Operational Test of the Side Stick Assembly
TASK 27-92-41-710-001-A
Operational Test of the Side Stick Assembly
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 27-92-41-860-054-A
Subtask 27-92-41-710-052-A
Subtask 27-92-41-860-055-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.01 04:25:18 UTC
Operational Test of the Side Stick Assembly
WARNING:
MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED BEFORE YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT. UNWANTED ELECTRICAL POWER CAN BE DANGEROUS.
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.
NOTE: Two persons are necessary for this procedure.
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) - ADJUSTABLE |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 211 | COCKPIT |
| 212 | COCKPIT |
| 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 34-10-00-860-004-A | Inertial Reference (IR) Alignment-Procedure |
| TASK 34-10-00-860-004-A-01 | Automatic Inertial Reference (IR) Alignment-Procedure |
| TASK 34-10-00-860-004-A-02 | Inertial Reference (IR) Alignment-Procedure to do a Check of the Links between each Flight Management and Guidance Computer (FMGC) and the three Air Data/Inertial Reference Units (ADIRUs) |
Subtask 27-92-41-860-054-A
A. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) Do the IR alignment procedure (Ref. AMM TASK 34-10-00-860-004).
(3) On the panel 23VU:
(6) On the center pedestal, on the ECAM control panel, push the F/CTL key (on the lower ECAM display unit, the F/CTL page comes into view).
(7) On the overhead panel 50VU:
(Ref. AMM TASK 29-23-00-863-001) (Ref. AMM TASK 29-24-00-863-001) (Ref. AMM TASK 29-10-00-863-003).
Subtask 27-92-41-010-071-A (1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) Do the IR alignment procedure (Ref. AMM TASK 34-10-00-860-004).
(3) On the panel 23VU:
- release the FLT CTL/ELAC 1 and FLT CTL/SEC 1 pushbutton switches (on these pushbutton switches, the OFF legends come on)
- make sure that the FLT CTL/FAC1 is engaged (on this pushbutton switch, the OFF legends is off).
- release the FLT CTL/ELAC 2, FLT CTL/SEC 2 and FLT CTL/SEC 3 pushbutton switches (on these pushbutton switches, the OFF legends come on)
- make sure that the FLT CTL/FAC2 is engaged (on this pushbutton switch, the OFF legend is off).
(6) On the center pedestal, on the ECAM control panel, push the F/CTL key (on the lower ECAM display unit, the F/CTL page comes into view).
(7) On the overhead panel 50VU:
- make sure that the SVCE INT OVRD pushbutton switch is released (the ON legend is off).
- make sure that the AUDIO SWITCHING selector switch is at NORM.
- the INT/RAD switches are set to the middle position
- the legends of all the transmission pushbutton switches are off
- all the reception pushbutton switches are pushed (no reception).
(Ref. AMM TASK 29-23-00-863-001) (Ref. AMM TASK 29-24-00-863-001) (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.
(3) On the battery power center 105VU:
Subtask 27-92-41-865-061-A (1) Put the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE in position at the access door 822.
(2) Open the access door 822.
