**ON A/C 159-199, 210-210,
 (1) Engine Run Up Report Data Field Description <11> (Engine Type CFMI with Advanced EVMU)
 NOTE : Only the parts of the ENGINE RUN UP REPORT <11> which are not
____ included in the ENGINE CRUISE REPORT <01> are given in the subsequent table.
R 1EFF : 106-149, 159-199, 210-299, 301-399, 1 31-37-73Page B18 1401-499, 1Aug 01/05 1 1 1CES 1R +---------------------------------------------------------------------+ R | Value | Content Description | R |--------------|------------------------------------------------------| R | EGTK | Corrected Exhaust Gas Temperature | R | X999 | (-55 to 999.9 C) | R | | TAT = 06.1.211.01 | R | | 06.2.211.10 | R | | EGT = 7C.1.345.01 Engine 1 | R | | 7C.2.345.10 Engine 2 | R |--------------|------------------------------------------------------| R | N1K | Corrected N1 | R | 9999 | (0 to 120%rpm) | R | | TAT = 06.1.211.01 | R | | 06.2.211.10 | R | | N1 = 7C.1.346.01 Engine 1 | R | | 7C.2.346.10 Engine 2 | R |--------------|------------------------------------------------------| R | N2K | Corrected N2 | R | 9999 | (0 to 120%rpm) | R | | TAT = 06.1.211.01 | R | | 06.2.211.10 | R | | N2 = 7C.1.344.01 Engine 1 | R | | 7C.2.344.10 Engine 2 | R |--------------|------------------------------------------------------| R | FFK | Corrected Engine Fuel Flow | R | 9999 | (0 to 70000 kg/h) | R | | TAT = 06.1.211.01 | R | | 06.2.211.10 | R | | FF = 7C.1.345.01 Engine 1 | R | | 7C.2.345.10 Engine 2 | R | | PT2 = 7C.1.131.01 Engine 1 | R | | 7C.2.131.10 Engine 2 | R +---------------------------------------------------------------------+

R 1EFF : 159-199, 210-210, 1 31-37-73Page B19 1 1 May 01/05 1 1 1CES 1R **ON A/C 001-049, 051-099, 101-105, 151-158, 201-209,

 (2) Engine Run Up Report Logic <11> (Engine Type CFMI with Advanced EVMU)
 +----------------------------------------------------------------------+ |Code|Item | |Progr.|Standard | | No.|No. | Description of Function Item |MCDU |Value or | | | | |GSE |Table TXY| |----|------|-----------------------------------------|------|---------| | |A | Report Format | | | | |B | Parameter Table | | | | |C | First three lines of Report | C | Blank | | |D | Print Out Rules | C | 2 | | |E | Transfer to ACARS MU | C | No | | |F | Increment of the report counter if the | C | 1 | | | | report was triggered by a code number | | | | | | > 1000; 1=yes, 0=no | | | | |G1 | n1 value (N1) | AI | 0.5 | | |G2 | n2 value (EGT) | AI | 1.05 | | |G3 | n3 value (N2) | AI | 0.5 | | |G4 | n4 value (FF) | AI | 0.63 | |----|------|-----------------------------------------|------|---------| |1000|1 | Manual selection via MCDU | | | |----|------|-----------------------------------------|------|---------| |2000|2 | Flight phase dependent manual | | | | | | selection via remote print button | | | | | | if programmed. | | | | |2.1 | Remote Print Button assignment. | C | 2 and 3 | |----|------|-----------------------------------------|------|---------| |3000|3 | Programmable Start Logic | | | | |3.1 | Trigger condition | C | not | |----|------|-----------------------------------------|------|---------| |8100|8.1 | ACARS MU uplink request with IMI 'REQ11'| | | | | | The report <11> is immediately generated| | | | | | and transmitted to the ACARS MU. | | | |----------------------------------------------------------------------| | AI = Programmable by Airbus Industrie | | C = Programmable by Customer | +----------------------------------------------------------------------+
R 1EFF : 001-049, 051-099, 101-105, 151-158, 1 31-37-73Page B20 1201-209, 1May 01/05 1 1 1CES 1R **ON A/C 106-149, 159-199, 210-299, 301-399, 401-499,

 (2) Engine Run Up Report Logic <11> (Engine Type CFMI with Advanced EVMU)
 +----------------------------------------------------------------------+ |Code|Item | |Progr.|Standard | | No.|No. | Description of Function Item |MCDU |Value or | | | | |GSE |Table TXY| |----|------|-----------------------------------------|------|---------| | |A | Report Format | | | | |B | Parameter Table | | | | |C | First three lines of Report | C | Blank | | |D | Print Out Rules | C | | | |E | Transfer to ACARS MU | C | Yes | | |F | Increment of the report counter if the | C | 1 | | | | report was triggered by a code number | | | | | | > 1000; 1=yes, 0=no | | | | | | Exponents for correction of N1, N2 EGT | | | | | | and FF. | | | | |G1 | n1 value (N1) | A | 0.5 | | |G2 | n2 value (EGT) | A | 1.05 | | |G3 | n3 value (N2) | A | 0.5 | | |G4 | n4 value (FF) | A | 0.63 | |----|------|-----------------------------------------|------|---------| |1000|1 | Manual selection via MCDU | | | |----|------|-----------------------------------------|------|---------| |2000|2 | Flight phase dependent manual | | | | | | selection via remote print button | | | | | | if programmed. | | | | |2.1 | Remote Print Button assignment. | C | 2 and 3 | |----|------|-----------------------------------------|------|---------| |3000|3 | Programmable Start Logic | | | | |3.1 | Trigger condition | C | not | | | | | | progr. | |----|------|-----------------------------------------|------|---------| |8100|8.1 | ACARS MU uplink request with IMI 'REQ1' | | | | | | The report <11> is immediately generated| | | | | | and transmitted to the ACARS MU. | | | |----------------------------------------------------------------------| |  A  =  Programmable by Airbus Industrie | |  C  =  Programmable by Customer | +----------------------------------------------------------------------+
　
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