R 1EFF : 001-049, 051-099, 101-105, 151-158, 1 31-37-49Page 22 1201-209, 1May 01/05 1 1 1CES 1 +---------------------------------------------------------------------+ | Value | Content Description | |--------------|------------------------------------------------------| |--------------|------------------------------------------------------| | LCDT | Load Compressor Discharge Temperature | | X999 | (-50 to 220 C) | | | param. 7A.1.074.01 | |--------------|------------------------------------------------------| | GLA | APU Generator Load | | 999 | (0 to 256 %) | | | param. 29.1.100.00 | | | 29.2.100.00 | +---------------------------------------------------------------------+

 (2) APU Shutdown Report Logic
 +----------------------------------------------------------------------+ |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 | | | | |G | 'Y14.1' Average intervals for MES param.| C | 1 | |----|------|-----------------------------------------|------|---------| |1000|1 | Manual selection via MCDU | | | |----|------|-----------------------------------------|------|---------| |2000|2 | Flight phase dependent manual | | | | | | selection via remote print button | | | | | | if programmed. | | | | |2.1 | Logic algorithm | | | | |2.2 | Flight Phase (no standard programming) | C | 1 | |----|------|-----------------------------------------|------|---------| |3000|3 | Programmable Start Logic | | | | |3.1 | Logic algorithm | C | | | |3.2 | Logic criteria values | C | not | |----|------|-----------------------------------------|------|---------| |4000|4 | APU shutdown detected by ECB. The DMU | | | | | | shall observe 7A.1.037.01.17 when this | | | | | | bit is set to 1, then the reason for the| | | | | | shut down is detected by one of the | | |
R 1EFF : 001-049, 051-099, 101-105, 151-158, 1 31-37-49Page 23 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| |----|------|-----------------------------------------|------|---------| | | | bits describe as follows: | | | | | | | | | |4110|4.1 | 7A.1.353.01.11 = 1 (NO FLAME) | C | | | | | or | | | |4120|4.2 | 7A.1.353.01.12 = 1 (REVERSE FLOW) | C | | | | | or | | | |4130|4.3 | 7A.1.353.01.13 = 1 (LOSS OF DC POWER) | C | | | | | or | | | |4140|4.4 | 7A.1.353.01.14 = 1 (HIGH OIL TEMPERAT.) | C | | | | | or | | | |4160|4.6 | 7A.1.353.01.17 = 1 (AIR INTAKE NOT OPEN)| C | | | | | or | | | |4170|4.7 | 7A.1.353.01.18 = 1 (GENERATOR HIGH OIL | C | | | | | TEMPERATURE) | | | | | | or | | | |4180|4.8 | 7A.1.353.01.20 = 1 (OVERTEMPERATURE) | C | | | | | or | | | |4190|4.9 | 7A.1.353.01.21 = 1 (SENSOR FAILURE) | C | | | | | or | | | |4200|4.10 | 7A.1.353.01.22 = 1 (NO ACCELERATION) | C | | | | | or | | | |4210|4.11 | 7A.1.353.01.23 = 1 (START TIME EXCEEDED)| C | | | | | or | | | |4220|4.12 | 7A.1.353.01.24 = 1 (OVERSPEED) | C | | | | | or | | | |4230|4.13 | 7A.1.353.01.25 = 1 (ECB FAILURE) | C | | | | | or | | | |4240|4.14 | 7A.1.353.01.26 = 1 (LOW OIL PRESSURE) | C | | | | | or | | | |4250|4.15 | 7A.1.353.01.27 = 1 (LOSS OF SPEED) | C | | | | | or | | | |4260|4.16 | 7A.1.353.01.28 = 1 (IGV FAILURE) | C | | | | | or | | | | |4.17 | It is possible to suppress each item | | | | | | individually via the GSE. | | | |----|------|-----------------------------------------|------|---------| |8100|8.1 | ACARS MU uplink request with IMI 'REQ14'| | | | | | The report <14> 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 31-37-49Page 24 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| |----|------|-----------------------------------------|------|---------| +----------------------------------------------------------------------+

R **ON A/C 106-149, 211-299, 301-399, 401-499,
 (1) APU Shutdown Report Data Field Description
 +---------------------------------------------------------------------+ | Value | Content Description | |--------------|------------------------------------------------------| | ASN | APU Serial Number | | 9999 | (0 to 9999) | | | param. 7A.1.050.01 | |--------------|------------------------------------------------------| | AHRS | APU Operating Hours | | 99999 | (0 to 99999) | | | param. 0D.1.110.00 | |--------------|------------------------------------------------------| | ACYC | APU Start Cycles | | 99999 | (0 to 99999) | | | param. 0D.1.111.00 | |--------------|------------------------------------------------------| | PFAD | APU Performance Adjustment | | XXXXX | | | | param. 7A.1.004.01 | |--------------|------------------------------------------------------| | ACW3 | APU Control Word 3 | | XXXXX | Each 'X' represents 4 Bits in hexadecimal code of | | | a defined ARINC 429 word: | | | XXXXX Bits HEX | | | |||||___________ 14, 13, 12, 11 0...F | | | ||||____________ 18, 17, 16, 15 0...F | | | |||_____________ 22, 21, 20, 19 0...F | | | ||______________ 26, 25, 24, 23 0...F | | | |_______________ 29, 28, 27 0...7 | | | --------------------------------------------| | | | | | Bit Label Parameter Description | | | 11 7A.1.351.01.11 = 1 PT Sensor Failed | | | 12 7A.1.351.01.12 = 1 Delta P Sensor Failed | | | 13 7A.1.351.01.13 = 1 Speed Sensor No.1 Failed | | | 14 7A.1.351.01.14 = 1 Speed Sensor No.2 Failed |
　
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