Operational Check of Logics Activating ELAC 1&2, & SEC 1 STBY PWR SPLY & Ability of SEC 1&2 to Achieve Pitch CTL & Ability of Sidestick Priority Function
TASK 27-96-00-710-018-A
Operational Check of Logics Activating ELAC 1&2, & SEC 1 STBY PWR SPLY & Ability of SEC 1&2 to Achieve Pitch CTL & Ability of Sidestick Priority Function
Refer to the MPD TASK: 279000-05
OPERATIONAL CHECK :
You must do the four parts of the procedure (Chapter 4.A., then 4.B., then 4.C., then 4.D.) to complete this operational test.
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 27-96-00-860-050-A ** ON A/C NOT FOR ALL
Subtask 27-96-00-710-082-D
Subtask 27-96-00-865-077-A
[Rev.10 from 2021]
2026.04.01 00:00:01 UTC
Operational Check of Logics Activating ELAC 1&2, & SEC 1 STBY PWR SPLY & Ability of SEC 1&2 to Achieve Pitch CTL & Ability of Sidestick Priority Function
WARNING:
MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS SURFACES ARE CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT.
ZONE: 210
1. Reason for the JobRefer to the MPD TASK: 279000-05
OPERATIONAL CHECK :
You must do the four parts of the procedure (Chapter 4.A., then 4.B., then 4.C., then 4.D.) to complete this operational test.
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | 1 | ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE |
| No specific | AR | SAFETY CLIP - CIRCUIT BREAKER |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 210 | CKPT,FWD COMPT BHD TO FLT COMPT BULKHEAD |
| 822 |
| 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 29-10-00-863-003-A | Pressurize the Blue Hydraulic System with a Hydraulic Ground Power-Cart |
| TASK 29-10-00-863-003-A-01 | Pressurize the Blue Hydraulic System with the Blue Electric Pump |
| TASK 29-10-00-864-003-A | Depressurize the Blue Hydraulic System |
| TASK 29-23-00-863-001-A | Pressurize the Green Hydraulic System from the Yellow Hydraulic System through the PTU with the Electric Pump |
| TASK 29-23-00-864-001-A | Depressurize the Green and Yellow Hydraulic Systems after Operation of the PTU |
| TASK 29-24-00-863-001-A | Pressurize the Yellow Hydraulic System with the Electric Pump |
| TASK 29-24-00-864-001-A | Depressurize the Yellow Hydraulic System |
| TASK 31-60-00-860-001-A | EIS Start Procedure |
| TASK 31-60-00-860-002-A | EIS Stop Procedure |
| TASK 52-41-00-010-002-A | Open the Avionics Compartment Doors for Access |
| TASK 52-41-00-410-002-A | Close the Avionics Compartment Doors after Access |
| TSM 27-96-00-810-801 | (for corrective action) |
| TSM 27-96-00-810-802 | (for corrective action) |
Subtask 27-96-00-860-050-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) On the overhead panel 23VU:
(7) On the center pedestal, on the ECAM control panel push:
(Ref. AMM TASK 29-23-00-864-001) (Ref. AMM TASK 29-24-00-864-001).
(9) Pressurize the Blue hydraulic system
(Ref. AMM TASK 29-10-00-863-003).
Subtask 27-96-00-860-050-B ** ON A/C NOT FOR ALL (1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) On the overhead panel 23VU:
- Make sure that the ELAC 1 and SEC 1 pushbutton switches are pushed (the OFF and FAULT legends are off).
- Make sure that the ELAC 2, SEC 2 and SEC 3 pushbutton switches are pushed (the OFF and FAULT legends are off).
- Set the 3 OFF/NAV/ATT selector switches to NAV.
- Make sure that the PTU pushbutton switch is set to AUTO.
(7) On the center pedestal, on the ECAM control panel push:
- The CLEAR key until all the warnings (if any) stop
- The F/CTL key (on the lower ECAM display unit, the F/CTL page comes into view).
(Ref. AMM TASK 29-23-00-864-001) (Ref. AMM TASK 29-24-00-864-001).
(9) Pressurize the Blue hydraulic system
(Ref. AMM TASK 29-10-00-863-003).
A. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) On the overhead panel 23VU:
(7) On the center pedestal, on the ECAM control panel push:
(Ref. AMM TASK 29-23-00-864-001) (Ref. AMM TASK 29-24-00-864-001).
