Functional Test of the bulk-erase function and bulk-erase inhibition-logic of the CVR
TASK 23-71-00-720-002-A
Functional Test of the bulk-erase function and bulk-erase inhibition-logic of the CVR
To make sure that the CVR will erase only when the aircraft is on the ground with the parking brake set.
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 23-71-00-860-057-A ** ON A/C NOT FOR ALL
Subtask 23-71-00-720-050-A ** ON A/C NOT FOR ALL
Subtask 23-71-00-860-056-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.01 08:26:27 UTC
Functional Test of the bulk-erase function and bulk-erase inhibition-logic of the CVR
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.
NOTE: This procedure is applicable to the CVR and the SSCVR.
ZONE: 210
1. Reason for the JobTo make sure that the CVR will erase only when the aircraft is on the ground with the parking brake set.
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | 1 | HEADSET 600 OHMS |
| 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 32-69-00-860-001-A | Simulation of Flight (With Aircraft on Ground) |
Subtask 23-71-00-860-057-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) Make sure that the engine shutdown occured not less than 5 minutes before you do the procedure.
(3) On the maintenance panel 50VU, connect a HEADSET 600 OHMS to the CVR/HEAD SET connector.
Subtask 23-71-00-865-052-A ** ON A/C NOT FOR ALL (1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) Make sure that the engine shutdown occured not less than 5 minutes before you do the procedure.
(3) On the maintenance panel 50VU, connect a HEADSET 600 OHMS to the CVR/HEAD SET connector.
B. Make sure that this(these) circuit breaker(s) is(are) closed:
4. Procedure| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | COM/CVR/SPLY | 2RK | E14 |
| 49VU | COM/CVR/CTL | 4RK | E13 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | COM/CVR/SPLY | 23RK | E14 |
| 49VU | COM/CVR/CTL | 26RK | E13 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | HYDRAULIC/PARK BRK/CTL/STBY | 71GG | N37 |
| 121VU | HYDRAULIC/PARK BRK/CTL/NORM | 70GG | N36 |
Subtask 23-71-00-720-050-A ** ON A/C NOT FOR ALL
A. Do the functional test with the parking brake locked and the aircraft in the ground configuration:
(1) Aircraft Maintenance Configuration
(a) On the panel 110VU, make sure that the Parking Brake Control Switch (73GG) is in the ON position.
(b) Make sure that the aircraft is on the ground (landing gear compressed).
(2) Test:
Subtask 23-71-00-720-054-A ** ON A/C NOT FOR ALL (1) Aircraft Maintenance Configuration
(a) On the panel 110VU, make sure that the Parking Brake Control Switch (73GG) is in the ON position.
(b) Make sure that the aircraft is on the ground (landing gear compressed).
(2) Test:
| ACTION | RESULT |
|---|---|
| 1.On the overhead control and indicating panel 21VU: | On the panel 21VU: |
|
|
| | In the headset:
|
| In the headset:
|
B. Do the functional test with the parking brake unlocked:
(1) Aircraft Maintenance Configuration
(a) On the panel 110VU, put the Parking Brake Control Switch (73GG) in the OFF position.
(b) Make sure that the aircraft is on the ground (landing gear compressed).
(2) Test:
Subtask 23-71-00-720-055-A ** ON A/C NOT FOR ALL (1) Aircraft Maintenance Configuration
(a) On the panel 110VU, put the Parking Brake Control Switch (73GG) in the OFF position.
(b) Make sure that the aircraft is on the ground (landing gear compressed).
(2) Test:
| ACTION | RESULT |
|---|---|
1.On the overhead control and indicating panel 21VU:
| In the headset:
|
C. Do the functional test with the aircraft in the flight configuration:
(1) Aircraft Maintenance Configuration
(a) On the panel 110VU, put the Parking Brake Control Switch (73GG) in the ON position.
(b) Put the aircraft in the flight configuration (Ref. AMM TASK 32-69-00-860-001).
(2) Test:
5. Close-up(1) Aircraft Maintenance Configuration
(a) On the panel 110VU, put the Parking Brake Control Switch (73GG) in the ON position.
(b) Put the aircraft in the flight configuration (Ref. AMM TASK 32-69-00-860-001).
(2) Test:
| ACTION | RESULT |
|---|---|
1.On the overhead control and indicating panel 21VU:
| In the headset:
|
Subtask 23-71-00-860-056-A ** ON A/C NOT FOR ALL
A. Put the aircraft back to its initial configuration.
(1) Disconnect the headset from the CVR/HEAD SET connector.
(2) Put the aircraft in the ground configuration (Ref. AMM TASK 32-69-00-860-001).
(3) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
(1) Disconnect the headset from the CVR/HEAD SET connector.
(2) Put the aircraft in the ground configuration (Ref. AMM TASK 32-69-00-860-001).
(3) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).