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Power Supply Figure 008A
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Power Supply
R Figure 008B
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Power Supply
R Figure 008C
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R **ON A/C 051-099, 106-149, 201-299, 301-399,
5. Interface_________
R **ON A/C 051-099, 201-210,
A. Electrical Interface The data busses of the passenger entertainment digital audio data and passenger service data are input to the SEB 100MK through the connectors J1 and/or J2. These are from the SEB to the SEB cables, that connect one SEB with the other. BITE data results are transmitted back to the MM with the data 1 and 2 lines.
B. Cabin Intercommunication Data System Interface The CIDS interface is described in the component description (Para. 6B(2)).
C. Electrical Components Interface The electrical components interface is described in the component description (Para. 6E(1)).
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A. System Interfaces
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(Ref. Fig. 003A)
**ON A/C 301-399,
(Ref. Fig. 003B)
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The PES Music has interfaces with: - 23-32-00 - Announcement - Music Tape Reproducer System - 23-36-00 - Passenger Entertainment System Video (PES Video) - 23-73-00 - Cabin Intercommunication Data System (CIDS)
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6. Component Description_____________________
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A. Audio Reproducer The CD reproducer 10MK has four CD drives. Each CD drive drives one CD. Each CD drive provides four monophonic or two stereophonic channels. The CD reproducer has a total of sixteen output channels.
B. Main Multiplexer (Ref. Fig. 007) The Main Multiplexer (MM) 8MK is mechanically assembled in an ARINC 600 standard from factor 2MCU. The connector is ARINC 600 size 1. The MPES has a minimum of eighteen audio input channels. Up to six channels can be used for video tape reproducer inputs. The MPES permits a bilingual movie in each of the aircraft zones (up to three zones).
(1) Boarding Music Four channel nummbers can be used to provide the boarding music. The flight attendants control the boarding music on the Forward Attendant Panel (FAP).
(2) Passenger Address Audio
R **ON A/C 051-099,
(Ref. Fig. 005)
R **ON A/C 201-210,
R (Ref. Fig. 005A)
R **ON A/C 051-099, 201-210,
Three Passenger Address (PA) audio-inputs control all the MPES channels in each applicable aircraft zone. The CIDS controls the MPES mode and permits the use of the PA in each zone of the aircraft. The aircraft seat layout will have an effect on this system.
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(3)
Cabin Intercommunication Data System (CIDS) Interface (Ref. Fig. 002,005) The ARINC 429 input databus receives data from the CIDS directors. The ARINC 429 output databus sends data to the CIDS directors. In the Fig. 002 the CIDS has different functional interfaces. These are :
-Power ON/OFF,
-Built-In Test Equipment (BITE) information initialization and data transfer,
-PA announcement control and seat layout data transfer to the MPES.
(4)
ARINC 429 Output Data Port The MPES output data has a BITE fault data. The CIDS directors send this data to the Center Fault Display System (CFDS) and to the Programming and Test Panel (PTP) through the CIDS.
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