A320飞机维护手册 AMM 指示/记录系统 3(13)

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R  is triggered through the print button. The report/SAR channel 
R  assignment of the remote print button is GSE programmable. 
R 
R  (h) PCMCIA 
R  The integrated PCMCIA interface contains optional DAR recording 
R  function, store of SAR generated files and store of AIDS standard 
R  reports. Additional it is possible to emulate data loader 
R  function. When using this functions a PCMCIA card must be 
R  inserted in the PCMCIA interface. 
R  - Additional Processor Board 
R  - Access to the incoming data buses 
R  - Access to MCDU, MDDU, Printer and ACARS 
R  **ON A/C 001-049, 051-099, 101-105,
 4. Power Supply____________ 

R 1EFF : 001-049, 051-099, 101-105, 1 31-36-00Page 13 1 1 Config-1 May 01/05 1 1 1CES 1

R  **ON A/C 001-049, 101-105,
 (Ref. Fig. 003)
 The DMU is connected to the 115 V AC bus via the circuit breaker 4TV (AIDS). The maximum of power consumption and the busbar connections are as listed below.
 ----------------------------------------------------------------------------COMPONENT | PWR.CONS. | VOLTAGE | BUSBAR | C/B ----------------------------------------------------------------------------DMU | 40 W | 115 V AC | 202XP NORM | 4TV ----------------------------------------------------------------------------
R  **ON A/C 051-099, 
R R R R R  (Ref. Fig. 003) The DMU is connected to the 115 V AC bus via the circuit breaker 4TV (AIDS). The maximum of power consumption and the busbar connections are as listed below. 
R R R R R  ----------------------------------------------------------------------------COMPONENT | PWR.CONS. | VOLTAGE | BUSBAR | C/B ----------------------------------------------------------------------------DMU | 70 W | 115 V AC | 202XP NORM | 4TV ----------------------------------------------------------------------------
R  **ON A/C 001-049, 051-099, 101-105,
 5. Interface_________
 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 related sources. 

R 1EFF : 001-049, 051-099, 101-105, 1 31-36-00Page 14 1 1 Config-1 May 01/05 1 1 1CES 1

 AIDS - Power Supply
 Figure 003

R 1EFF : 001-049, 051-099, 101-105, 1 31-36-00Page 15 1 1 Config-1 May 01/05 1 1 1CES 1

 B. DMU Input Sources
 (1) The following systems are connected to the DMU:
 (a) Air Conditioning (ATA 21)
 -Pressure Controller (11HL, 12HL)
 -Zone Controller (8HK)
 -Pack Controller (7HH, 27HH)
 (b) 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)

 (c) Communication (ATA23)
 -Aircraft Communications Addressing and Reporting Management Unit (1RB1)
 (d) Flight Controls (ATA 27)
 -Flight Control Data Concentrator (3CE1, 3CE2)
 -Slat and Flap Control Computer (21CV, 22CV)
 (e) Fuel (ATA 28)
 -Fuel Quantity Unit (3QT)
 (f) Indication/Recording (ATA 31)
 -Display Management Computer (1WT1, 1WT2)
 -Flight Warning Computer (1WW1, 1WW2)
 -System Data Aquisition Concentrator (1WV1, 1WV2)
 -Flight Data Interface Unit (2TU)
 (g) Landing Gear (ATA 32)
 -Break System Control Unit 1, 2 (10GG)
 -Landing Gear Control and Interface Unit (5GA1, 5GA2)
 (h) Navigation (ATA 34)
 -Ground Proximity Warning Computer (1WZ)
 -Air Data/inertial Reference Unit (1FP1, 1FP2)
 (i) Pneumatic (ATA 36)
 -Bleed Monitoring Computer (1HA1, 1HA2)
 (j) Onboard Maintenance System (ATA 45)
 -Central Fault Display Interface Unit (1TM1)
 -Printer (2TP)
R 1EFF : 001-049, 051-099, 101-105, 1 31-36-00Page 16 1 1 Config-1 May 01/05 1 1 1CES 1

 (k) Airborne Auxiliary Power (ATA 49)
 -Electronic Control Box (59KD)
 (l) Engine Fuel and Control (ATA 73)
 -Engine Vibration Monitoring Unit (2EV)
 -Electronic Engine Control/Engine Control Unit Eng 1, Eng 2 (4000KS)
R 1EFF : 001-049, 051-099, 101-105, 1 31-36-00Page 17 1 1 Config-1 May 01/05 1 1 1CES 1

 C. Summary of Input/Output Data The connection between the related computers and the DMU is shown in the AIDS Inputs - Schematic. The summary of the input pin assignment is shown:
　
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