Operational Check of CVR Recording Logic Including Time Delay Relay
TASK 23-71-00-710-002-B
Operational Check of CVR Recording Logic Including Time Delay Relay
Refer to the MPD TASK: 237100-02
OPERATIONAL CHECK OF CVR RECORDING LOGIC INCLUDING TIME DELAY RELAY
To do a check of the flight or ground power supply of the CVR.
To do a check of the CVR power supply to the engines.
To make sure that recorder power-delay relays 46TU (for ENG1) and 45TU (for ENG2) operate correctly.
To make sure that oil low pressure and ground relay 10KS1 (for ENG1) operates correctly for the logic related to relay 46TU.
To make sure that oil low pressure and ground relay 12KS2 (for ENG2) operates correctly for the logic related to relay 45TU.
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 23-71-00-860-089-A ** ON A/C NOT FOR ALL
Subtask 23-71-00-710-062-A ** ON A/C NOT FOR ALL
Subtask 23-71-00-860-090-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.03.31 23:16:05 UTC
Operational Check of CVR Recording Logic Including Time Delay Relay
WARNING:
BEFORE YOU OPEN PHC CIRCUIT BREAKERS 2DA1(2,3), OPEN PROBE HEATER CIRCUIT-BREAKERS 1DA1(2), 3DA1(2,3), 4DA1(2,3) AND 5DA1(2,3). IF YOU DO NOT OBEY THIS SEQUENCE:
- THE PROBES WILL BECOME TOO HOT.
- THIS CAN CAUSE DAMAGE TO EQUIPMENT AND INJURY TO MAINTENANCE PERSONNEL.
NOTE: This procedure is applicable to the Cockpit Voice Recorder (CVR) and the Solid State Cockpit Voice Recorder (SSCVR).
NOTE: During the test, it is possible that you hear an audio signal related to the synchronization with the second recorder (Solid State Flight Data Recorder (SSFDR)). You can ignore it.
ZONE: 210
1. Reason for the JobRefer to the MPD TASK: 237100-02
OPERATIONAL CHECK OF CVR RECORDING LOGIC INCLUDING TIME DELAY RELAY
To do a check of the flight or ground power supply of the CVR.
To do a check of the CVR power supply to the engines.
To make sure that recorder power-delay relays 46TU (for ENG1) and 45TU (for ENG2) operate correctly.
To make sure that oil low pressure and ground relay 10KS1 (for ENG1) operates correctly for the logic related to relay 46TU.
To make sure that oil low pressure and ground relay 12KS2 (for ENG2) operates correctly for the logic related to relay 45TU.
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | 1 | HEADSET 600 OHMS |
| No specific | AR | STOPWATCH |
| 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) |
Subtask 23-71-00-860-089-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
(1) Wait for a minimum of five minutes after the engines were stopped.
(2) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(3) Make sure that the PARK BRK control handle is in the ON position.
(4) Make sure that the aircraft is in the ground configuration.
(5) On maintenance panel 50VU, connect the HEADSET 600 OHMS to the CVR/HEADSET connector.
Subtask 23-71-00-865-080-A ** ON A/C NOT FOR ALL (1) Wait for a minimum of five minutes after the engines were stopped.
(2) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(3) Make sure that the PARK BRK control handle is in the ON position.
(4) Make sure that the aircraft is in the ground configuration.
(5) On maintenance panel 50VU, connect the HEADSET 600 OHMS to the CVR/HEADSET connector.
