-61-05-01-010 RIVETS (7) and the (1 off) AIPC 23-61-05-01-020 RIVET (8).
(2) Put the retainer (14) and the new AIPC 23-61-05-01-065 WASHERS (13) in position and install them with the (4 off) AIPC 23-61-05-01-050 RIVETS (11) and the (2 off) AIPC 23-61-05-01-060 RIVETS (12).
(3) Use a clean Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) to remove the unwanted sealant from around the applicable static discharger retainer.
J. Installation of the Static Discharger Retainers at Zone 590 (690) (Ailerons)
(1) Put the retainer (2) in position and install it with the (4 off) AIPC 23-61-05-01-100 RIVETS (3) and the (1 off) AIPC 23-61-05-01-110 RIVET (1).
(2) Use a clean Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) to remove the unwanted sealant from around the applicable static discharger retainer.
Subtask 23-61-42-420-061-D ** ON A/C NOT FOR ALL (1) Put the retainer (2) in position and install it with the (4 off) AIPC 23-61-05-01-100 RIVETS (3) and the (1 off) AIPC 23-61-05-01-110 RIVET (1).
(2) Use a clean Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) to remove the unwanted sealant from around the applicable static discharger retainer.
K. Installation of the Static Discharger Retainers at Zone 534 (634) (Wing-Tip)
(1) Put the retainer (2) in position and install it with the (2 off) AIPC 23-61-05-02-080 RIVETS (1) and the (4 off) AIPC 23-61-05-02-070 RIVETS (3).
(2) Use a clean Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) to remove the unwanted sealant from around the applicable static discharger retainer.
Subtask 23-61-42-420-062-D ** ON A/C NOT FOR ALL (1) Put the retainer (2) in position and install it with the (2 off) AIPC 23-61-05-02-080 RIVETS (1) and the (4 off) AIPC 23-61-05-02-070 RIVETS (3).
(2) Use a clean Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) to remove the unwanted sealant from around the applicable static discharger retainer.
L. Installation of the Static Discharger Retainers at Zone 534 (634) (Wing-Tip Fence)
(1) Put the retainer (3) in position with the packer (4) and install it with the (4 off) AIPC 23-61-05-03-010 RIVETS (1) and the (2 off) AIPC 23-61-05-03-140 RIVETS (2).
(2) Put the retainer (5) in position and install it with the (6 off) AIPC 23-61-05-03-200 RIVETS (6).
(3) Put the retainer (9) in position with the packer (7) and install it with the (5 off) AIPC 23-61-05-03-010 RIVETS (1).
(4) Use a clean Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) to remove the unwanted sealant from around the applicable static discharger retainer.
Subtask 23-61-42-420-062-E ** ON A/C NOT FOR ALL (1) Put the retainer (3) in position with the packer (4) and install it with the (4 off) AIPC 23-61-05-03-010 RIVETS (1) and the (2 off) AIPC 23-61-05-03-140 RIVETS (2).
(2) Put the retainer (5) in position and install it with the (6 off) AIPC 23-61-05-03-200 RIVETS (6).
(3) Put the retainer (9) in position with the packer (7) and install it with the (5 off) AIPC 23-61-05-03-010 RIVETS (1).
(4) Use a clean Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) to remove the unwanted sealant from around the applicable static discharger retainer.
L. Installation of the Static Discharger Retainers at Zone 534 (634) (Wing-Tip Fence)
(1) Put the retainer (2) in position with the packer (3) and install it with the AIPC 23-61-05-03-010 RIVETS (1).
(2) Put the retainer (5) in position and install it with the AIPC 23-61-05-03-200 RIVET (4).
(3) Put the retainer (7) in position and install it with the AIPC 23-61-05-03-200 RIVET (6).
(4) Use a clean Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-- Methyl Alcohol - (Material No.08BBE1) to remove the unwanted sealant from around the applicable static discharger retainer.
Subtask 23-61-42-420-064-A ** ON A/C NOT FOR ALL (1) Put the retainer (2) in position with the packer (3) and install it with the AIPC 23-61-05-03-010 RIVETS (1).
(2) Put the retainer (5) in position and install it with the AIPC 23-61-05-03-200 RIVET (4).
(3) Put the retainer (7) in position and install it with the AIPC 23-61-05-03-200 RIVET (6).
(4) Use a clean Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-- Methyl Alcohol - (Material No.08BBE1) to remove the unwanted sealant from around the applicable static discharger retainer.
M. Installation of the Static Discharger Retainers at Zone 534 (634) (Sharklet)
(1) Put the retainer (2) in position and install it with the (4 off) AIPC 23-61-05-10-010 RIVETS (1) or AIPC 23-61-85-01-010 RIVETS (1).
(2) Put the retainer (7) in position and install it with:
Subtask 23-61-42-760-050-A (1) Put the retainer (2) in position and install it with the (4 off) AIPC 23-61-05-10-010 RIVETS (1) or AIPC 23-61-85-01-010 RIVETS (1).
