Apply Temporary Protection to End Fittings of Electrical Conduits in Fuselage Tail Area
TASK 24-92-00-210-010-A
Apply Temporary Protection to End Fittings of Electrical Conduits in Fuselage Tail Area
Refer to the MPD TASK: 240000-12
APPLY TEMPORARY PROTECTION TO END FITTINGS OF ELECTRICAL CONDUITS IN FUSELAGE TAIL AREA
Apply temporary protection to end fittings of electrical conduits in the fuselage tail area.
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 24-92-00-862-059-A Subtask 24-92-00-869-069-A Subtask 24-92-00-010-059-A
Subtask 24-92-00-210-059-A
Subtask 24-92-00-410-060-A
[Rev.10 from 2021]
2026.03.31 23:25:46 UTC
Apply Temporary Protection to End Fittings of Electrical Conduits in Fuselage Tail Area
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:
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.
WARNING:
MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND THE CAUTIONS INCLUDED IN THE REFERENCED PROCEDURES.
WARNING:
BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
1. Reason for the JobRefer to the MPD TASK: 240000-12
APPLY TEMPORARY PROTECTION TO END FITTINGS OF ELECTRICAL CONDUITS IN FUSELAGE TAIL AREA
Apply temporary protection to end fittings of electrical conduits in the fuselage tail area.
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | 1 | ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE |
| No specific | AR | BRUSH - BRISTLED |
| No specific | AR | SPRAY - BOTTLE, PUMP TYPE (NON AEROSOL) |
| REFERENCE | DESIGNATION |
|---|---|
| (Material No.08BAA9) | Non Aqueous Cleaner-General - - |
| (Material No.08BLA9) | Non Aqueous Cleaner-Wing - Legacy |
| (Material No.08BPA1) | Non Aqueous Cleaner-Non structural use - - |
| (Material No.12ACB1) | Corrosion Preventive Compound-Heavy Duty Hard Film - |
| (Material No.14SBA1) | Textile-Lint free Cotton - |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 311 | AFT FUSLG TAIL SECTION |
| 312 | AFT FUSLG TAIL SECTION |
| 312AR, 314AR, 315AL, 316AR |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 12-34-24-869-002-A | Aircraft Grounding (Earthing) for the Maintenance Operations |
| TASK 12-34-24-869-002-A-01 | Aircraft Grounding (Earthing) during Transit, Turnaround or Overnight Stop |
| 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 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 |
| ESPM 203330 | |
Subtask 24-92-00-862-059-A Subtask 24-92-00-869-069-A Subtask 24-92-00-010-059-A
C. Get Access
(1) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the fuselage tail area.
(2) Open the access doors 312AR and 314AR.
(3) Open the access doors 315AL and 316AR (Ref. AMM TASK 52-41-00-010-001).
4. Procedure(1) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the fuselage tail area.
(2) Open the access doors 312AR and 314AR.
(3) Open the access doors 315AL and 316AR (Ref. AMM TASK 52-41-00-010-001).
Subtask 24-92-00-210-059-A
A. Inspection of the End Fittings of Electrical Conduits
(a) Use Non Aqueous Cleaner-Non structural use - - (Material No.08BPA1) or Non Aqueous Cleaner-General - - (Material No.08BAA9) or Non Aqueous Cleaner-Wing - Legacy (Material No.08BLA9) and a Textile-Lint free Cotton - (Material No.14SBA1) to remove any contamination from the fitting.
(b) Remove any flakes or blisters, make sure that the you do not damage the base metal while you do this task.
5. Close-upWARNING:
BE CAREFUL NOT TO CUT YOUR FINGERS. FLAKES OF NICKEL ARE SHARP.
(1) At each fitting use the procedure that follows to protect against corrosion: (a) Use Non Aqueous Cleaner-Non structural use - - (Material No.08BPA1) or Non Aqueous Cleaner-General - - (Material No.08BAA9) or Non Aqueous Cleaner-Wing - Legacy (Material No.08BLA9) and a Textile-Lint free Cotton - (Material No.14SBA1) to remove any contamination from the fitting.
(b) Remove any flakes or blisters, make sure that the you do not damage the base metal while you do this task.
NOTE: We recommend that you use a dental tool or a seal tool (non metallic) to remove the flakes and the blisters.
(c) Use a BRUSH - BRISTLED or an SPRAY - BOTTLE, PUMP TYPE (NON AEROSOL) to apply a continuous thin and smooth coat of Corrosion Preventive Compound-Heavy Duty Hard Film - (Material No.12ACB1) , to cover all the fitting ESPM 203330. Subtask 24-92-00-410-060-A
A. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Close the access doors 312AR and 314AR.
(3) Close the access doors 315AL and 316AR (Ref. AMM TASK 52-41-00-410-001).
(4) Disconnect the aircraft from the ground (Ref. AMM TASK 12-34-24-869-002).
(5) Remove the access platform(s).
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Close the access doors 312AR and 314AR.
(3) Close the access doors 315AL and 316AR (Ref. AMM TASK 52-41-00-410-001).
(4) Disconnect the aircraft from the ground (Ref. AMM TASK 12-34-24-869-002).
(5) Remove the access platform(s).
Electrical Harness Conduits - Corrosion Protection