B. Make sure that this(these) circuit breaker(s) is(are) closed:
Subtask 23-71-00-865-081-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | COM/CVR/SPLY | 23RK | E14 |
| 49VU | COM/CVR/CTL | 26RK | E13 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | ENGINE/2/FADEC A/AND EIU 2 | 2KS2 | A05 |
| 49VU | ENGINE/1/FADEC A/AND EIU 1 | 2KS1 | A04 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | RCDR1 CVR&FDR | 40TU | E14 |
| 49VU | RCDR CTL | 41TU | E13 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | ENGINE/ENG2/FADEC B/AND EIU2 | 4KS2 | Q40 |
| 121VU | ENGINE/ENG1/FADEC B/AND EIU 1 | 4KS1 | R41 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | ENGINE/ENG2/FADEC B/AND EIU2 | 4KS2 | R41 |
| 121VU | ENGINE/ENG1/FADEC B/AND EIU 1 | 4KS1 | R40 |
C. Open, safety and tag these circuit breakers in this sequence:
Subtask 23-71-00-865-082-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| FOR FIN: 9DA1 (PROBEPITOT, 1) | |||
| 122VU | ANTI ICE/PROBES/1/TAT | 1DA1 | Z12 |
| 49VU | ANTI ICE/PROBES/PITOT/1 | 3DA1 | D02 |
| 49VU | ANTI ICE/PROBES/AOA/1 | 4DA1 | D04 |
| 122VU | ANTI ICE/PROBES/1/STATIC | 5DA1 | Z13 |
| FOR FIN: 9DA2 (PROBEPITOT, 2) | |||
| 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 |
| FOR FIN: 9DA3 (PROBEPITOT, 3) | |||
| 122VU | ANTI ICE/PROBES/3/PITOT | 3DA3 | Z16 |
| 122VU | ANTI ICE/PROBES/3/AOA | 4DA3 | Z15 |
| 122VU | ANTI ICE/PROBES/3/STATIC | 5DA3 | Z14 |
D. Open, safety and tag these circuit breakers in this sequence:
4. Procedure| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| FOR FIN: 9DA1 (PROBEPITOT, 1) | |||
| 49VU | ANTI ICE/PROBES/PHC/1 | 2DA1 | D03 |
| FOR FIN: 9DA2 (PROBEPITOT, 2) | |||
| 122VU | ANTI ICE/PROBES/PHC/2 | 2DA2 | Y12 |
| FOR FIN: 9DA3 (PROBEPITOT, 3) | |||
| 122VU | ANTI ICE/PROBES/PHC/3 | 2DA3 | Y16 |
Subtask 23-71-00-710-062-A ** ON A/C NOT FOR ALL
A. Operational Test of the Recorder Power-Flight Control-Relay (23TU)
After you complete the test, set the parking brake back to ON.
Subtask 23-71-00-710-063-A ** ON A/C NOT FOR ALL NOTE: During the test, it is possible that you hear your voice in the headset.
During the test, if you hear a sound (Larsen effect), do the test of the CVR with headset jack 22RK and the parking brake set to OFF. Before you set the parking brake to OFF and start the test, install the wheel chocks or apply the brakes.After you complete the test, set the parking brake back to ON.
| ACTION | RESULT |
|---|---|
1.On the overhead panel, on panel 21VU:
| There is no tone in the headset. |
2.On panel 21VU:
| On panel 21VU, on the RCDR/GND CTL/AUTO pushbutton switch:
|
3.On panel 21VU:
| You can hear a tone in the headset connected to the CVR. |
4.On panel 21VU:
| On panel 21VU, on the RCDR/GND CTL/AUTO pushbutton switch:
|
B. Operational Test of Recorder-Power ENG1 Control-Relay 24TU, Time Delay of Recorder-Power ENG1 Delay-Relay 46TU of the CVR with Engine 1 and the Related Logic of Oil Low Pressure and Ground Relay 10KS1
After you complete the test, set the parking brake back to ON.
Subtask 23-71-00-710-065-A ** ON A/C NOT FOR ALL NOTE: The stopwatch is necessary to measure the time in the cockpit.
NOTE: During the test, it is possible that you hear your voice in the headset.
During the test, if you hear a sound (Larsen effect), do the test of the CVR with headset jack 22RK and the parking brake set to OFF. Before you set the parking brake to OFF and start the test, install the wheel chocks or apply the brakes.After you complete the test, set the parking brake back to ON.
| ACTION | RESULT |
|---|---|
1.On the overhead panel, on panel 21VU:
| There is no tone in the headset. |
2.On the overhead panel, on panel 49VU:
| |
3.On the rear panel, on panel 121VU:
| |
4.On panel 21VU:
| You can hear a tone in the headset connected to the CVR. NOTE: The test of relay 24TU is satisfactory. |
5.On panel 49VU:
| |
6.On panel 121VU:
| |
| 7.Immediately start the STOPWATCH in the cockpit. | |
| 8.On panel 21VU: | |
| You can hear a tone in the headset connected to the CVR. |
| There is no tone in the headset. NOTE: The test of relay 46TU is satisfactory with the related logic of relay 10KS1. |
C. Operational Test of Recorder-Power ENG2 Control-Relay 22TU, Time Delay of Recorder-Power ENG2 Delay-Relay 45TU of the CVR with Engine 2 and the Related Logic of Oil Low Pressure and Ground Relay 12KS2
After you complete the test, set the parking brake back to ON.
