| TP | 11E | 11F | ARINC 429 | | X | CFDIU, MCDU 1, | OUT A |
| | | | | | | MCDU 2, PRINTER | |
| | | | | | | | |
| MP | 11J | 11K | ARINC 429 | | X | ACARS | OUT B |
| | | | | | | | |
| TP | 11C | 11D | ARINC 429 | X | | MDDU | OUT C |
| | | | | | | | |
| TP | 11G | 11H | ARINC 429 | | X | RESERVED | OUT D |
| | | | | | | | |
| TP | 13A | 13B | HARVARD | | | DAR RECORD DATA | |
| | | | BI-PHASE | | | | |
| | | | | | | | |
| TP | 15A | 15B | SPECIAL | | | DAR SYNC SIGNAL | |
| | | | | | | | |
| TP | 12A | 12B | RS 422 | | | RESERVED FOR | |
| | | | | | | DAR CONTROL OUT | |
-------------------------------------------------------------------------------FDIMU (DMU-part) Bus Outputs - Table 1
R 1EFF : 106-149, 211-299, 301-399, 401-499, 1 31-36-00Page 21 1 1 Config-2 Aug 01/05 1 1 1CES 1
-------------------------------------------------------------------------------
| CONNECTOR | PIN | TYPE | SPEED | SOURCE | PORT NO | | | HI | LO | | HI | LO | LRU / SYSTEM | | |---------------------------------------------------------------------------- | | MP | 5C | 5D | ARINC 429 | | X | CFDIU | IN-A | | | | | | | | | | | MP | 5J | 5K | ARINC 429 | | X | ACARS | IN-B | | | | | | | | | | | MP | 11C | 11D | ARINC 429 | X | | MDDU | IN-C | | | | | | | | | | | MP | 11A | 11B | ARINC 429 | | X | MCDU 2 | IN-E | | | | | | | | | | | TP | 11A | 11B | ARINC 429 | | X | MCDU 1 | IN-F | | | | | | | | | | | TP | 11J | 11K | ARINC 429 | | X | PRINTER | IN-H | | | | | | | | | | | MP | 12A | 12B | RS 422 | | | DAR CONTROL IN | | -------------------------------------------------------------------------------
FDIMU (DMU-Part) Bus Inputs - Table 2
**ON A/C 151-199, 201-210,
A. Architecture of Inputs The DMU is connected to various source systems to collect the whole parameter set. The block diagram of input sources (Ref. 31-37-00) shows the connection of the DMU to the respective sources.
B. DMU Input Sources
The following systems are connected to the DMU:
-Air Conditioning (ATA 21)
-Pressure Controller (11HL, 12HL)
-Zone Controller (8HK)
-Pack Controller (7HH, 27HH).
-Auto Flight (ATA 22)
-Multipurpose Control and Display Unit (3CA1, 3CA2)
-
Flight Control Unit (2CA)
-
Flight Augmentation Computer (1CC1, 1CC2)
-
Flight Management, Guidance and Envelope Computer (1CA1, 1CA2).
-Communication (ATA23)
-Aircraft Communications Addressing and Reporting Management Unit (1RB1).
-
Flight Controls (ATA 27)
-
Flight Control Data Concentrator (3CE1, 3CE2)
-Slat and Flap Control Computer (21CV, 22CV).
-Fuel (ATA 28)
R 1EFF : 106-149, 151-199, 201-299, 301-399, 1 31-36-00Page 22 1401-499, 1Config-2 Aug 01/05 1 1 1CES 1
R - Fuel Quantity Unit (3QT).
R - Indication/Recording (ATA 31)
R - Display Management Computer (1WT1, 1WT2)
R - Flight Warning Computer (1WW1, 1WW2)
R - System Data Aquisition Concentrator (1WV1, 1WV2)
R - Flight Data Interface Unit (2TU).
R - Landing Gear (ATA 32)
R - Break System Control Unit 1, 2 (10GG)
R - Landing Gear Control and Interface Unit (5GA1, 5GA2).
R - Navigation (ATA 34)
R - Ground Proximity Warning Computer (1WZ)
R - Air Data/inertial Reference Unit (1FP1, 1FP2)
R - Pneumatic (ATA 36)
R - Bleed Monitoring Computer (1HA1, 1HA2).
R - Onboard Maintenance System (ATA 45)
R - Central Fault Display Interface Unit (1TM1)
R - Printer (2TP).
R - Airborne Auxiliary Power (ATA 49)
R - Electronic Control Box (59KD).
R - Engine Fuel and Control (ATA 73)
R - Engine Vibration Monitoring Unit (2EV)
R - Electronic Engine Control/Engine Control Unit Eng 1, Eng 2 (4000KS).
R C. Summary of Input/Output Data
R
R The connection between the related computers and the DMU is shown in the
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