(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:
4. Procedure| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/ELAC1/NORM/SPLY | 15CE1 | B11 |
| 49VU | FLIGHT CONTROLS/FCDC1/SPLY | 20CE1 | B10 |
| 49VU | FLIGHT CONTROLS/SEC1/NORM/SPLY | 21CE1 | B08 |
| 49VU | FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 | 6CV | B07 |
| 49VU | FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 | 5CV | B06 |
| 49VU | AUTO FLT/FCU/1 | 9CA1 | B05 |
| 49VU | AUTO FLT/FMGC/1 | 10CA1 | B02 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | COM/AUDIO/ACP/F/O | 5RN | G07 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | COM/AUDIO/FLT/INTPH | 9RN | G08 |
| 49VU | COM/AUDIO/ACP/CAPT | 4RN | G06 |
| ** ON A/C ALL | |||
| 49VU | CAPT/LOUD/SPKR | 5WW | F10 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | COM/ACP F/O/BITE/ INT 2 AUDIO/3&5 OCCPNT | 5RN | G07 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | COM/INT/1+2 | 9RN | G08 |
| 49VU | COM/ACP CAPT/SELCAL/INT 1 AUDIO/AVNCS | 4RN | G06 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/ELAC1/NORM/SPLY | 15CE1 | B06 |
| 49VU | FLIGHT CONTROLS/FCDC1/SPLY | 20CE1 | B05 |
| 49VU | FLIGHT CONTROLS/SEC1/NORM/SPLY | 21CE1 | B03 |
| 49VU | FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 | 6CV | B02 |
| 49VU | FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 | 5CV | B01 |
| 49VU | AUTO FLT/FCU/1 | 9CA1 | H11 |
| 49VU | AUTO FLT/FMGC/1 | 10CA1 | H08 |
| ** 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 | AUTO FLT/STICK/LOCK | 13CA | N16 |
| ** ON A/C ALL | |||
| 121VU | AUTO FLT/FCU/2 | 9CA2 | M21 |
| 121VU | AUTO FLT/FMGC/2 | 10CA2 | M17 |
| 121VU | COM NAV/ACP/THIRD/OCCPNT | 6RN | M02 |
| 121VU | EIS/F/O/LOUD/SPKR | 4WW | P08 |
| 121VU | FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 | 8CV | Q21 |
| 121VU | FLIGHT CONTROLS/FCDC2/SPLY | 20CE2 | Q20 |
| 121VU | FLIGHT CONTROLS/SEC3/SPLY | 21CE3 | Q19 |
| 121VU | FLIGHT CONTROLS/SEC2/SPLY | 21CE2 | Q18 |
| 121VU | FLIGHT CONTROLS/SLT/CTL/SYS2 | 7CV | R21 |
| 121VU | FLIGHT CONTROLS/ELAC2/NORM/SPLY | 15CE2 | R20 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | AUTO FLT/STICK/LOCK | 13CA | N18 |
Subtask 27-92-41-710-052-A
A. Operational Test of the Side Stick Assembly
5. Close-upNOTE: During the test, on the F/CTL page:
- make sure that the indexes move to the full range (index in the fixed white scale).
| ACTION | RESULT |
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1.On the overhead panel 23VU:
| On this pushbutton switch:
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2.On the CAPT (F/O) side:
| On the lower ECAM display unit:
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3.On the overhead panel 23VU:
| On this pushbutton switch:
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4.On the overhead panel 24VU:
| On this pushbutton switch:
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5.On the CAPT (F/O) side:
| On the lower ECAM display unit:
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6.On the overhead panel 24VU:
| On this pushbutton switch:
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7.On the overhead panel 23VU:
| On this pushbutton switch:
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8.On the CAPT (F/O) side:
| On the lower ECAM display unit:
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9.On the overhead panel 23VU:
| On this pushbutton switch:
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10.On the overhead panel 24VU:
| On this pushbutton switch:
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11.On the CAPT (F/O) side:
| On the lower ECAM display unit:
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12.On the overhead panel 24VU:
| On this pushbutton switch:
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13.On the overhead panel 24VU:
| On this pushbutton switch:
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14.On the CAPT (F/O) side:
| On the lower ECAM display unit:
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15.On the overhead panel 24VU:
| On this pushbutton switch:
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16.On the overhead panel 23VU:
| On these pushbutton switches:
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17.On the CAPT (F/O) lateral console on the side stick:
| You can hear a synthetic voice. On the panel 130VU (131VU):
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18.On the CAPT (F/O) side:
| On the lower ECAM display unit:
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19.On the F/O (CAPT) side:
| On the lower ECAM display unit, on the F/CTL page:
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| On the panel 131VU (130VU), on the SIDE STICK PRIORITY/CAPT (SIDE STICK PRIORITY/F/O) annunciator light:
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20.On the F/O (CAPT) lateral console, on the side stick:
| On the panel 130VU (131VU):
