Parameter Loading with the USB Flash Drive
TASK 46-41-00-610-808-A
Parameter Loading with the USB Flash Drive
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 46-41-00-280-055-A ** ON A/C NOT FOR ALL
Subtask 46-41-00-860-072-AX ** ON A/C NOT FOR ALL
Subtask 46-41-00-862-090-D ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.02 06:26:13 UTC
Parameter Loading with the USB Flash Drive
ZONE: 200
1. Reason for the JobSelf explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | 1 | LAPTOP - FOR GSM ALNA MAINTENANCE |
| No specific | 1 | USB FLASH DRIVE, MIN. 2GB CAPACITY |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 200 | UPPER HALF FUSELAGE |
| 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 46-41-00-720-817-A | Avionic Data Availability Check |
| TASK 46-41-00-860-801-A | Connection of the Maintenance Laptop to the Cabin Plug |
| TSM 46-41-00-810-813 | Status Monitoring Avionic Data not available |
Subtask 46-41-00-280-055-A ** ON A/C NOT FOR ALL
A. System configuration
The installation sequence is given below. Obey to the installation sequence each time you do the parameter loading procedure.
These parameters are applicable:
The procedure that follows has these steps:
Subtask 46-41-00-861-090-D ** ON A/C NOT FOR ALL The installation sequence is given below. Obey to the installation sequence each time you do the parameter loading procedure.
These parameters are applicable:
- FIN 3001RFSW8 SOFTWARE-ALNA, PARAMETER
The procedure that follows has these steps:
- Uploading procedure of the parameter to the equipment
- Do a check of the equipment/parameter configuration after the upload procedure.
B. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) Connect the maintenance laptop (Ref. AMM TASK 46-41-00-860-801).
Subtask 46-41-00-865-097-A ** ON A/C NOT FOR ALL (1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) Connect the maintenance laptop (Ref. AMM TASK 46-41-00-860-801).
C. Make sure that this(these) circuit breaker(s) is(are) closed:
4. Procedure| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 2000VU | WAP | 27MH | D07 |
| 2000VU | CINS-HESU | 21RF | E02 |
| 2000VU | CINS-HESU | 21RF | E02 |
Subtask 46-41-00-860-072-AX ** ON A/C NOT FOR ALL
A. Aircraft configuration
(2) If the Avionics Data shows as "Not Available" do the related troubleshooting procedure TSM 46-41-00-810-813.
Subtask 46-41-00-610-058-A ** ON A/C NOT FOR ALL NOTE: The aircraft must be on the ground for the software loading.
(1) Make sure that the Avionics Data shows as "Available" (Ref. AMM TASK 46-41-00-720-817).(2) If the Avionics Data shows as "Not Available" do the related troubleshooting procedure TSM 46-41-00-810-813.
B. Parameter Loading with the USB Flash Drive
5. Close-upNOTE: This procedure will be done at the LAPTOP - FOR GSM ALNA MAINTENANCE.
NOTE: You must copy the dedicated load onto the USB Stick in the folder "PACKAGES". e.g. U:/packages/3001RFSW8.
| ACTION | RESULT |
|---|---|
| In the cabin, at the Maintenance Laptop: | On the Maintenance Laptop: |
| 1.Put the USB FLASH DRIVE, MIN. 2GB CAPACITY with the loads into the USB-port of the Maintenance Laptop. | |
| 2.Click on the "DATA LOADING" icon. |
|
| 3.Click on the "ARROW-DOWN" icon adjacent to the icon "CONFIGURATION TO INSTALL". |
|
| 4.Click on the "INSERTED MEDIA" icon. |
|
| 5.Click on the "SW INSTALL" icon. |
|
| 6.Click on the "OK" icon to start the installation. |
|
| |
|
| 7.Click on the "OK" icon. | |
| 8.Click on the "SYSTEM MON." icon. |
|
| 9.Click on the "RESET" icon in the line HESU and then click on the "OK" to start the reset. |
|
| 10.Wait for approximately 10 minutes. |
|
| 11.Click on the "LOGIN" icon. |
|
| 12.Enter the correct password and press the "OK" icon. |
|
| 13.Click on the "SYSTEM IDENT." icon. |
|
| 14.Make sure that all part numbers are correct. | |
| 15.Remove the USB Flash Drive from the USB-port of the maintenance laptop. | |
Subtask 46-41-00-862-090-D ** ON A/C NOT FOR ALL
A. Put the aircraft back to its initial configuration.
(1) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
(2) Click on the "LOGOFF" icon.
(4) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
(1) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
(2) Click on the "LOGOFF" icon.
NOTE: It is not necessary to log off, if you continue with a different test procedure.
(3) Disconnect and shut down the maintenance laptop. (4) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).