| |4.4 | Parameters which are observed for | C | |
| | | changes in each line. | | |
| | | Limits which cause a print out of one | | |
| | | line when exceeded: | | |
| | | Parameter Limit | | |
| |4.4.1 | N1 (7C.1.346.01) +/- 1% | C | |
| |4.4.2 | (7C.2.346.10) | C | |
| |4.4.3 | PBV (8E.1.112.11) +/- 2.5% | C | |
| |4.4.4 | (8E.2.112.00) | C | |
| |4.4.5 | PF (8E.1.126.11) +/- 0.1kg/sec | C | |
| |4.4.6 | (8E.2.126.00) | C | |
| |4.4.7 | P3 (7C.1.264.01) +/- 20 psia | C | |
1EFF : 159-199, 210-229, 301-302, 1 31-37-21Page 31 1 1 Aug 01/05 1 1 1CES 1 +----------------------------------------------------------------------+ |Code|Item | |Progr.|Standard | | No.|No. | Description of Function Item |MCDU |Value or | | | | |GSE |Table TXY| |----|------|-----------------------------------------|------|---------| | |4.4.8 | (7C.2.264.10) | C | | | |4.4.9 | T3 (7C.1.265.01) +/- 20 C | C | | | |4.4.10| (7C.2.265.10) | C | | | |4.4.11| ALT (06.1.203.01) +/- 300ft | C | | | | | (06.2.203.10) | | | | |4.4.12| TAT (06.1.211.01) +/- 5 C | C | | | |4.4.13| ZCB (5C.1.151.01) +/- 100 ft | C | | | | | PCSW (5C.1.057.01) change of one bit | | | | |4.4.14| PDC (5C.1.144.01) +/- 0.1 psi | C | | |----|------|-----------------------------------------|------|---------| | |5 | Report is generated if one of the limits| | | | | | described as follows is exceeded: | | | | | | | | | |5100| | ZCB > ZCBL in PH 1.1 to 10 | | | |5200| | PDC > PDCL in PH 3 to 8 | | | | |5.1 | ZCBL = 15000 ft | C | | | |5.2 | PDCL = 8.5 psi | C | | |----|------|-----------------------------------------|------|---------| |8100|8.1 | ACARS MU uplink request with IMI 'REQ19'| | | | | | The report <19> is immediately generated| | | | | | and transmitted to the ACARS MU. | | | |----------------------------------------------------------------------| | AI = Programmable by Airbus Industrie | | C = Programmable by Customer | +----------------------------------------------------------------------+
1EFF : 159-199, 210-229, 301-302, 1 31-37-21Page 32 1 1 Aug 01/05 1 1 1CES 1 AIDS - APU REPORTS - DESCRIPTION AND OPERATION
______________________________________________
1. General
_______ The AIDS Reports are results of the related AIDS monitored aircraft systems (refer to the list below for the list of reports which are available). The reports can be requested manually or are started automatically. The monitor functions have fixed trigger mechanisms, fixed data collection and output formatting. Collected monitored-aircraft-data is automatically supplied to the related systems during unusual aircraft operation. If a report is requested manually with the remote print button, it is generated immediately (independently of any other start logic). The manually or automatically generated reports (stored in the SSMM) can be transferred to the printer and/or the MDDU, and/or the ACARS and/or the DAR/SAR. Some parameters for customer requirements are re-programmable through the MCDU or by GSE (For more information refer to 31-36-00). The following APU AIDS Reports are available:
-<13> APU MES/TDLE Report,
-<14> APU Shutdown Report.
2. Reports
_______
A. APU MES/IDLE Report <13> (Ref. Fig. 001) The APU MES/IDLE Report is an averange collection of APU related parameters during the starting of each main engine as well as during APU idle conditions. This information will be primarily used by ground APU performance analysis program. The report is generated when one of the logic conditions 1000 to 4000 (for details see the APU MES/IDLE Report logic) is present.
R **ON A/C 001-049, 051-099, 101-105, 151-158, 201-209,
(1) APU MES/IDLE Report Data Field Description
+---------------------------------------------------------------------+ | Value | Content Description | |--------------|------------------------------------------------------| | ASN | APU Serial Number | | 9999 | (0 to 9999) | | | param. 7A.1.050.01 | |--------------|------------------------------------------------------| | AHRS | APU Operating Hours | | 99999 | (0 to 99999) | | | param. 0D.1.110.00 | |--------------|------------------------------------------------------| | ACYC | APU Start Cycles |
1EFF : ALL 1 31-37-49Page 1 1 1 May 01/05 1 1 1CES 1
APU MES/IDLE Report <13>
Figure 001
1EFF : ALL 1 31-37-49 Page 2
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