Operational Check of CVR and CVR-Channel Recording
TASK 23-71-00-710-001-A
Operational Check of CVR and CVR-Channel Recording
Refer to the MPD TASK: 237100-01
OPERATIONAL CHECK OF CVR AND CVR-CHANNEL RECORDING
To do a check of the operation of the CVR.
To do a check of the recording of the communications from the CAPT, F/O and third occupant stations and the CVR microphone.
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 23-71-00-860-051-A
Subtask 23-71-00-710-050-A ** ON A/C NOT FOR ALL
Subtask 23-71-00-860-050-A
[Rev.10 from 2021]
2026.04.01 05:29:56 UTC
Operational Check of CVR and CVR-Channel Recording
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 Cockpit Voice Recorder (CVR) and the Solid State Cockpit Voice Recorder (SSCVR).
NOTE: For this procedure, you must make sure that the PARK BRK control handle is in the ON position (accumulator pressure pointer on the triple indicator is in the green range).
ZONE: 210
1. Reason for the JobRefer to the MPD TASK: 237100-01
OPERATIONAL CHECK OF CVR AND CVR-CHANNEL RECORDING
To do a check of the operation of the CVR.
To do a check of the recording of the communications from the CAPT, F/O and third occupant stations and the CVR microphone.
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | 1 | HEADSET 600 OHMS |
| No specific | 1 | MICROPHONE 150 OHMS - HAND |
| 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 23-71-00-860-051-A
A. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) On the Audio Control Panels (ACP) of the CAPT, F/O and third occupant stations, make sure that:
(4) Make sure that the PARK BRK control handle is in the ON position.
(5) Make sure that the aircraft is in the ground configuration.
(6) Make sure that the engine shutdown occurred five minutes or more before you do this procedure.
(7) On maintenance panel 50VU, connect the HEADSET 600 OHMS to the CVR/HEADSET connector.
(8) Connect the MICROPHONE 150 OHMS - HAND to the HAND MIC connectors of the CAPT, F/O and third occupant stations.
Subtask 23-71-00-865-050-A (1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) On the Audio Control Panels (ACP) of the CAPT, F/O and third occupant stations, make sure that:
- The INT/RAD selector switch is in the neutral position.
- The green lines of all the transmission keys are off.
- All the reception pushbutton switches are pushed (no reception).
(4) Make sure that the PARK BRK control handle is in the ON position.
(5) Make sure that the aircraft is in the ground configuration.
(6) Make sure that the engine shutdown occurred five minutes or more before you do this procedure.
(7) On maintenance panel 50VU, connect the HEADSET 600 OHMS to the CVR/HEADSET connector.
(8) Connect the MICROPHONE 150 OHMS - HAND to the HAND MIC connectors of the CAPT, F/O and third occupant stations.
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 | |||
| 49VU | RCDR1 CVR&FDR | 40TU | E14 |
| 49VU | RCDR CTL | 41TU | E13 |
Subtask 23-71-00-710-050-A ** ON A/C NOT FOR ALL
A. Test of the CVR
Before you set the parking brake to the OFF position, make sure that the wheel chocks are installed on the MLG wheels.
After the test of the CVR, make sure that you set the parking brake back to the ON position.
Subtask 23-71-00-710-050-D ** ON A/C NOT FOR ALL NOTE: You can use the HEADSET 600 OHMS with the jack (22RK) as an alternative to the cockpit loudspeakers.
NOTE: Before this test, you can hear the frequency shift keying-signal that gives an audio signal at intervals of four seconds. The Flight Data Interface Unit (FDIU) (or Flight Data Interface and Management Unit (FDIMU)) gives this frequency shift keying-signal for the synchronization of the SSCVR clock with the Solid State Flight Data Recorder (SSFDR). This audio signal operates independently from the test of the CVR.
NOTE: During the test, if there is an acoustic feedback (Larsen effect), we recommend that you do the test of the CVR with the 22RK jack headset.
For this test, make sure that the PARK BRK control switch (on RUD TRIM/PARKING BRK panel 110VU) is in the OFF position.Before you set the parking brake to the OFF position, make sure that the wheel chocks are installed on the MLG wheels.
After the test of the CVR, make sure that you set the parking brake back to the ON position.
