R 1EFF : 001-049, 051-099, 101-105, 151-158, 1 31-37-73Page 65
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| |----|------|-----------------------------------------|------|---------| |----|------|-----------------------------------------|------|---------| | |6 | The parameters VN, VL, PHA and N1 in | | | | | | report line V3 and V4 is from the last | | | | | | stable descent. It means the a.m. param.| | | | | | are computed during descent (PH 7.1) | | | | | | when N1 is within N1 target 'N1T.1' +/- | | | | | | a tolerance band of 'X1.1' %rpm. | | | | | | This stable conditions is kept for a | | | | | | time period of 'T1.1' seconds. The | | | | | | vibration parameters are avergaged about| | | | | | the 'T1.1' observing time period and | | | | | | stored in the DMU until the next stable | | | | | | descent is detected. In case of report | | | | | | generation the last stored value is | | | | | | printed. | | | | |6.1 | 'N1T.1' %rpm stable N1 value for descent| C | T22/T23 | | | | | | | | |6.2 | 'X1.1' %rpm tolerance band for descent | C | T22/T23 | | | | | | | | |6.3 | 'T1.1' seconds stable observing time | C | T22/T23 | | | | for descent (max. 20 sec). | | | |----|------|-----------------------------------------|------|---------| | |7 | The parameters VN, VL, PHA, PHT and N1 | | | | | | report line V5 and V6 is from the last | | | | | | stable take off. It means the a.m. | | | | | | parameters are computed during climb | | | | | | (PH 5.1) when N1 is within N1target | | | | | | 'N1T.2' +/- a tolerance band of 'X1.2' | | | | | | %rpm. This stable conditions are kept | | | | | | for a time period of 'T1.2' seconds. The| | | | | | vibration parameters are averaged about | | | | | | the 'T1.2' observing time period and | | | | | | stored in the DMU until the next stable | | | | | | take off is detected. In case of report | | | | | | generation the last stored value is | | | | | | printed. | | | | | | | | | | |7.1 | 'N1T.2' %rpm stable N1 value for climb | C | T22/T23 | | | | | | | | |7.2 | 'X1.2' %rpm tolerance band for climb | C | T22/T23 | | | | | | | | |7.3 | 'T1.2' seconds stable observing time for| C | T22/T23 |
R 1EFF : 001-049, 051-099, 101-105, 151-158, 1 31-37-73Page 66
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| |----|------|-----------------------------------------|------|---------| | | | climb (max. 20 sec) | | | |----|------|-----------------------------------------|------|---------| |8100|8.1 | ACARS MU uplink request with IMI 'REQ02'| | | | | | 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 | +----------------------------------------------------------------------+
R **ON A/C 106-149, 211-299, 301-399, 401-499,
(1) Cruise Performance Report Data Field Description <02> (Engine Type CFMI with Advanced EVMU)
NOTE : Only the parts of the CRUISE PERFORMANCE REPORT <02> which are
____ not included in the ENGINE CRUISE REPORT <01> are given in the subsequent table.
+---------------------------------------------------------------------+ | Value | Content Description | |--------------|------------------------------------------------------| | QA | Aircraft Quality Number, Report Stability | | 99 | DMU (00 to 99) | | | NOTE: 00 = best stable frame | | | 99 = worst stable frame | |--------------|------------------------------------------------------| | WFQ | Fuel Quantity Inner Cell | | 99999 | FQIC (0 to 99999 kg) | | | 5A.2.257.10 Left Inner Cell Fuel Quantity | | | 5A.2.261.10 Right Inner Cell Fuel Quantity | | | NOTE: Report line 'X1' shows Left Inner Cell Fuel | | | Quantity. | | | Report line 'X2' shows Right Inner Cell Fuel |
R 1EFF : 001-049, 051-099, 101-149, 151-158, 1 31-37-73Page 67 1201-209, 211-299, 301-399, 401-499, 1Aug 01/05 1 1 1CES 1 +---------------------------------------------------------------------+ | Value | Content Description | |--------------|------------------------------------------------------| | | Quantity. | |--------------|------------------------------------------------------| | ELEV | Elevator Position | | X999 | FCDC (-30 to 15 deg) | | | 6C.1.314.01 Left Elevator Position | | | 6C.2.314.10 | | | 6C.1.334.01 Right Elevator Position | | | 6C.2.334.10 | | | NOTE: Negative values are shown with N in the | | | first position. | | | Otherwise the first position has a 0. | | | NOTE: Report line 'X1' shows the Left Elevator | | | Position. | | | Report line 'X2' shows the Right Elevator | | | Position. | |--------------|------------------------------------------------------| | AOA | Corrected Angle of Attack | | X999 | ADIRU (-30 to 85 deg) | | | 06.1.241.01 AOA System 1 | | | 06.2.241.10 AOA System 2 | | | NOTE: Negative values are shown with N in the | | | first position. | | | Otherwise the first position has a 0. | | | NOTE: Report line 'X1' shows ADA System 1. | | | Report line 'X2' shows ADA System 2. | |--------------|------------------------------------------------------| | SLP | Side Slip Angle | | X999 | FAC (-32.0 to 32.0 deg) | | | 0A.1.226.00 SLP System 1 | | | 0A.2.226.00 SLP System 2 | | | NOTE: Negative values are shown with N in the | | | first position. | | | Otherwise the first position has a 0. | | | NOTE: Report line 'X1' shows SLP System 1. | | | Report line 'X2' shows SLP System 2. | |--------------|------------------------------------------------------| | CFPG | Calculated Flight Path Acceleration | | X9999 | DMU (-0.9999 to 4.0000 g) | | | NOTE: Negative values are shown with N in the | | | first position. | | | Otherwise the first position has a 0. | | | NOTE: Report line 73 shows CFPG calculated with GS | | | from ADIRU System 1. | | | Report line 75 shows CFPG calculated with GS |
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