Subtask 23-71-00-710-064-A ** ON A/C NOT FOR ALL NOTE: The stopwatch is necessary to measure the time in the cockpit.
NOTE: During the test, it is possible that you hear your voice in the headset.
During the test, if you hear a sound (Larsen effect), do the test of the CVR with headset jack 22RK and the parking brake set to OFF. Before you set the parking brake to OFF and start the test, install the wheel chocks or apply the brakes.After you complete the test, set the parking brake back to ON.
| ACTION | RESULT |
|---|---|
1.On the overhead panel, on panel 21VU:
| There is no tone in the headset. |
2.On the overhead panel, on panel 49VU:
| |
3.On the rear panel, on panel 121VU:
| |
4.On panel 21VU:
| You can hear a tone in the headset connected to the CVR. NOTE: The test of relay 22TU is satisfactory. |
5.On panel 49VU:
| |
6.On panel 121VU:
| |
| 7.Immediately start the STOPWATCH in the cockpit. | |
| 8.On panel 21VU: | |
| You can hear a tone in the headset connected to the CVR. |
| There is no tone in the headset. NOTE: The test of relay 45TU is satisfactory with the related logic of relay 12KS2. |
D. Operational Test of Recorder-Power ENG1 Delay-Relay 46TU and Recorder-Power ENG2 Delay-Relay 45TU
After you complete the test, set the parking brake back to ON.
Subtask 23-71-00-865-083-A ** ON A/C NOT FOR ALL NOTE: During the test, it is possible that you hear your voice in the headset.
During the test, if you hear a sound (Larsen effect), do the test of the CVR with headset jack 22RK and the parking brake set to OFF. Before you set the parking brake to OFF and start the test, install the wheel chocks or apply the brakes.After you complete the test, set the parking brake back to ON.
| ACTION | RESULT |
|---|---|
| 1.On the overhead panel, on panel 49VU: | |
| |
| 2.Immediately start the STOPWATCH in the cockpit. | |
| 3.On the overhead panel, on panel 21VU: | |
| You can hear a tone in the headset connected to the CVR. |
| There is no tone in the headset. NOTE: The test of relays 45TU and 46TU is satisfactory. |
E. Remove the safety clips and tags and close these circuit breakers in this sequence:
Subtask 23-71-00-865-084-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| FOR FIN: 9DA1 (PROBEPITOT, 1) | |||
| 49VU | ANTI ICE/PROBES/PHC/1 | 2DA1 | D03 |
| FOR FIN: 9DA2 (PROBEPITOT, 2) | |||
| 122VU | ANTI ICE/PROBES/PHC/2 | 2DA2 | Y12 |
| FOR FIN: 9DA3 (PROBEPITOT, 3) | |||
| 122VU | ANTI ICE/PROBES/PHC/3 | 2DA3 | Y16 |
F. Remove the safety clips and tags and close these circuit breakers in this sequence:
5. Close-up| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| FOR FIN: 9DA1 (PROBEPITOT, 1) | |||
| 122VU | ANTI ICE/PROBES/1/TAT | 1DA1 | Z12 |
| 49VU | ANTI ICE/PROBES/PITOT/1 | 3DA1 | D02 |
| 49VU | ANTI ICE/PROBES/AOA/1 | 4DA1 | D04 |
| 122VU | ANTI ICE/PROBES/1/STATIC | 5DA1 | Z13 |
| FOR FIN: 9DA2 (PROBEPITOT, 2) | |||
| 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 |
| FOR FIN: 9DA3 (PROBEPITOT, 3) | |||
| 122VU | ANTI ICE/PROBES/3/PITOT | 3DA3 | Z16 |
| 122VU | ANTI ICE/PROBES/3/AOA | 4DA3 | Z15 |
| 122VU | ANTI ICE/PROBES/3/STATIC | 5DA3 | Z14 |
Subtask 23-71-00-860-090-A ** ON A/C NOT FOR ALL
A. Put the aircraft back to its initial configuration.
(1) Disconnect the headset from the CVR/HEADSET connector.
(2) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
(1) Disconnect the headset from the CVR/HEADSET connector.
(2) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).