NOTE: If no headset is available on the aircraft, to decrease the Larsen effect you can put your hand on the cockpit microphone.
| ACTION | RESULT |
|---|---|
1.On overhead control and indicating panel 21VU:
| On the RCDR/GND CTL pushbutton switch:
|
| 2.Speak in the cockpit. | You can hear your voice from the CVR microphone in the headset connected to the 22RK jack. |
3.On overhead control and indicating panel 21VU:
| At the CAPT and F/O stations:
NOTE: At the F/O station only, there can be an acoustic interference during the test, but this does not make the removal of the CVR necessary. |
4.On overhead control and indicating panel 21VU:
|
|
5.On overhead control and indicating panel 21VU:
| On the RCDR/GND CTL pushbutton switch:
|
A. Test of the CVR
Before you set the parking brake to the OFF position, make sure that the wheel chocks are installed on the MLG wheels.
After the test of the CVR, make sure that you set the parking brake back to the ON position.
Subtask 23-71-00-710-055-B NOTE: You can use the HEADSET 600 OHMS with the jack (22RK) as an alternative to the cockpit loudspeakers.
NOTE: Before this test, you can hear the frequency shift keying-signal that gives an audio signal at intervals of four seconds. The Flight Data Interface Unit (FDIU) (or Flight Data Interface and Management Unit (FDIMU)) gives this frequency shift keying-signal the synchronization of the SSCVR clock with the Solid State Flight Data Recorder (SSFDR). This audio signal operates independently from the test of the CVR.
NOTE: During the test, if there is an acoustic feedback (Larsen effect), we recommend that you do the test of the CVR with the 22RK jack headset.
For this test, make sure that the PARK BRK control switch (on RUD TRIM/PARKING BRK panel 110VU) is in the OFF position.Before you set the parking brake to the OFF position, make sure that the wheel chocks are installed on the MLG wheels.
After the test of the CVR, make sure that you set the parking brake back to the ON position.
NOTE: If no headset is available on the aircraft, to decrease the Larsen effect you can put your hand on the cockpit microphone.
NOTE: During the test, you can hear your voice from the headset or from the cockpit loudspeakers.
| ACTION | RESULT |
|---|---|
1.On overhead control and indicating panel 21VU:
| On the RCDR/GND CTL pushbutton switch:
|
| 2.Speak in the cockpit. | You can hear your voice from the CVR microphone in the headset connected to the 22RK jack. |
3.On overhead control and indicating panel 21VU:
| At the CAPT (F/O or third occupant) station:
NOTE: At the F/O station only, there can be an acoustic interference during the test, but this does not make the removal of the CVR necessary. |
4.On overhead control and indicating panel 21VU:
|
|
5.On overhead control and indicating panel 21VU:
| On the RCDR/GND CTL pushbutton switch:
|
B. Test of the CVR Channel Recording with the Hot-Mike Function
This procedure is applicable to the CVR supplied with 115VAC or 28VDC.
For this procedure:
5. Close-upThis procedure is applicable to the CVR supplied with 115VAC or 28VDC.
For this procedure:
- Make sure that all the boomsets are disconnected.
- Use only the HEADSET 600 OHMS on maintenance panel 50VU.
- Make sure that the INT/RAD selector switch is set to the neutral position.
NOTE: This test is applicable to the CAPT station. To do this test on the other stations, you can use the indications between the parentheses.
| ACTION | RESULT |
|---|---|
1.On overhead control and indicating panel 21VU:
| On the RCDR/GND CTL pushbutton switch:
|
| 2.Speak in the cockpit. | You can hear your voice from the CVR microphone in the CVR headset. |
| 3.Put a cover on the CVR microphone. | |
| You cannot hear your voice from the CVR microphone in the CVR headset. |
4.On the CAPT (F/O or third occupant) ACP:
| |
5.On the CAPT (F/O or third occupant) station:
| |
| You can hear your voice from the hand microphone in the CVR headset. |
6.On the CAPT (F/O or third occupant) station:
| |
| |
| 7.Remove the cover from the CVR microphone. | |
8.On overhead control and indicating panel 21VU:
| On the RCDR/GND CTL pushbutton switch:
|
Subtask 23-71-00-860-050-A
A. Put the aircraft back to its initial configuration.
(1) On the ACPs of the CAPT, F/O and third occupant stations, make sure that:
(Ref. AMM TASK 24-41-00-862-002).
(1) On the ACPs of the CAPT, F/O and third occupant stations, make sure that:
- The INT/RAD selector switch is in the neutral position.
- The green lines of all the transmission keys are off.
- All the reception pushbutton switches are pushed (no reception).
(Ref. AMM TASK 24-41-00-862-002).