Installation of the 1M and 2M Harnesses on the MLG Axle
TASK 32-11-43-400-003-A
Installation of the 1M and 2M Harnesses on the MLG Axle
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 32-11-43-941-056-A
(2) If necessary, attach a STRING - DRAW to each applicable cableform at the cable access holes.
(3) Pull the draw strings through the axle, one at a time, to put the cableforms in position. Remove the draw strings.
(5) For the 1M harness:
(a) Connect the electrical plug (3) to the 1M harness electrical connector (2).
(6) For the 2M harness:
(a) Make sure that the 2M harness is not caught between the cable clamp (6) and the axle.
(b) Put the cable clamp (6) in position and install with the washers (5) and the bolts (4).
14QFB1 Wire-Locking Dia: 0.8 mm CRES Nickel Alloy - .
(d) Connect the electrical connector (7) to the 2M harness electrical connector (8).
(7) Do the steps that follow:
(b) Make a mark on the backshells of all the electrical connectors that you removed with red Top Coat Polyurethane-- Decorative External Structure (Material No.04JMD3) .
(c) Apply a layer of Polysulfide Sealant-General Purpose Fillet - (Material No.06AAB1) to all the bolts, screws and washers you installed.
Subtask 32-11-43-410-065-A ** ON A/C NOT FOR ALL
Subtask 32-11-43-942-057-A
[Rev.10 from 2021]
2026.04.01 00:40:59 UTC
Installation of the 1M and 2M Harnesses on the MLG Axle
WARNING:
MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING NOTICES ARE IN POSITION.
WARNING:
MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING GEAR. THIS WILL PREVENT UNWANTED MOVEMENT OF THE LANDING GEAR, AND THUS POSSIBLE INJURY TO PERSONS AND DAMAGE TO THE AIRCRAFT AND/OR EQUIPMENT.
WARNING:
BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
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 2M (6 FT) |
| No specific | AR | SAFETY BARRIER(S) |
| No specific | AR | STRING - DRAW |
| No specific | 1 | WARNING NOTICE(S) |
| REFERENCE | DESIGNATION |
|---|---|
| (Material No.04JMD3) | Top Coat Polyurethane-- Decorative External Structure |
| (Material No.05BAB1) | Threadlocking Adhesive-- Low strength Low viscosity - |
| (Material No.06AAB1) | Polysulfide Sealant-General Purpose Fillet - |
| (Material No.08BAA9) | Non Aqueous Cleaner-General - - |
| (Material No.14QFB1) | Wire-Locking Dia: 0.8 mm CRES Nickel Alloy - |
| (Material No.14SBA1) | Textile-Lint free Cotton - |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 730 | LEFT MAIN LANDING GEAR & DOORS |
| 740 | RIGHT MAIN LANDING GEAR & DOORS |
| REFERENCE | DESIGNATION |
|---|---|
| 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 32-00-00-481-001-A | Installation of the Safety Devices on the Landing Gears |
| TASK 32-12-00-010-001-A | Open the Main Gear Doors for Access |
| TASK 32-12-00-410-001-A | Close the Main Gear Doors after Access |
| TASK 32-41-11-000-006-A | Removal of the MLG Wheel |
| TASK 32-41-11-400-006-A | Installation of the MLG Wheel |
| TASK 32-42-00-720-002-A | Functional Test of the Tachometers and the Anti-Skid System with the Normal Braking System ON |
| TASK 32-42-57-000-001-A | Removal of the Tachometer |
| TASK 32-42-57-400-001-A | Installation of the Tachometer |
| TASK 32-48-51-000-005-A | Removal of the Fan Assy |
| TASK 32-48-51-400-005-A | Installation of the Fan Assy |
| TASK 32-69-00-740-001-A | BITE Check of Landing-Gear Control Interface-Unit (LGCIU) With Use of MCDU to Ensure that Continuous BITE is Operative |
| ESPM 203300 | |
Subtask 32-11-43-941-056-A
A. Safety Precautions
(1) Make sure that the SAFETY BARRIER(S) are in position.
(2) Make sure that the ground safety locks are on the landing gear (Ref. AMM TASK 32-00-00-481-001).
(3) On panel 400VU:
Subtask 32-11-43-869-060-A (1) Make sure that the SAFETY BARRIER(S) are in position.
(2) Make sure that the ground safety locks are on the landing gear (Ref. AMM TASK 32-00-00-481-001).
(3) On panel 400VU:
- Make sure that the landing-gear control-lever 6GA is in the DOWN position
- Make sure that the WARNING NOTICE(S) is in position to tell persons not to operate the landing gear.
B. Flight Configuration Precautions
(1) If you did not open the LGCIU circuit breakers, make sure that the electrical circuits are de-energized (Ref. AMM TASK 24-41-00-862-002).
Subtask 32-11-43-865-061-A (1) If you did not open the LGCIU circuit breakers, make sure that the electrical circuits are de-energized (Ref. AMM TASK 24-41-00-862-002).
