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时间:2011-03-25 12:16来源:蓝天飞行翻译 作者:admin
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R 1EFF : 001-049, 051-099, 101-105, 151-158, 1 31-37-21Page 25 1201-209, 1May 01/05 1 1 1CES 1 +----------------------------------------------------------------------+ |Code|Item | |Progr.|Standard | | No.|No. | Description of Function Item |MCDU |Value or | | | | |GSE |Table TXY| |----|------|-----------------------------------------|------|---------| | | | or Pack outlet > 95 C) | | | | | | or | | | |4230|4.2.3 | 8E.1.062.11.14 = 1 | C | | | | | (pack compressor LH outlet temp. > 260 C| | | | | | or Pack outlet > 95 C) | | | | | | or | | | |4240|4.2.4 | 8E.1.062.00.14 = 1 | C | | | | | (pack compressor RH outlet temp. > 260 C| | | | | | or Pack outlet > 95 C) | | | | | | or | | | |4310|4.3.1 | 5C.1.057.01.14 = 1 | | | | | | (excessive cabin altitude warning) | | | | | | | | | | | | It is possible to suppress each logic | | | | | | item individually via the GSE. | | | |----|------|-----------------------------------------|------|---------| | |4.4 | Parameters which are observed for | C | | | | | changes in each line. | | | | | | Limits which are 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 | | | |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 | | | | | PSCW (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 | | |


R 1EFF : 001-049, 051-099, 101-105, 151-158, 1 31-37-21Page 26 1201-209, 1May 01/05 1 1 1CES 1


 +----------------------------------------------------------------------+
 |Code|Item | |Progr.|Standard |
 | No.|No. | Description of Function Item |MCDU |Value or |
 | | | |GSE |Table TXY|
 |----|------|-----------------------------------------|------|---------|
 |5200| | PDC > PDCL in PH 3 to 8 | | |
 | |5.1 | ZCBL = 15000 ft | | |
 | |5.2 | PDCL = 8.5 psi | | |
 |----|------|-----------------------------------------|------|---------|
 |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 |
 +----------------------------------------------------------------------+ 
R  **ON A/C 106-149, 230-299, 303-399, 401-499, 
R  (2) ECS Report Logic <19> 
R  +----------------------------------------------------------------------+ 
R  |Code|Item | |Progr.|Standard | 
R  | No.|No. | Description of Function Item |MCDU |Value or | 
R  | | | |GSE |Table TXY| 
R  |----|------|-----------------------------------------|------|---------| 
R  | |A | Report Format | | | 
R  | |B | Parameter Table | | | 
R  | |C | First three lines of Report | C | Blank | 
R  | |D | Print Out Rules | C | | 
R  | |E | Transfer to ACARS MU | C | Yes | 
R  | |F | Increment of the report counter if the | C | 1 | 
R  | | | report was triggered by a code number | | | 
R  | | | > 1000; 1=yes, 0=no | | | 
R  | |G | 'Y19.1' second pre-events interval | C | 15 | 
R  |----|------|-----------------------------------------|------|---------| 
R  |1000|1 | Manual selection via MCDU | | | 
R  |----|------|-----------------------------------------|------|---------| 
R  |2000|2 | Flight phase dependent manual | | | 
R  | | | selection via remote print button | | | 
R  | | | if programmed. | | | 
R  | |2.1 | Logic algorithm | | | 
R  | |2.2 | Flight Phase | C | not | 
R  | | | | | assigned| 
R  |----|------|-----------------------------------------|------|---------| 
R  |3000|3 | Programmable Start Logic | | | 

R 1EFF : 001-049, 051-099, 101-149, 151-158, 1 31-37-21Page 27 1201-209, 230-299, 303-399, 401-499, 1Aug 01/05 1 1 1CES 1
 
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