Operational Test of the Passenger Visual Information-System

TASK 23-34-00-710-001-A
Operational Test of the Passenger Visual Information-System

1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Referenced Information

REFERENCE	DESIGNATION
TASK 23-36-00-710-001-A	Operational Test of the Passenger Entertainment (Video)
TASK 23-73-00-861-001-A	Energize the Cabin Intercommunication Data System (CIDS)
TASK 23-73-00-862-001-A	De-energize the Cabin Intercommunication Data System (CIDS)
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 31-60-00-860-001-A	EIS Start Procedure
TASK 31-60-00-860-002-A	EIS Stop Procedure
TASK 34-10-00-860-002-A	ADIRS Start Procedure
TASK 34-10-00-860-004-A	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

3. Job Set-up
Subtask 23-34-00-860-052-F ** 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 EIS start procedure (upper ECAM DU and lower ECAM DU only)
(Ref. AMM TASK 31-60-00-860-001).
(3) Do the ADIRS Start Procedure (Ref. AMM TASK 34-10-00-860-002).
(4) Do the IR Alignment Procedure (Ref. AMM TASK 34-10-00-860-004).

NOTE: For the alignment procedure, make sure that the correct values for the longitude and latitude of the A/C position are shown.

NOTE: During the alignment procedure, make sure that a point of departure and a destination (airport identification) are put in on the MCDU. The point of departure must be where the A/C location is now.

(5) Make sure that the Cabin Intercommunication Data System (CIDS) is energized (Ref. AMM TASK 23-73-00-861-001).
(6) Make sure that the Passenger Entertainment System (PES) (Video) is energized (Ref. AMM TASK 23-36-00-710-001).
(7) Make sure that the CD-ROM DIU (190MH1) is in the Digital Interface Unit (DIU) (190MH).

Subtask 23-34-00-865-077-A ** ON A/C NOT FOR ALL

B. Make sure that this(these) circuit breaker(s) is(are) closed:

PANEL	DESIGNATION	FIN	LOCATION
** ON A/C NOT FOR ALL
49VU	AUTO FLT/FCU/1	9CA1	B05
49VU	AUTO FLT/FMGC/1	10CA1	B02
121VU	AUTO FLT/FCU/2	9CA2	M21
121VU	AUTO FLT/FMGC/2	10CA2	M17
121VU	ADIRS/ADIRU/2/26VAC AND AOA	5FP2	N08
121VU	ADIRS/ADIRU/2/115VAC	4FP2	N06
121VU	ADIRS/ADIRU/2/28VDC	6FP2	N04
2000VU	PES PFIS	189MH	C07
2000VU	PES-VIDEO-CABIN-RH AFT	25MH	C06
2000VU	PES-VIDEO-CABIN-LH	23MH	C05
2000VU	PES-VIDEO-CABIN-RH FWD	24MH	C04
2000VU	PES-VIDEO-CABIN-LH FWD	22MH	C03
2000VU	PES-VIDEO-CONTROL-VCC	21MH	C02
2000VU	PES-VIDEO-CONTROL-MAIN	20MH	C01

4. Procedure
Subtask 23-34-00-710-051-N ** ON A/C NOT FOR ALL

A. Test of the Passenger Visual Information System (PVIS)
(1) Do this test.

ACTION	RESULT
1.On the circuit breaker panel 2000VU:
remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 189MH (C 7), PES/PVIS.	The PVIS energizes.
2.On the PES video System Control Unit (SCU) 11MH:	On the PES video SCU 11MH:
push the pushbutton switch MASTER POWER.	all LED come on while the SCU 11MH does the self test of the system, the green LED PASS comes on at the end of the self test.
	On the SCU 11MH, on the monitor: the AUTO MODE page comes into view.
3.On the SCU 11MH, on the MODE SELECT area:	On the SCU 11MH, on the monitor:
push the pushbutton switch again and again until the LED ALL ZONES comes on	the ALL ZONES MODE page comes into view,
On the SCU 11MH:
push the pushbutton switch MENU again and again until the BCS/AIRSHOW/PRAM page on the monitor,	the BCS/AIRSHOW/PRAM page comes into view,
push the arrow up or arrow down membrane switches and select the line AIRSHOW,
push the ENTER membrane switch,	the AIRSHOW MENU comes into view,
push the arrow up or arrow down membrane switches and select the line SET DISPLAY MODE,
push the ENTER membrane switch,	the SET DISPLAY MODE page comes into view,
push the arrow up or arrow down membrane switches and select the line TEST resp. AUTO,
push the ENTER membrane switch.	a new SET DISPLAY MODE page comes into view.
4.On the SCU 11MH:	On the SCU 11MH:
push the PREVIEW SELECT switch.	monitor the MANUAL CONTROL board of the SCU for the indicators of AUX and PRI to be on and the digital display to show 7.
5.On the SCU 11MH, the MANUAL CONTROL board, ALL ZONES:	On the SCU 11MH, the MANUAL CONTROL board, ALL ZONES:
push the SOURCE/SEL switch for selection, if necessary again and again.	the AUX and PRI indicators come on and the digital display shows 7.
6.On the SCU 11MH, the MANUAL CONTROL board, ALL ZONES:	On the SCU 11MH, the MANUAL CONTROL board, ALL ZONES:
push the ON/OFF/PWR switch.	the related LED of the PWR switch comes on.
	On the SCU 11MH, on the monitor the airshow information comes into view.
	In the cabin: all Hatrack Mounted Display Units 100MH (HMDU) move out of the hatrack.
	In the cabin, on all HMDU 100MH the airshow information comes into view.
7.On the circuit breaker panel 2000VU:
open, safety and tag this(these) circuit breaker(s): 189MH (C 7), PES/PVIS.	The PVIS is de-energized.
	In the cabin: the HMDU 100MH do not show PVIS information.
8.On the SCU 11MH:
push the pushbutton switch MASTER POWER	In the cabin: all HMDU 100MH move up into the hatracks.

5. Close-up
Subtask 23-34-00-860-053-C ** ON A/C NOT FOR ALL

A. Put the aircraft back to its initial configuration.
(1) De-energize the Cabin Intercommunication Data System (CIDS) (Ref. AMM TASK 23-73-00-862-001).
(2) Do the ADIRS stop procedure (Ref. AMM TASK 34-10-00-860-005).
(3) Do the EIS stop procedure
(Ref. AMM TASK 31-60-00-860-002).
(4) Make sure that the work area is clean and clear of tools and other items.
(5) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).

[Rev.10 from 2021] 2026.04.02 06:50:36 UTC