(2) Put the retainer (7) in position and install it with:
- The (2 off) AIPC 23-61-05-10-020 RIVETS (3) or AIPC 23-61-85-01-020 RIVETS (3)
- The (2 off) AIPC 23-61-05-10-030 RIVETS (4) or AIPC 23-61-85-01-030 RIVETS (4) and AIPC 23-61-85-01-040 RIVETS (4)
- The (1 off) AIPC 23-61-05-10-060 RIVETS (5) or AIPC 23-61-85-01-050 RIVETS (5) and the (1 off) AIPC 23-61-05-10-050 RIVETS (5) or AIPC 23-61-85-01-060 RIVETS (5).
- The (2 off) AIPC 23-61-05-10-020 RIVETS (8) or AIPC 23-61-85-01-020 RIVETS (8) and AIPC 23-61-85-01-040 RIVETS (8)
- The (2 off) AIPC 23-61-05-10-040 RIVETS (9) or AIPC 23-61-85-01-030 RIVETS (9)
- The (2 off) AIPC 23-61-05-10-060 RIVETS (10) or AIPC 23-61-85-01-050 RIVETS (10) and AIPC 23-61-85-01-070 RIVETS (10).
- The (1 off) AIPC 23-61-05-10-030 RIVETS (12) or AIPC 23-61-85-01-040 RIVETS (12)
- The (1 off) AIPC 23-61-05-10-020 RIVETS (13) or AIPC 23-61-85-01-020 RIVETS (13)
- The (1 off) AIPC 23-61-05-10-050 RIVETS (14) or AIPC 23-61-85-01-060 RIVETS (14)
- The (1 off) AIPC 23-61-05-10-040 RIVETS (15) or AIPC 23-61-85-01-030 RIVETS (15)
- The (2 off) AIPC 23-61-05-10-070 RIVETS (16) or AIPC 23-61-85-01-070 RIVETS (16) and AIPC 23-61-85-01-080 RIVETS (16).
- The (2 off) AIPC 23-61-05-10-020 RIVETS (18) or AIPC 23-61-85-01-040 RIVETS (18)
- The (2 off) AIPC 23-61-05-10-040 RIVETS (19) or AIPC 23-61-85-01-060 RIVETS (19)
- The (1 off) AIPC 23-61-05-10-070 RIVETS (20) or AIPC 23-61-85-01-080 RIVETS (20)
- The (1 off) AIPC 23-61-05-10-060 RIVETS (21) or AIPC 23-61-85-01-070 RIVETS (21).
N. Test
(1) Do a check of the bonding between the applicable static discharger retainers and the adjacent metal part of the aircraft structure (Ref. AMM TASK 23-61-00-200-001).
Subtask 23-61-42-420-052-A (1) Do a check of the bonding between the applicable static discharger retainers and the adjacent metal part of the aircraft structure (Ref. AMM TASK 23-61-00-200-001).
O. Installation of the Static Discharger Retainer
(1) If necessary, paint the applicable static discharger retainer the same as the adjacent structure.
(2) Do not paint the interfaces of the applicable static discharger retainer.
5. Close-up(1) If necessary, paint the applicable static discharger retainer the same as the adjacent structure.
(2) Do not paint the interfaces of the applicable static discharger retainer.
Subtask 23-61-42-410-050-A
A. Close Access
(1) Install the applicable static discharger (Ref. AMM TASK 23-61-41-400-001).
(2) Remove the access platform(s).
Subtask 23-61-42-865-052-A (1) Install the applicable static discharger (Ref. AMM TASK 23-61-41-400-001).
(2) Remove the access platform(s).
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 23-61-42-942-050-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/ELAC1/NORM/SPLY | 15CE1 | B11 |
| 49VU | FLIGHT CONTROLS/THS/ACTR/MOT2 | 19CE2 | B09 |
| 49VU | FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 | 6CV | B07 |
| 49VU | AUTO FLT/FAC1/28VDC | 5CC1 | B04 |
| 49VU | AUTO FLT/FAC1/26VAC | 14CC1 | B03 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/ELAC1/NORM/SPLY | 15CE1 | B06 |
| 49VU | FLIGHT CONTROLS/THS/ACTR/MOT2 | 19CE2 | B04 |
| 49VU | FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 | 6CV | B02 |
| 49VU | AUTO FLT/FAC1/28VDC | 5CC1 | H10 |
| 49VU | AUTO FLT/FAC1/26VAC | 14CC1 | H09 |
| ** ON A/C ALL | |||
| 105VU | FLIGHT CONTROLS/ELAC2/STBY SPLY | 16CE2 | A02 |
| 105VU | FLT CTL/ELAC1/STBY SPLY | 16CE1 | A01 |
| 121VU | AUTO FLT/FAC2/28VDC | 5CC2 | M19 |
| 121VU | AUTO FLT/FAC2/26VAC | 14CC2 | M18 |
| 121VU | FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 | 8CV | Q21 |
| 121VU | FLIGHT CONTROLS/THS ACTR/MOT3 | 19CE3 | Q17 |
| 121VU | FLIGHT CONTROLS/THS ACTR/MOT1 | 19CE1 | Q16 |
| 121VU | FLIGHT CONTROLS/ELAC2/NORM/SPLY | 15CE2 | R20 |
C. Removal of Equipment
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Remove the SAFETY BARRIERS.
(3) Remove the WARNING NOTICE(S).
(4) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Remove the SAFETY BARRIERS.
(3) Remove the WARNING NOTICE(S).
(4) Remove the ground support and maintenance equipment, the special and standard tools and all other items.