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 Config-2 Aug 01/02

 +----------------------------------------------------------------------+ |Code|Item | |Progr.|Standard | | No.|No. | Description of Function Item |MCDU |Value or | | | | |GSE |Table TXY| |----|------|-----------------------------------------|------|---------| | | | | | | | |5.8 | ROLL ANGLE 04.1.325.01 degr. | AI | T24/T25 | | | | 04.2.325.10 | | | | |5.8.1 | WA of ROLL ANGLE | C | T24/T25 | | | | | | | | |5.9 | TAT 06.1.211.01 C | AI | T24/T25 | | | | 06.2.211.10 | | | | |5.9.1 | WA of TAT | C | T24/T25 | | | | | | | | |5.10 | N2 7C.1.344.01 Eng.1 % | AI | T24/T25 | | | | 7C.2.344.10 Eng.2 | | | | |5.10.1| WA of N2 | C | T24/T25 | | | | | | | | |5.11 | EGT 7C.1.345.01 Eng.1 C | AI | T24/T25 | | | | 7C.2.345.10 Eng 2 | | | | |5.11.1| WA of EGT | C | T24/T25 | | | | | | | | |5.12 | VACC 04.1.364.01 g | AI | T24/T25 | | | | 04.2.364.10 | | | | |5.12.1| WA of VACC | C | T24/T25 | | | | | | | | |5.13 | MN 06.1.205.01 Mach | AI | T24/T25 | | | | 06.2.205.10 | | | | |5.13.1| WA of MN | C | T24/T25 | | | | | | | | |5.14 | N1 7C.1.346.01 Eng.1 % | AI | T24/T25 | | | | 7C.2.346.10 Eng.2 | | | | |5.14.1| WA of N1 | C | T24/T25 | | | | | | | | |5.15 | PT2 7C.1.131.91 Eng.1 psia | AI | T24/T25 | | | | 7C.2.131.10 Eng.2 | | | | |5.15.1| WA of PT2 | C | T24/T25 | | | | | | | | |5.16 | FF 7C.1.244.01 Eng.1 kg/h | AI | T24/T25 | | | | 7C.2.244.10 Eng.2 | | | | |5.16.1| WA of FF | C | T24/T25 | | | | | | | | |5.17 | EPR 7C.1.340.01 Eng.1 % | AI | T24/T25 | | | | 7C.2.340.10 Eng.2 | | | | |5.17.1| WA of EPR | C | T24/T25 | |----|------|-----------------------------------------|------|---------| |8100|8.1 | ACARS MU uplink request with IMI .REQ02.| | |
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 Config-2 Aug 01/02  +----------------------------------------------------------------------+ |Code|Item | |Progr.|Standard | | No.|No. | Description of Function Item |MCDU |Value or | | | | |GSE |Table TXY| |----|------|-----------------------------------------|------|---------| | | | The report <02> is immediately generated| | | | | | and transmitted to the ACARS MU. | | | |----|------|-----------------------------------------|------|---------| |8200|8.2 | ACARS MU uplink request with IMI .G02. | | | | | | The report <02> is generated as soon as | | | | | | stable frame criteria are met, i.e. the | | | | | | DMU is immediately start searching for | | | | | | stable frame criteria independing from | | | | | | any other logic. | | | |----------------------------------------------------------------------| | AI = Programmable by Airbus Industrie | | C = Programmable by Customer | +----------------------------------------------------------------------+

 M. Engine Take-Off Report <04> (Ref. Fig. 013, 014) The Engine Take-Off Report is an average data collection of aircraft and engine around the point of peak N1 while in take-off flight phase. The engine take-off report, is generated when one of the logic conditions 1000 to 5009 (for details see engine take-off report logic) is present. Each Take-Off Report is contain a T/O delta N1 respective EPR summary.
　
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本文鏈接地址：getting to grips with aircraft performance monitoring(90)