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
Subtask 32-11-43-860-053-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C ALL | |||
| 49VU | L/G/LGCIU/SYS1/NORM | 1GA | C09 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | LGCIU/BAT SPLY/SYS2 | 59GA | R33 |
| 121VU | LGCIU/BAT SPLY/SYS1 | 58GA | R32 |
| ** ON A/C ALL | |||
| 121VU | HYDRAULIC/LGCIU/SYS2 | 2GA | Q35 |
| 121VU | HYDRAULIC/LGCIU/SYS1/GRND SPLY | 52GA | Q34 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | LGCIU/BAT SPLY/SYS2 | 59GA | R32 |
| 121VU | LGCIU/BAT SPLY/SYS1 | 58GA | R31 |
D. Aircraft Maintenance Configuration
(1) Make sure that the applicable MLG door is open (Ref. AMM TASK 32-12-00-010-001).
(2) Make sure that the ACCESS PLATFORM 2M (6 FT) is adjacent to the applicable MLG.
(3) Make sure that the applicable MLG wheels are removed (Ref. AMM TASK 32-41-11-000-006).
(4) Make sure that the applicable tachometers are removed (Ref. AMM TASK 32-42-57-000-001).
Subtask 32-11-43-860-053-B ** ON A/C NOT FOR ALL (1) Make sure that the applicable MLG door is open (Ref. AMM TASK 32-12-00-010-001).
(2) Make sure that the ACCESS PLATFORM 2M (6 FT) is adjacent to the applicable MLG.
(3) Make sure that the applicable MLG wheels are removed (Ref. AMM TASK 32-41-11-000-006).
(4) Make sure that the applicable tachometers are removed (Ref. AMM TASK 32-42-57-000-001).
D. Aircraft Maintenance Configuration
(1) Make sure that the applicable MLG door is open (Ref. AMM TASK 32-12-00-010-001).
(2) Make sure that the ACCESS PLATFORM 2M (6 FT) is adjacent to the applicable MLG.
(3) Make sure that the applicable MLG wheels are removed (Ref. AMM TASK 32-41-11-000-006).
(4) Make sure that the applicable brake fan assemblies are removed (Ref. AMM TASK 32-48-51-000-005).
(5) Make sure that the applicable tachometers are removed (Ref. AMM TASK 32-42-57-000-001).
4. Procedure(1) Make sure that the applicable MLG door is open (Ref. AMM TASK 32-12-00-010-001).
(2) Make sure that the ACCESS PLATFORM 2M (6 FT) is adjacent to the applicable MLG.
(3) Make sure that the applicable MLG wheels are removed (Ref. AMM TASK 32-41-11-000-006).
(4) Make sure that the applicable brake fan assemblies are removed (Ref. AMM TASK 32-48-51-000-005).
(5) Make sure that the applicable tachometers are removed (Ref. AMM TASK 32-42-57-000-001).
WARNING:
MAKE SURE THAT THE INSTALLATION AND ROUTING OF ALL ELECTRICAL CABLES AGREE WITH THE REQUIREMENTS OF THE ELECTRICAL STANDARD PRACTICES MANUAL.
Subtask 32-11-43-420-076-A A. Preparation for Installation
(2) Do an inspection of the component interfaces and the adjacent area.
(3) Make sure that the parts retained from the removed component are clean and in the correct condition.
(4) Make sure that all the electrical connections are clean and in the correct condition.
(5) Make sure that the 1M and 2M harnesses are in correct condition ESPM 203300.
Subtask 32-11-43-420-077-C WARNING:
BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
(1) Clean the component interfaces and the adjacent areas with a Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) . (2) Do an inspection of the component interfaces and the adjacent area.
(3) Make sure that the parts retained from the removed component are clean and in the correct condition.
(4) Make sure that all the electrical connections are clean and in the correct condition.
(5) Make sure that the 1M and 2M harnesses are in correct condition ESPM 203300.
WARNING:
USE PROTECTIVE GOGGLES AND GLOVES WHEN YOU REMOVE OR INSTALL LOCKWIRE. EACH TIME YOU CUT LOCKWIRE, REMOVE AND DISCARD IT IMMEDIATELY. LOOSE LOCKWIRE CAN CUT YOU OR MAKE YOU BLIND, AND/OR CAN CAUSE DAMAGE.
CAUTION:
MAKE SURE THAT ALL ELECTRICAL CONNECTORS ARE IDENTIFIED WITH THEIR FIN NO. TO CORRECTLY CONNECT EACH PLUG TO ITS RELATED RECEPTACLE. INCORRECT CONNECTION OF THE ELECTRICAL CONNECTORS CAN CAUSE DAMAGE TO THE AIRCRAFT ELECTRICAL SYSTEM.
B. Installation of the 1M and 2M Harnesses on the MLG Axle NOTE: Make sure that there are no kinks in the 1M and 2M harnesses.
(1) Identify the positions of the three cableforms at the end of each harness. (2) If necessary, attach a STRING - DRAW to each applicable cableform at the cable access holes.
(3) Pull the draw strings through the axle, one at a time, to put the cableforms in position. Remove the draw strings.
