R 1EFF : 001-049, 051-099, 101-105, 1 31-36-00Page 2 1 1 Config-1 May 01/05 1 1 1CES 1
-------------------------------------------------------------------------------FIN | FUNCTIONAL DESIGNATION | PANEL|ZONE|ACCESS | ATA
| | | | DOOR | REF. ______________________________________________________________________________ 1TV DMU 87VU 127 824 31-36-34 1TV1 DMU System Software Disk 31-36-00 1TV2 DMU Setup Database Disk 31-36-00
The DMU is installed in the electronics rack, the Remote Print Button is
installed on the pedestal of the cockpit.
For component location of equipment which is not part of circuit TV see
respective ATA chapter:
ATA 22-82 AFL - CONTROL AND DISP. UNIT for CA
ATA 23-24 COM - AIRCRAFT COMMUNICATION for RB
ATA 31-32 IND - CENTRALIZED FAULT DISP for TW
ATA 31-33 IND - FLIGHT DATA RECORDING for TU
ATA 31-35 IND - MULTIFUNCTION PRINTER for TW
3. System Description
__________________
R **ON A/C 001-049, 101-105,
(Ref. Fig. 002)
The AIDS mainly consists of the Data Management Unit (DMU) and an optional
Digital AIDS Recorder (DAR). The DMU is the central part of the AIDS and is
reconfigurable via the Ground Support Equipment (GSE).
The DMU is a high-performance avionic computer specialized for the
acquisition of ARINC 429 DITS data and associated processing. The multi
tasking architecture allows processing of the various tasks in real time.
An integral part of the DMU is the optional Smart Access Recorder (SAR).
This function is based on a nonvolatile Solid State Mass Memory (SSMM)
module which is used to store flight data. Sophisticated data compression
algorithms ensure efficient usage of the limited capacity of the SSMM.
A. System Architecture
(1)
Hardware
-a Data Management Unit (DMU)
-
an Digital AIDS Recorder (DAR) (option)
-
an in the DMU integrated Smart Access Recorder (SAR)
(2)
Software
-Boot Software
-
DMU Operational Software
-
DMU Database Software
R 1EFF : 001-049, 051-099, 101-105, 1 31-36-00Page 3 1 1 Config-1 May 01/05 1 1 1CES 1 Component Location Figure 001 (SHEET 1)
R 1EFF : 001-049, 101-105, 1 31-36-00Page 4 1 1 Config-1 May 01/05 1 1 1CES 1 Component Location Figure 001 (SHEET 2)
R 1EFF : 001-049, 101-105, 1 31-36-00Page 5 1 1 Config-1 May 01/05 1 1 1CES 1R Component Location R Figure 001A (SHEET 1)
R 1EFF : 051-099, 1 31-36-00Page 6 1 1 Config-1 May 01/05 1 1 1CES 1R Component Location R Figure 001A (SHEET 2)
R 1EFF : 051-099, 1 31-36-00Page 7 1 1 Config-1 May 01/05 1 1 1CES 1
System Block Diagram
Figure 002
R 1EFF : 001-049, 051-099, 101-105, 1 31-36-00Page 8 1 1 Config-1 May 01/05 1 1 1CES 1
(3) Generic function of the DMU One of the generic functions of the DMU is the generation of reports as a result of specific events defined by trigger conditions.
The following AIDS standard reports are defined:
-Engine Cruise Report <01> (Ref. 31-37-73)
-Cruise Performance Report <02> (Ref. 31-37-73)
-
Engine Take-Off Report <04> (Ref. 31-37-73)
-
Engine Report O/R <05> (Ref. 31-37-73)
-
Engine Gas Path Adsvisory Report <06> (Ref. 31-37-73)
-
Engine Mechanical Advisory Report <07> (Ref. 31-37-73)
-
Engine Divergence Report <09> (Ref. 31-37-73)
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:A320飞机维护手册 AMM 指示/记录系统 3(10)