Bonding of the Pins on the Accoustic Bulkhead (APS 3200)
TASK 49-20-00-340-001-A
Bonding of the Pins on the Accoustic Bulkhead (APS 3200)
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Consumable Materials
C. Work Zones and Access Panels
D. Referenced Information
3. Job Set-up
Subtask 49-20-00-860-060-A ** ON A/C NOT FOR ALL
Subtask 49-20-00-915-050-A ** ON A/C NOT FOR ALL
Subtask 49-20-00-865-090-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.01 12:42:39 UTC
Bonding of the Pins on the Accoustic Bulkhead (APS 3200)
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 | 1 | ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE |
| No specific | AR | SAFETY CLIP - CIRCUIT BREAKER |
| No specific | AR | SOLDERING IRON |
| REFERENCE | DESIGNATION |
|---|---|
| (Material No.05EML8) | Epoxy Adhesive-- - Legacy 2 |
| (Material No.08BAA9) | Non Aqueous Cleaner-General - - |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 315AL, 316AR |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 24-41-00-861-002-A | Energize the Aircraft Electrical Circuits from the External Power |
| TASK 24-41-00-861-002-A-01 | Energize the Aircraft Electrical Circuits from the APU |
| TASK 24-41-00-861-002-A-02 | Energize the Aircraft Electrical Circuits from Engine 1(2) |
| TASK 24-41-00-862-002-A | De-energize the Aircraft Electrical Circuits Supplied from the External Power |
| TASK 24-41-00-862-002-A-01 | De-energize the Aircraft Electrical Circuits Supplied from the APU |
| TASK 24-41-00-862-002-A-02 | De-energize the Aircraft Electrical Circuits Supplied from the Engine 1(2) |
| TASK 29-00-00-864-001-A | Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action |
| TASK 29-14-00-614-001-A | Depressurization of the Hydraulic Reservoirs |
| TASK 52-41-00-010-001-A | Open the APU Doors for Access |
| TASK 52-41-00-410-001-A | Close the APU Doors after Access |
Subtask 49-20-00-860-060-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
(1) Put the warning notice on panel 25VU to tell persons not to start the APU.
(2) Energize the ground service network
(Ref. AMM TASK 24-41-00-861-002).
(3) Make sure that the hydraulic systems are depressurized
(Ref. AMM TASK 29-14-00-614-001).
Subtask 49-20-00-865-079-A ** ON A/C NOT FOR ALL (1) Put the warning notice on panel 25VU to tell persons not to start the APU.
(2) Energize the ground service network
(Ref. AMM TASK 24-41-00-861-002).
(3) Make sure that the hydraulic systems are depressurized
(Ref. AMM TASK 29-14-00-614-001).
B. Open, safety and tag this(these) circuit breaker(s):
Subtask 49-20-00-010-063-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 121VU | APU/APU/CTL | 2KD | L42 |
| 121VU | APU/ECB/SPLY | 1KD | L41 |
C. Get Access
(1) Put the ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE in position below the APU access doors 315AL 316AR.
(2) Open the APU access doors 315AL and 316AR (Ref. AMM TASK 52-41-00-010-001).
(3) Set the light switch 11LJ to on.
4. Procedure(1) Put the ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE in position below the APU access doors 315AL 316AR.
(2) Open the APU access doors 315AL and 316AR (Ref. AMM TASK 52-41-00-010-001).
(3) Set the light switch 11LJ to on.
Subtask 49-20-00-915-050-A ** ON A/C NOT FOR ALL
A. Bonding of the pins on the Accoustic Bulkhead
(1) Removal of the pins.
(a) Warm up the pins (1) and (2) with SOLDERING IRON and remove the pins with a tong.
(2) Prepare the pins for installation.
(a) Clean the pins and the related area of accoustic bulkhead with Non Aqueous Cleaner-General - - (Material No.08BAA9) .
(b) Mix the Epoxy Adhesive-- - Legacy 2 (Material No.05EML8) . Obey the manufacture instruction.
(c) Apply a thin layer of the Epoxy Adhesive-- - Legacy 2 (Material No.05EML8) to the pins.
(d) Install the pins.
(e) Apply pressure to the pins and let it harden. Using a heat lamp. Hardening times as follows:
5. Close-up(1) Removal of the pins.
(a) Warm up the pins (1) and (2) with SOLDERING IRON and remove the pins with a tong.
(2) Prepare the pins for installation.
(a) Clean the pins and the related area of accoustic bulkhead with Non Aqueous Cleaner-General - - (Material No.08BAA9) .
(b) Mix the Epoxy Adhesive-- - Legacy 2 (Material No.05EML8) . Obey the manufacture instruction.
(c) Apply a thin layer of the Epoxy Adhesive-- - Legacy 2 (Material No.05EML8) to the pins.
(d) Install the pins.
(e) Apply pressure to the pins and let it harden. Using a heat lamp. Hardening times as follows:
- 8 hours at 20 DEG.C (68.00 DEG.F)
- 6 hours at 60 DEG.C (140.00 DEG.F)
- 15 minutes at 80 DEG.C (176.00 DEG.F)
- 10 minutes at 100 DEG.C (212.00 DEG.F)
Subtask 49-20-00-865-090-A ** ON A/C NOT FOR ALL
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 49-20-00-410-065-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 121VU | APU/APU/CTL | 2KD | L42 |
| 121VU | APU/ECB/SPLY | 1KD | L41 |
B. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Set the light switch 11LJ to off.
(3) Close the access doors 315AL and 316AR (Ref. AMM TASK 52-41-00-410-001).
(4) Remove the access platform(s).
Subtask 49-20-00-860-061-A ** ON A/C NOT FOR ALL (1) Make sure that the work area is clean and clear of tools and other items.
(2) Set the light switch 11LJ to off.
(3) Close the access doors 315AL and 316AR (Ref. AMM TASK 52-41-00-410-001).
(4) Remove the access platform(s).
C. Aircraft Maintenance Configuration
(1) Put the related hydraulic system in the pressurized configuration (Ref. AMM TASK 29-00-00-864-001).
(2) De-energize the ground service network
(Ref. AMM TASK 24-41-00-862-002).
(3) Remove the WARNING NOTICE(S).
(1) Put the related hydraulic system in the pressurized configuration (Ref. AMM TASK 29-00-00-864-001).
(2) De-energize the ground service network
(Ref. AMM TASK 24-41-00-862-002).
(3) Remove the WARNING NOTICE(S).
Bonding of the Pins