(9) Pressurize the Blue hydraulic system
(Ref. AMM TASK 29-10-00-863-003).
Subtask 27-96-00-010-064-A (1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) On the overhead panel 23VU:
- Make sure that the ELAC 1 and SEC 1 pushbutton switches are pushed (the OFF and FAULT legends are off).
- Make sure that the ELAC 2, SEC 2 and SEC 3 pushbutton switches are pushed (the OFF and FAULT legends are off).
- Set the 3 OFF/NAV/ATT selector switches to NAV.
- Make sure that the PTU pushbutton switch is set to AUTO.
(7) On the center pedestal, on the ECAM control panel push:
- The CLEAR key until all the warnings (if any) stop
- The F/CTL key (on the lower ECAM display unit, the F/CTL page comes into view).
(Ref. AMM TASK 29-23-00-864-001) (Ref. AMM TASK 29-24-00-864-001).
(9) Pressurize the Blue hydraulic system
(Ref. AMM TASK 29-10-00-863-003).
B. Get Access
(1) Put the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE in position at the access door 822.
(2) Open the access door 822 (Ref. AMM TASK 52-41-00-010-002).
(3) On the battery power center 105VU:
Subtask 27-96-00-865-073-A (1) Put the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE in position at the access door 822.
(2) Open the access door 822 (Ref. AMM TASK 52-41-00-010-002).
(3) On the battery power center 105VU:
- Loosen the two screws and remove the protective cover.
C. Make sure that this(these) circuit breaker(s) is(are) closed:
Subtask 27-96-00-865-076-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/ELAC1/NORM/SPLY | 15CE1 | B11 |
| 49VU | FLIGHT CONTROLS/THS/ACTR/MOT2 | 19CE2 | B09 |
| 49VU | FLIGHT CONTROLS/SEC1/NORM/SPLY | 21CE1 | B08 |
| ** ON A/C ALL | |||
| 49VU | L/G/LGCIU/SYS1/NORM | 1GA | C09 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/ELAC1/NORM/SPLY | 15CE1 | B06 |
| 49VU | FLIGHT CONTROLS/THS/ACTR/MOT2 | 19CE2 | B04 |
| 49VU | FLIGHT CONTROLS/SEC1/NORM/SPLY | 21CE1 | B03 |
| ** ON A/C ALL | |||
| 105VU | FLIGHT CONTROLS/ELAC2/STBY SPLY | 16CE2 | A02 |
| 105VU | FLT CTL/ELAC1/STBY SPLY | 16CE1 | A01 |
| 105VU | FLT CTL/SEC1/STBY SPLY | 22CE | B01 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | LGCIU/BAT SPLY/SYS1 | 58GA | R32 |
| ** ON A/C ALL | |||
| 121VU | HYDRAULIC/LGCIU/SYS1/GRND SPLY | 52GA | Q34 |
| 121VU | FLIGHT CONTROLS/SEC3/SPLY | 21CE3 | Q19 |
| 121VU | FLIGHT CONTROLS/SEC2/SPLY | 21CE2 | Q18 |
| 121VU | FLIGHT CONTROLS/THS ACTR/MOT3 | 19CE3 | Q17 |
| 121VU | FLIGHT CONTROLS/THS ACTR/MOT1 | 19CE1 | Q16 |
| 121VU | FLIGHT CONTROLS/ELAC2/NORM/SPLY | 15CE2 | R20 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | LGCIU/BAT SPLY/SYS1 | 58GA | R31 |
D. Open, safety and tag this(these) circuit breaker(s):
4. Procedure| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C ALL | |||
| 49VU | ANTI ICE/PROBES/AOA/1 | 4DA1 | D04 |
| 49VU | ANTI ICE/PROBES/PITOT/1 | 3DA1 | D02 |
| 122VU | ANTI ICE/WINDOWS/R | 4DG2 | W14 |
| 122VU | ANTI ICE/WHC/2 | 5DG2 | W13 |
| 122VU | ANTI ICE/WINDOWS/L | 4DG1 | X14 |
| 122VU | ANTI ICE/WHC/1 | 5DG1 | X13 |
| 122VU | ANTI ICE/PROBES/2/TAT | 1DA2 | Y15 |
| 122VU | ANTI ICE/PROBES/2/PITOT | 3DA2 | Y14 |
| 122VU | ANTI ICE/PROBES/2/AOA | 4DA2 | Y13 |
| 122VU | ANTI ICE/PROBES/2/STATIC | 5DA2 | Y11 |
| 122VU | ANTI ICE/PROBES/3/PITOT | 3DA3 | Z16 |
| 122VU | ANTI ICE/PROBES/3/AOA | 4DA3 | Z15 |
| 122VU | ANTI ICE/PROBES/3/STATIC | 5DA3 | Z14 |
| 122VU | ANTI ICE/PROBES/1/STATIC | 5DA1 | Z13 |
| 122VU | ANTI ICE/PROBES/1/TAT | 1DA1 | Z12 |
Subtask 27-96-00-710-082-D
A. Operational Test of the Logics that activate the ELAC 1 & 2 and SEC 1 STBY PWR SPLY
Subtask 27-96-00-710-090-A ** ON A/C NOT FOR ALL NOTE: During the test, ignore the MASTER CAUT light and single chime.
