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时间:2011-03-20 21:11来源:蓝天飞行翻译 作者:admin
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 The subsequent main modes of operation can be selected by the use of
 menus on the RCU:
 -AUTO MODE The AUTO MODE supplies an automatic cycling of all available pictures.
 -MAP MODE
 The MAP MODE supplies only maps.

 1EFF : 051-099, 1 23-34-00Page 11 1 1 May 01/05 1 1 1CES 1


 System Block Diagram
 Figure 007
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 System Schematic
 Figure 008
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 -INFO MODE The INFO MODE supplies only flight information pages.
 -LOGO MODE The LOGO MODE supplies logos or graphics.
 -TERM MODE The TERM MODE supplies airport terminal charts only.
 A total of 32 modes of operation are available. The airline may select their own logos or other graphics to be shown.
 1EFF : 051-099, 1 23-34-00Page 14 1 1 May 01/05 1 1 1CES 1 PASSENGER INFORMATION SYSTEM - ADJUSTMENT/TEST


______________________________________________
 TASK 23-34-00-710-001
 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 -------------------------------------------------------------------------------
23-36-00-710-001 Operational Test of the Passenger Entertainment (Video) 23-73-00-861-001 Energize the Cabin Intercommunication Data System (CIDS) 23-73-00-862-001 De-energize the Cabin Intercommunication Data System (CIDS) 24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
 from the External Power 31-60-00-860-001 EIS Start Procedure 31-60-00-860-002 EIS Stop Procedure 34-10-00-860-002 ADIRS Start Procedure 34-10-00-860-004 IR Alignment Procedure 34-10-00-860-005 ADIRS Stop Procedure
 3. Job Set-up
__________
 Subtask 23-34-00-860-052
 A. Aircraft Maintenance Configuration
 (1)
 Energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-861-002).


 (2)
 Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) (Ref. TASK 31-60-00-860-001).

 (3)
 Do the ADIRS Start Procedure (Ref. TASK 34-10-00-860-002).


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 (4)
 Make sure that the Cabin Intercommunication Data System (CIDS) is energized (Ref. TASK 23-73-00-861-001).

 (5)
 Make sure that the Passenger Entertainment System (PES) (Video) is energized (Ref. TASK 23-36-00-710-001) and the LCD monitors are extended.


 Subtask 23-34-00-865-050
 B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
 ------------------------------------------------------------------------------PANEL SERVICE IDENT. LOCATION ------------------------------------------------------------------------------121VU AUTO FLT/FMGC/2 10CA2 17 M 121VU ADIRS/ADIRU/2/28VDC 6FP2 05 N 121VU ADIRS/ADIRU/2/115VAC 4FP2 07 N 121VU ADIRS/ADIRU/2/26VAC 5FP2 09 N
 2000VU PES/PVIS 189MH 05 C
 4. Procedure
_________
 Subtask 23-34-00-710-050
 A. Test of the Passenger Visual Information System (PVIS)
 (1) Do this test (without the data from the Flight Management and Guidance Computer (FMGC) and the Air Data/Inertial Reference System (ADIRS)):
 -------------------------------------------------------------------------------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.
2. On the System Control Unit (SCU) 11MH:
 -push the SYST PWR pushbutton switch.
On the LCD of the PVIS Remote ControlUnit (RCU):
-STANDBY is indicated for theinitialization and self-test period.
-
the cursor is set to SET DISPLAY MODEafter the self-test is complete.

On the monitor of the SCU 11MH:

-
the integral light of the SYST PWRpushbutton switch comes on,


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