A320飞机维护手册 AMM 指示/记录系统 5(30)

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R 1EFF : 001-049, 051-099, 101-105, 151-158, 1 31-37-73Page A0 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| |----|------|-----------------------------------------|------|---------| | | | ing flight phase 4. | | | | | | | | | | |4.1 | The report is postponed to the next | | | | | | flight leg is at least one of the EGT | | | | | | values on Eng.1 or Eng.2 is below EGTL | | | | | | at the moment when the starter air valve| | | | | | switched from closed position to open | | | | | | position at engine start. | | | | | | Starter Air Valve open: | | | | | | Eng.1 param. 7C.1.270.01.13 = 1 | | | | | | Eng.2 param. 7C.2.270.10.13 = 1 | | | | | | | | | | | | or | | | | | | | | | | | | if the Wing Anti-Ice Status or the Na-| | | | | | celle Anti-Ice Status is switched during| | | | | | the search time period. | | | | | | | | | | | | Wing Anti-Ice Valve closed: | | | | | | param. 29.1.001.00.18 = 0 right hand | | | | | | 29.2.001.00.18 = 0 right hand | | | | | | param. 29.1.001.11.18 = 0 left hand | | | | | | 29.2.001.11.18 = 0 left hand | | | | | | Nacelle Anti-Ice Valve closed: | | | | | | Eng.1 param. 5D.2.061.10.28 = 0 | | | | | | Eng.2 param. 5D.2.061.10.27 = 0 | | | |----|------|-----------------------------------------|------|---------| |4100|4.1.1 | The same rules as desribed for Log. No. | C | disarmed| | | | 4000 is valid and in addition the report| | | | | | is postponed when the Wing Anti-Ice | | | | | | Status or Nacelle Anti-Ice Status is | | | | | | open during the search time period. This| | | | | | trigger condition is basically disarmend| | | | | | and can be armed via a GSE programmable.| | | | | | | | | | |4.2 | The report trigger logic is restarted in| | | | | | flight leg 'F04+n' (n=1, 2, ..F04) after| | | | | | no report generation in the previous leg| | | | | | 'F04+ (n-1)'. | | | | | | | | | | |4.3 | EGTL = EGT + TAT | C | T22/T23 | | | | | | |

R 1EFF : 001-049, 051-099, 101-105, 151-158, 1 31-37-73Page A1 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| |----|------|-----------------------------------------|------|---------| | |4.4 | 'F04' Take Off | C | T22/T23 | | | | | | | | |4.5 | 'Y04.1' seconds after PH 4 entry | C | T22/T23 | | | | | | | | |4.6 | T/O delta N1 summary limits | | | | | | delta N1 = N1MX - N1 | | | | | | N1MX = 7C.1.342.01 Eng.1 | | | | | | 7C.2.342.10 Eng.2 | | | | | | N1 = 7C.1.346.01 Eng.1 | | | | | | 7C.2.346.10 Eng.2 | | | | | | | | | | |4.7.1 | delta N1 > 10 % rpm | C | T22/T23 | | |4.7.2 | delta N1 > 8 % rpm and =/< 10 % rpm | C | T22/T23 | | |4.7.3 | delta N1 > 6 % rpm and =/< 8 % rpm | C | T22/T23 | | |4.7.4 | delta N1 > 4 % rpm and =/< 6 % rpm | C | T22/T23 | | |4.7.5 | delta N1 > 2 % rpm and =/< 4 % rpm | C | T22/T23 | | |4.7.6 | delta N1 > 0.2 % rpm and =/< 2 % rpm | C | T22/T23 | | |4.7.7 | delta N1 =/< 0.2 % | C | T22/T23 | | | | | | | | |4.8 | The calculation is made 'Y04.3' seconds | | | | | | after entry into flight phase 4. | | | | | | | | | | |4.8.1 | 'Y04.3' seconds after PH 4 entry. | C | T22/T23 | |----|------|-----------------------------------------|------|---------| |5001|5 | Each time when a report is generated by | | | |5002| | this logic the number (X04) is decremen-| | | |5003| | ted until zero is reached. The condi-| | | |5004| | tions are described under code No. 4000/| | | |5005| | 4001 (without item 4.2). | | | |. | | | | | |. | | The number (X04) is programmable. | | | |. | | | | | |. | | In case of change the engine serial | | | |500X| | number, (X04) are automatically set to | | | | | | five. | | | | | | The code is appaer in an increasing | | | | | | order, i.e. the first report have the | | | | | | code 5001, the next code is 5002 and so | | | | | | on until 5005 is reached. | | | | | | | | | | |5.1 | Number 'X04' for consecutive legs up to | C | T22/T23 | | | | 9. | | |

R 1EFF : 001-049, 051-099, 101-105, 151-158, 1 31-37-73Page A2 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| |----|------|-----------------------------------------|------|---------| | |5.2 | Number 'X04' in case of ESN change. | | 5 | | | | | | | |----|------|-----------------------------------------|------|---------| |8100|8.1 | ACARS MU uplink request with IMI 'REQ04'| | | | | | The report <04> is immediately generated| | | | | | and transmitted to the ACARS MU. | | | |----|------|-----------------------------------------|------|---------| |8200|8.2 | ACARS MU uplink request with IMI 'G04' | | | | | | The report <04> is generated as the next| | | | | | take-off according to code 4000 or 4100 | | | | | | depending on which logic is armed. | | | |----------------------------------------------------------------------| | AI = Programmable by Airbus Industrie | | C = Programmable by Customer | +----------------------------------------------------------------------+
　
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