NOTE: If the result of the test is not satisfactory, refer to the trouble shooting procedure TSM 27-96-00-810-801.
| ACTION | RESULT |
|---|---|
| 1.Open the circuit breakers 15CE1 and 21CE1. | On the FLT CTL section of the overhead panel 23VU:
|
2.On the overhead panel 50VU:
| On the overhead panel 50VU:
|
| | On the overhead panel 23VU:
|
| | After approximately 30 seconds:
|
3.On the overhead panel 50VU:
| On the overhead panel 50VU:
|
| | The above warnings are still shown. |
| 4.Close the circuit breakers 15CE1 and 21CE1. | On the FLT CTL section of the overhead panel 23VU:
|
| | On the upper ECAM display unit:
|
| | On the lower ECAM display unit:
|
| 5.Open the circuit breakers 58GA, 52GA, 1GA and 15CE2. NOTE: Ignore the warning related to the other systems. | On the overhead panel 24VU:
|
| | On the upper ECAM display unit:
|
| | On the lower ECAM display unit:
|
| 6.Open the circuit breaker 19CE1. | On the overhead panel 24VU:
|
| | On the upper ECAM display unit:
|
| | On the lower ECAM display unit:
|
| | After approximately 30 seconds:
|
7.On the overhead panel 40VU:
| On the overhead panel 40VU:
|
8.On the overhead panel 50VU:
| On the overhead panel 50VU:
|
| | On the overhead panel 24VU:
|
| | On the upper ECAM display unit:
|
| | On the lower ECAM display unit:
|
9.On the overhead panel 50VU:
| On the overhead panel 50VU:
|
| | On the upper ECAM display unit:
|
| | On the lower ECAM display unit:
|
| | On the overhead panel 24VU:
|
10.On the overhead panel 40VU:
| On the overhead panel 40VU:
|
| 11.Close the circuit breakers 58GA, 1GA and 52GA. | On the lower ECAM display unit:
|
| | On the upper ECAM display unit:
|
| 12.Open the circuit breakers 58GA, 1GA and 52GA. | On the lower ECAM display unit:
|
| | On the upper ECAM display unit:
|
| | On the overhead panel 24VU:
|
| 13.Close the circuit breakers 58GA, 1GA and 52GA. | On the lower ECAM display unit:
|
| | On the upper ECAM display unit:
|
| | On the overhead panel 24VU:
|
| 14.Go to Para. B. | |
B. Operational Test of the Sidestick Priority Function
Subtask 27-96-00-710-090-G ** ON A/C NOT FOR ALL NOTE: During the test, ignore the MASTER CAUT light and single chime.
