BITE Test of the Integrated Standby Instrument System (ISIS) Indicator with the Pushbutton Switches on the Face of the Indicator
TASK 34-22-25-740-001-A
BITE Test of the Integrated Standby Instrument System (ISIS) Indicator with the Pushbutton Switches on the Face of the Indicator
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 34-22-25-860-052-A ** ON A/C NOT FOR ALL
Subtask 34-22-25-740-050-A ** ON A/C NOT FOR ALL
Subtask 34-22-25-860-051-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.02 07:14:40 UTC
BITE Test of the Integrated Standby Instrument System (ISIS) Indicator with the Pushbutton Switches on the Face of the Indicator
ZONE: 210
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 |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 210 | CKPT,FWD COMPT BHD TO FLT COMPT BULKHEAD |
| 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 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) |
| TASK 34-10-00-860-005-A | ADIRS Stop Procedure |
Subtask 34-22-25-860-052-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) Do the IR Alignment procedure (Ref. AMM TASK 34-10-00-860-004)
Subtask 34-22-25-865-050-A ** ON A/C NOT FOR ALL (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)
B. Open, safety and tag this(these) circuit breaker(s):
Subtask 34-22-25-865-051-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | NAV/STBY/INST | 5FN | F12 |
C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 34-22-25-860-050-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | NAV/STBY/INST | 5FN | F12 |
D. Aircraft Maintenance Configuration
(1) On the center instrument panel 401VU, on the ISIS indicator:
4. Procedure(1) On the center instrument panel 401VU, on the ISIS indicator:
- Make sure that the INIT 90 s indication comes into view
- Make sure that the Functions page comes into view.
Subtask 34-22-25-740-050-A ** ON A/C NOT FOR ALL
A. BITE Test of the Integrated Standby Instrument System (ISIS) Indicator
(1) Make sure that you do not move the aircraft during the alignment period (110s indication) of this test.
(2) Do the BITE test of the ISIS indicator as follows:
Subtask 34-22-25-740-055-A ** ON A/C NOT FOR ALL (1) Make sure that you do not move the aircraft during the alignment period (110s indication) of this test.
(2) Do the BITE test of the ISIS indicator as follows:
| ACTION | RESULT |
|---|---|
| 1.On center instrument panel 401VU, on the ISIS indicator: | On center instrument panel 401VU, on the ISIS indicator: |
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B. BITE Test of the Integrated Standby Instrument System (ISIS) Indicator
(1) Make sure that you do not move the aircraft during the alignment period (110s) of this test.
(2) Do the BITE test of the ISIS indicator as follows:
5. Close-up(1) Make sure that you do not move the aircraft during the alignment period (110s) of this test.
(2) Do the BITE test of the ISIS indicator as follows:
| ACTION | RESULT |
|---|---|
| 1.On center instrument panel 401VU, on the ISIS indicator: | On center instrument panel 401VU, on the ISIS indicator: |
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Subtask 34-22-25-860-051-A ** ON A/C NOT FOR ALL
A. Put the aircraft back to its initial configuration.
(1) Do the ADIRS Stop procedure (Ref. AMM TASK 34-10-00-860-005)
(2) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
(1) Do the ADIRS Stop procedure (Ref. AMM TASK 34-10-00-860-005)
(2) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).