Installation of the Landing Gear Normal Control Lever
TASK 32-31-11-400-001-A
Installation of the Landing Gear Normal Control Lever
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Work Zones and Access Panels
C. Referenced Information
3. Job Set-up
Subtask 32-31-11-860-051-A
Subtask 32-31-11-420-050-A
Subtask 32-31-11-410-050-A
[Rev.10 from 2021]
2026.04.01 00:44:18 UTC
Installation of the Landing Gear Normal Control Lever
WARNING:
MAKE SURE THAT THE GROUND SAFETY LOCKS ARE CORRECTLY INSTALLED ON THE MLG AND NLG. MOVEMENTS OF THE LANDING GEARS CAN CAUSE INJURY TO PERSONS AND CAUSE DAMAGE TO THE AIRCRAFT AND/OR EQUIPMENT.
1. Reason for the JobSelf explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | SAFETY CLIP - CIRCUIT BREAKER |
| No specific | AR | TIE WRAP(S) |
| 98F32304000000 | 6 | TARGET-FALSE |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 211 | COCKPIT |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 29-10-00-864-001-A | Depressurize the Green Hydraulic System |
| TASK 32-00-00-081-002-A | Removal of the Safety Devices from the Landing Gear Doors |
| TASK 32-00-00-481-001-A | Installation of the Safety Devices on the Landing Gears |
| TASK 32-00-00-481-002-A | Installation of the Safety Devices on the Landing Gear Doors |
| TASK 32-00-00-860-001-A | Flight Configuration Precautions with Electrical Power |
| TASK 32-00-00-860-001-A-01 | Flight Configuration Precautions without Electrical Power |
| TASK 32-00-00-860-002-A | Ground Configuration after Flight Configuration with Electrical Power |
| TASK 32-00-00-860-002-A-01 | Ground Configuration after Flight Configuration without Electrical Power |
| 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 32-22-00-010-001-A | Nose Gear Doors - Ground Doors Opening |
| TASK 32-22-00-410-001-A | Nose Gear Doors - Ground Doors Closing |
| TASK 32-31-00-720-002-A | Functional Test of the Normal Extension and Retraction of the Landing Gear |
| 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 |
Subtask 32-31-11-860-051-A
A. Aircraft Maintenance Configuration
(1) Make sure that you obeyed the flight configuration precautions (Ref. AMM TASK 32-00-00-860-001).
(2) Make sure that the safety devices are installed on the MLG and NLG (Ref. AMM TASK 32-00-00-481-001).
Subtask 32-31-11-865-051-A (1) Make sure that you obeyed the flight configuration precautions (Ref. AMM TASK 32-00-00-860-001).
(2) Make sure that the safety devices are installed on the MLG and NLG (Ref. AMM TASK 32-00-00-481-001).
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
4. Procedure| 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 |
Subtask 32-31-11-420-050-A
A. Installation of the L/G Control Lever
(1) Remove the CAP-BLANKING from each electrical connector and receptacle.
(2) Make sure that all the electrical connections are clean and in the correct condition.
(3) Make sure that the L/G control lever (4) is in th DOWN position.
(4) Connect the electrical connectors (1) and (2) to the L/G control lever (4).
(5) Install the L/G control lever (4) in its housing.
(6) Tighten the screws (3).
Subtask 32-31-11-865-052-A (1) Remove the CAP-BLANKING from each electrical connector and receptacle.
(2) Make sure that all the electrical connections are clean and in the correct condition.
(3) Make sure that the L/G control lever (4) is in th DOWN position.
(4) Connect the electrical connectors (1) and (2) to the L/G control lever (4).
(5) Install the L/G control lever (4) in its housing.
(6) Tighten the screws (3).
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 32-31-11-941-050-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 |
C. Safety Precautions
(1) Open the MLG doors and the NLG doors (Ref. AMM TASK 32-12-00-010-001) (Ref. AMM TASK 32-22-00-010-001)
(2) Make sure that the safety devices are installed on the MLG doors and the NLG doors (Ref. AMM TASK 32-00-00-481-002).
(3) Make sure that the Green hydraulic system is depressurized (Ref. AMM TASK 29-10-00-864-001).
Subtask 32-31-11-720-050-B (1) Open the MLG doors and the NLG doors (Ref. AMM TASK 32-12-00-010-001) (Ref. AMM TASK 32-22-00-010-001)
(2) Make sure that the safety devices are installed on the MLG doors and the NLG doors (Ref. AMM TASK 32-00-00-481-002).
(3) Make sure that the Green hydraulic system is depressurized (Ref. AMM TASK 29-10-00-864-001).
D. Test of the Landing Gear Control-Lever
(1) Do the BITE test of the landing-gear control interface-unit (Ref. AMM TASK 32-69-00-740-001).
(a) Open, safety and tag this(these) circuit breaker(s):
(c) Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
(e) Set the landing gear control-lever to DOWN.
(f) Do the steps (d) and (e) again.
(g) Open, safety and tag this(these) circuit breaker(s):
(i) Remove the 98F32304000000 TARGET-FALSE from weight-on-wheels proximity sensors 20GA, 21GA, 22GA, 23GA, 24GA, and 25GA.
(j) Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
5. Close-up(1) Do the BITE test of the landing-gear control interface-unit (Ref. AMM TASK 32-69-00-740-001).
NOTE: As an alternative procedure, you can do this test without the centralized fault display-system (Ref. AMM TASK 32-31-00-720-002).
(2) Do a check of the mechanical integrity of the landing gear control-lever as follows:(a) Open, safety and tag this(these) circuit breaker(s):
- 1GA
- 2GA
- 52GA
- 58GA
- 59GA.
(c) Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
- 1GA
- 2GA
- 52GA
- 58GA
- 59GA.
(e) Set the landing gear control-lever to DOWN.
(f) Do the steps (d) and (e) again.
(g) Open, safety and tag this(these) circuit breaker(s):
- 1GA
- 2GA
- 52GA
- 58GA
- 59GA.
(i) Remove the 98F32304000000 TARGET-FALSE from weight-on-wheels proximity sensors 20GA, 21GA, 22GA, 23GA, 24GA, and 25GA.
(j) Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
- 1GA
- 2GA
- 52GA
- 58GA
- 59GA.
Subtask 32-31-11-410-050-A
A. Close access.
(1) Make sure that the work area is clean and clear of tool(s) and other items
(2) Remove the safety devices from the landing gear doors (Ref. AMM TASK 32-00-00-081-002).
(3) Close the MLG doors and the NLG doors (Ref. AMM TASK 32-12-00-410-001) (Ref. AMM TASK 32-22-00-410-001).
(4) Put the aircraft back to the correct (ground) condition. (Ref. AMM TASK 32-00-00-860-002)
(5) Install the thermoformed cover on the center instrument panel pedestal.
(1) Make sure that the work area is clean and clear of tool(s) and other items
(2) Remove the safety devices from the landing gear doors (Ref. AMM TASK 32-00-00-081-002).
(3) Close the MLG doors and the NLG doors (Ref. AMM TASK 32-12-00-410-001) (Ref. AMM TASK 32-22-00-410-001).
(4) Put the aircraft back to the correct (ground) condition. (Ref. AMM TASK 32-00-00-860-002)
(5) Install the thermoformed cover on the center instrument panel pedestal.
Landing Gear Normal Control Lever