NOTE: If the result of the test is not satisfactory, refer to the trouble shooting procedure TSM 27-96-00-810-801.
| ACTION | RESULT |
|---|---|
1.On the overhead panel 23VU:
| On the overhead panel 23VU:
|
| | On the lower ECAM display unit:
|
2.On the overhead panel 23VU:
| On the overhead panel 23VU:
|
| | On the overhead panel 24VU:
|
| | On the lower ECAM display unit:
|
| | On the upper ECAM display unit:
|
3.On the overhead panel 23VU:
| On the overhead panel 23VU:
|
| | On the overhead panel 24VU:
|
| | On the lower ECAM display unit:
|
| | On the upper ECAM display unit:
|
4.On the overhead panel 23VU:
| On the overhead panel 23VU:
|
| | On the lower ECAM display unit:
|
5.At the same time:
| You can hear an aural warning: PRIORITY LEFT. On the F/O side, on the glareshield panel 130VU:
|
| On the CAPT side, on the glareshield panel 131VU:
|
6.On the CAPT side:
| On the F/O side, on the glareshield panel 130VU:
|
7.At the same time:
| You can hear an aural warning: PRIORITY RIGHT. On the CAPT side, on the glareshield panel 131VU:
|
| On the F/O side, on the glareshield panel 130VU:
|
8.On the F/O side:
| On the CAPT side, on the glareshield panel 131VU:
|
| 9.Go to Para. C. | |
B. Operational Test of the Sidestick Priority Function
Subtask 27-96-00-710-089-B ** ON A/C NOT FOR ALL NOTE: During the test, ignore the MASTER CAUT light and single chime.
NOTE: If the result of the test is not satisfactory, refer to the trouble shooting procedure TSM 27-96-00-810-801.
| ACTION | RESULT |
|---|---|
1.On the overhead panel 23VU:
| On the overhead panel 23VU:
|
| | On the lower ECAM display unit:
|
2.On the overhead panel 23VU:
| On the overhead panel 23VU:
|
| | On the overhead panel 24VU:
|
| | On the lower ECAM display unit:
|
| | On the upper ECAM display unit:
|
3.On the overhead panel 23VU:
| On the overhead panel 23VU:
|
| | On the overhead panel 24VU:
|
| | On the lower ECAM display unit:
|
| | On the upper ECAM display unit:
|
4.On the overhead panel 23VU:
| On the overhead panel 23VU:
|
| | On the lower ECAM display unit:
|
5.On the CAPT and F/O sides:
| You can hear an aural announcement: DUAL INPUT |
| | On the glareshield panels 130VU and 131VU, on the SIDE STICK PRIORITY/CAPT and the SIDE STICK PRIORITY F/O annunciators:
|
6.At the same time:
| You can hear an aural warning: PRIORITY LEFT. On the F/O side, on the glareshield panel 130VU:
|
| On the CAPT side, on the glareshield panel 131VU:
|
7.On the CAPT side:
| On the F/O side, on the glareshield panel 130VU:
|
8.At the same time:
| You can hear an aural warning: PRIORITY RIGHT. On the CAPT side, on the glareshield panel 131VU:
|
| On the F/O side, on the glareshield panel 130VU:
|
9.On the F/O side:
| On the CAPT side, on the glareshield panel 131VU:
|
| 10.Go to Para. C. | |
C. Check of the Ailerons movement
Subtask 27-96-00-710-089-C ** ON A/C NOT FOR ALL | ACTION | RESULT |
|---|---|
1.On the CAPT side:
| On the lower ECAM display unit:
|
2.On the CAPT side:
| On the lower ECAM display unit:
|
3.On the CAPT side:
| On the lower ECAM display unit:
|
| 4.Close the circuit breakers 15CE2 and 19CE1. | On the overhead panel 24VU:
|
| | On the lower ECAM display unit:
|
| 5.Go to Para D. | |
C. Check of the Ailerons movement
Subtask 27-96-00-710-089-L ** ON A/C NOT FOR ALL | ACTION | RESULT |
|---|---|
1.On the CAPT side:
| On the lower ECAM display unit:
|
2.On the CAPT side:
| On the lower ECAM display unit:
|
3.On the CAPT side:
| On the lower ECAM display unit:
|
| 4.Close the circuit breakers 15CE2 and 19CE1. | On the overhead panel 24VU:
|
| | On the lower ECAM display unit:
|
| 5.Go to Para D. | |
C. Check of the Ailerons movement
Subtask 27-96-00-710-084-A | ACTION | RESULT |
|---|---|
1.On the CAPT side:
| On the lower ECAM display unit:
|
2.On the CAPT side:
| On the lower ECAM display unit:
|
3.On the CAPT side:
| On the lower ECAM display unit:
|
| 4.Close the circuit breakers 15CE2 and 19CE1. | On the overhead panel 24VU:
|
| | On the lower ECAM display unit:
|
| 5.Go to Para D. | |
D. Operational Test of the Ability of the ELAC 1 and SEC 1 & 2 to Achieve Pitch Control
5. Close-upNOTE: During the test, ignore the MASTER CAUT light and single chime.
NOTE: If the result of the test is not satisfactory, refer to the trouble shooting procedure TSM 27-96-00-810-802.