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21.On the CAPT (F/O) side:
| On the lower ECAM display unit:
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22.On the overhead panel 23VU:
| On these pushbutton switches:
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23.On the overhead panel 24VU:
| On these pushbutton switches:
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24.On the CAPT (F/O) lateral console on the side stick:
| You can hear a synthetic voice. On the panel 130VU (131VU):
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25.On the CAPT (F/O) side:
| On the lower ECAM display unit:
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| 26.On the F/O (CAPT) lateral console: Give the orders below one after the other and keep the side stick in each position during 3 seconds: | On the lower ECAM display unit, on the F/CTL page:
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| On the panel 131VU (130VU), on the SIDE STICK PRIORITY/CAPT (SIDE STICK PRIORITY/F/O) annunciator light:
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27.On the F/O (CAPT) lateral console, on the side stick controller:
| On the panel 130VU (131VU):
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28.On the CAPT (F/O) side:
| On the lower ECAM display unit:
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29.On the overhead panel 23VU:
| On this pushbutton switch:
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30.On the FCU:
NOTE: If they are not engaged, push the FD pushbutton switches on the FCU (glareshield 13VU). | |
31.On the FCU:
| This pushbutton switch comes on. On the upper section of the PFDs:
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32.On the CAPT (F/O) side stick controller:
| The AP 2 disengages. On the FCU:
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| 33.Engage the AP 2 again. | This pushbutton switch comes on. On the upper section of the PFDs:
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| 34.On the CAPT (F/O) side stick: | |
| The side stick controller is locked. |
| The AP 2 disengages. You can hear the cavalry charge warning. On the left part of the upper ECAM display unit
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| 35.On the glareshield, push the MASTER WARN light to cancel the AP warnings. | All the warnings stop, but the AUTO FLT AP OFF indication stays in view on the left part of the upper ECAM display unit. |
| 36.On the center pedestal, on the ECAM control panel, push the CLR key. | On the upper ECAM display unit, the AUTO FLT AP OFF indication goes out of view. |
37.On the overhead panel 23VU:
| On this pushbutton switch:
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| 38.On the center pedestal, on the CAPT (F/O) ACP: | |
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| 39.On the CAPT (F/O) side stick: | |
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| 40.On the center pedestal, on the CAPT (F/O) ACP: | |
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Subtask 27-92-41-860-055-A ** ON A/C NOT FOR ALL
A. Put the aircraft back to its 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) Put the system back to the serviceable condition.
(3) On the overhead panel, on the ADIRS CDU, set the OFF/NAV/ATT selector switches to OFF (Ref. AMM TASK 31-60-00-860-002).
(4) Do the EIS stop procedure (Ref. AMM TASK 31-60-00-860-002).
(5) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
Subtask 27-92-41-860-055-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) Put the system back to the serviceable condition.
(3) On the overhead panel, on the ADIRS CDU, set the OFF/NAV/ATT selector switches to OFF (Ref. AMM TASK 31-60-00-860-002).
(4) Do the EIS stop procedure (Ref. AMM TASK 31-60-00-860-002).
(5) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
A. Put the aircraft back to its 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) Put the system back to the serviceable condition.
(3) On the overhead panel 41VU, on the ADIRS MSU, set the OFF/NAV/ATT selector switches to OFF (Ref. AMM TASK 31-60-00-860-002).
(4) Do the EIS stop procedure (Ref. AMM TASK 31-60-00-860-002).
(5) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
Subtask 27-92-41-410-068-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) Put the system back to the serviceable condition.
(3) On the overhead panel 41VU, on the ADIRS MSU, set the OFF/NAV/ATT selector switches to OFF (Ref. AMM TASK 31-60-00-860-002).
(4) Do the EIS stop procedure (Ref. AMM TASK 31-60-00-860-002).
(5) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
B. Close Access
(1) Install the protective cover on the battery power center 105VU.
(2) Tighten the two screws.
(3) Close the access door 822.
(4) Remove the access platform(s).
(1) Install the protective cover on the battery power center 105VU.
(2) Tighten the two screws.
(3) Close the access door 822.
(4) Remove the access platform(s).