NOTE: Make sure that there are no kinks in the cableforms when they are put in position.
(4) Remove the CAP-BLANKING from each electrical connector and receptacle.(5) For the 1M harness:
(a) Connect the electrical plug (3) to the 1M harness electrical connector (2).
(6) For the 2M harness:
(a) Make sure that the 2M harness is not caught between the cable clamp (6) and the axle.
(b) Put the cable clamp (6) in position and install with the washers (5) and the bolts (4).
WARNING:
USE PROTECTIVE GOGGLES AND GLOVES WHEN YOU REMOVE OR INSTALL LOCKWIRE. EACH TIME YOU CUT LOCKWIRE, REMOVE AND DISCARD IT IMMEDIATELY. LOOSE LOCKWIRE CAN CUT YOU OR MAKE YOU BLIND, AND/OR CAN CAUSE DAMAGE.
(c) Safety the bolts (4) together with (d) Connect the electrical connector (7) to the 2M harness electrical connector (8).
(7) Do the steps that follow:
WARNING:
BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
(a) Apply Threadlocking Adhesive-- Low strength Low viscosity - (Material No.05BAB1) to the backshells of all the electrical connectors that you removed. (b) Make a mark on the backshells of all the electrical connectors that you removed with red Top Coat Polyurethane-- Decorative External Structure (Material No.04JMD3) .
(c) Apply a layer of Polysulfide Sealant-General Purpose Fillet - (Material No.06AAB1) to all the bolts, screws and washers you installed.
C. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Install the applicable tachometers (Ref. AMM TASK 32-42-57-400-001).
(3) Install the applicable MLG wheels (Ref. AMM TASK 32-41-11-400-006).
(4) Remove the access platform(s).
(5) Close the applicable MLG door (Ref. AMM TASK 32-12-00-410-001).
Subtask 32-11-43-410-065-B ** ON A/C NOT FOR ALL (1) Make sure that the work area is clean and clear of tools and other items.
(2) Install the applicable tachometers (Ref. AMM TASK 32-42-57-400-001).
(3) Install the applicable MLG wheels (Ref. AMM TASK 32-41-11-400-006).
(4) Remove the access platform(s).
(5) Close the applicable MLG door (Ref. AMM TASK 32-12-00-410-001).
C. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Install the applicable tachometers (Ref. AMM TASK 32-42-57-400-001).
(3) Install the applicable brake fan assemblies (Ref. AMM TASK 32-48-51-400-005).
(4) Install the applicable MLG wheels (Ref. AMM TASK 32-41-11-400-006).
(5) Remove the access platform(s).
(6) Close the applicable MLG door (Ref. AMM TASK 32-12-00-410-001).
Subtask 32-11-43-865-062-A (1) Make sure that the work area is clean and clear of tools and other items.
(2) Install the applicable tachometers (Ref. AMM TASK 32-42-57-400-001).
(3) Install the applicable brake fan assemblies (Ref. AMM TASK 32-48-51-400-005).
(4) Install the applicable MLG wheels (Ref. AMM TASK 32-41-11-400-006).
(5) Remove the access platform(s).
(6) Close the applicable MLG door (Ref. AMM TASK 32-12-00-410-001).
D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 32-11-43-740-053-A Subtask 32-11-43-720-054-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C ALL | |||
| 49VU | L/G/LGCIU/SYS1/NORM | 1GA | C09 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | LGCIU/BAT SPLY/SYS2 | 59GA | R33 |
| 121VU | LGCIU/BAT SPLY/SYS1 | 58GA | R32 |
| ** ON A/C ALL | |||
| 121VU | HYDRAULIC/LGCIU/SYS2 | 2GA | Q35 |
| 121VU | HYDRAULIC/LGCIU/SYS1/GRND SPLY | 52GA | Q34 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | LGCIU/BAT SPLY/SYS2 | 59GA | R32 |
| 121VU | LGCIU/BAT SPLY/SYS1 | 58GA | R31 |
F. Functional Test
5. Close-upCAUTION:
DURING THE FUNCTIONAL TEST OF THE TACHOMETERS, MAKE SURE THAT THE OPERATION OF THE BRAKE PISTONS IS CORRECT AND AGREES WITH EACH STEP GIVEN IN THIS TEST: INCORRECT OPERATION OF THE BRAKE PISTONS CAN BE CAUSED BY A BAD OR A CROSSED CONNECTION OF THE TACHOMETERS DURING INSTALLATION, AND CAN CAUSE UNSATISFACTORY BRAKING AND/OR A TIRE BURST DURING AIRCRAFT OPERATION.
(1) Do a functional test of the tachometers (Ref. AMM TASK 32-42-00-720-002). Subtask 32-11-43-942-057-A
A. Removal of Equipment
(1) Remove the WARNING NOTICE(S).
(2) Remove the SAFETY BARRIER(S).
(3) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
(1) Remove the WARNING NOTICE(S).
(2) Remove the SAFETY BARRIER(S).
(3) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
MLG Axle Harnesses 1M and 2M - Cableform Identification