| ACTION | RESULT |
|---|---|
| 1.Pressurize the Green and Yellow hydraulic systems. (Ref. AMM TASK 29-23-00-863-001) (Ref. AMM TASK 29-24-00-863-001). | On the lower ECAM display unit, the G and Y indications become green. |
| 2.Depressurize the Blue hydraulic system (Ref. AMM TASK 29-10-00-864-003). | On the lower ECAM display unit, the B indication becomes amber. |
| 3.Wait for 5 seconds. | |
| 4.Pressurize the Blue hydraulic system (Ref. AMM TASK 29-10-00-863-003). | On the lower ECAM display unit, the B indication becomes green. |
5.On the overhead panel 23VU:
| On the overhead panel 23VU:
|
6.On the overhead panel 24VU:
| On the overhead panel 24VU:
|
7.On the CAPT or F/O side:
| On the lower ECAM display unit:
|
8.On the overhead panel 23VU:
| On the overhead panel 23VU:
|
9.On the overhead panel 24VU:
| On the overhead panel 24VU:
|
| 10.Depressurize the Green and Yellow hydraulic systems. (Ref. AMM TASK 29-23-00-864-001) (Ref. AMM TASK 29-24-00-864-001). | On the lower ECAM display unit, the G and Y indications become amber. |
| 11.Wait for 5 seconds. | |
| 12.Pressurize the Green and Yellow hydraulic systems (Ref. AMM TASK 29-23-00-863-001) (Ref. AMM TASK 29-24-00-863-001). | On the lower ECAM display unit, the G and Y indications become green. |
13.On the overhead panel 23VU:
| On the overhead panel 23VU:
|
14.On the overhead panel 24VU:
| On the overhead panel 24VU:
|
15.On the CAPT side:
| On the lower ECAM display unit, on the F/CTL page:
|
16.On the F/O side:
| On the lower ECAM display unit, on the F/CTL page:
|
| 17.Set the pitch-trim control wheel to the 10 UP position. | |
18.On the overhead panel 24VU:
| After approximately five seconds, the pitch-trim control wheel goes back automatically to the O position. |
| | On the lower ECAM display unit, on the F/CTL page:
|
| 19.Set the pitch-trim control wheel to the 3 DN position. | |
20.On the overhead panel 24VU:
| After approximately five seconds, the pitch-trim control wheel goes back automatically to the O position. |
| | On the lower ECAM display unit, on the F/CTL page:
|
21.On the overhead panel 23VU:
| On the overhead panel 23VU:
|
22.On the overhead panel 24VU:
| On the overhead panel 24VU:
|
| 23.Depressurize the Blue hydraulic system (Ref. AMM TASK 29-10-00-864-003). | On the lower ECAM display unit, the B indication becomes amber. |
| 24.Wait for 5 seconds. | |
| 25.Pressurize the Blue hydraulic system (Ref. AMM TASK 29-10-00-863-003). | On the lower ECAM display unit, the B indication becomes green. |
26.On the overhead panel 23VU:
| On the overhead panel 23VU:
|
27.On the overhead panel 24VU:
| On the overhead panel 24VU:
|
28.On the CAPT side:
| On the lower ECAM display unit, on the F/CTL page:
|
29.On the F/O side:
| On the lower ECAM display unit, on the F/CTL page:
|
| 30.Set the pitch-trim control wheel to the 10 UP position. | |
31.On the overhead panel 23VU:
| After approximately five seconds, the pitch-trim control wheel goes back automatically to the O position. |
| | On the lower ECAM display unit, on the F/CTL page:
|
| 32.Set the pitch-trim control wheel to the 3 DN position. | |
33.On the overhead panel 23VU:
| After approximately five seconds, the pitch-trim control wheel goes back automatically to the O position. |
| | On the lower ECAM display unit, on the F/CTL page:
|
| 34.Open the circuit breakers 15CE1 and 15CE2. | On the upper ECAM display unit:
|
35.On the CAPT or F/O side:
| On the lower ECAM display unit, on the F/CTL page:
|
36.On the overhead panel 24VU:
| On the overhead panel 24VU:
|
37.On the overhead panel 23VU:
| On the overhead panel 23VU:
|
38.On the CAPT or F/O side:
| On the lower ECAM display unit, on the F/CTL page:
|
| 39.Close the circuit breakers 15CE1 and 15CE2. | On the upper ECAM display unit:
|
Subtask 27-96-00-865-077-A
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 27-96-00-860-084-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C ALL | |||
| 49VU | ANTI ICE/PROBES/AOA/1 | 4DA1 | D04 |
| 49VU | ANTI ICE/PROBES/PITOT/1 | 3DA1 | D02 |
| 122VU | ANTI ICE/WINDOWS/R | 4DG2 | W14 |
| 122VU | ANTI ICE/WHC/2 | 5DG2 | W13 |
| 122VU | ANTI ICE/WINDOWS/L | 4DG1 | X14 |
| 122VU | ANTI ICE/WHC/1 | 5DG1 | X13 |
| 122VU | ANTI ICE/PROBES/2/TAT | 1DA2 | Y15 |
| 122VU | ANTI ICE/PROBES/2/PITOT | 3DA2 | Y14 |
| 122VU | ANTI ICE/PROBES/2/AOA | 4DA2 | Y13 |
| 122VU | ANTI ICE/PROBES/2/STATIC | 5DA2 | Y11 |
| 122VU | ANTI ICE/PROBES/3/PITOT | 3DA3 | Z16 |
| 122VU | ANTI ICE/PROBES/3/AOA | 4DA3 | Z15 |
| 122VU | ANTI ICE/PROBES/3/STATIC | 5DA3 | Z14 |
| 122VU | ANTI ICE/PROBES/1/STATIC | 5DA1 | Z13 |
| 122VU | ANTI ICE/PROBES/1/TAT | 1DA1 | Z12 |
B. Put the aircraft back to the initial configuration
(1) Depressurize the aircraft hydraulic systems
(Ref. AMM TASK 29-23-00-864-001) (Ref. AMM TASK 29-24-00-864-001) (Ref. AMM TASK 29-10-00-864-003).
(2) On the overhead panel 23VU:
(Ref. AMM TASK 31-60-00-860-002).
(6) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
(7) Remove the warning notice.
Subtask 27-96-00-860-084-B ** ON A/C NOT FOR ALL (1) Depressurize the aircraft hydraulic systems
(Ref. AMM TASK 29-23-00-864-001) (Ref. AMM TASK 29-24-00-864-001) (Ref. AMM TASK 29-10-00-864-003).
(2) On the overhead panel 23VU:
- Push the ELAC 1 and SEC 1 pushbutton switches (the OFF legends go off).
- Push the ELAC 2 pushbutton switch (the OFF legend goes off).
- Set the 3 OFF/NAV/ATT selector switches to OFF.
(Ref. AMM TASK 31-60-00-860-002).
(6) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
(7) Remove the warning notice.
B. Put the aircraft back to the initial configuration
(1) Depressurize the aircraft hydraulic systems
(Ref. AMM TASK 29-23-00-864-001) (Ref. AMM TASK 29-24-00-864-001) (Ref. AMM TASK 29-10-00-864-003).
(2) On the overhead panel 23VU:
(Ref. AMM TASK 31-60-00-860-002).
(6) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
(7) Remove the warning notice.
Subtask 27-96-00-410-065-A (1) Depressurize the aircraft hydraulic systems
(Ref. AMM TASK 29-23-00-864-001) (Ref. AMM TASK 29-24-00-864-001) (Ref. AMM TASK 29-10-00-864-003).
(2) On the overhead panel 23VU:
- Push the ELAC 1 and SEC 1 pushbutton switches (the OFF legends go off).
- Push the ELAC 2 pushbutton switch (the OFF legend goes off).
- Set the 3 OFF/NAV/ATT selector switches to OFF.
(Ref. AMM TASK 31-60-00-860-002).
(6) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
(7) Remove the warning notice.
C. Close Access
(1) On the battery power center 105VU:
(3) Remove the access platform(s).
(1) On the battery power center 105VU:
- Install the protective cover and tighten the two screws.
(3) Remove the access platform(s).