| Value | Content Description |
|--------------|------------------------------------------------------| R | 999 | (1 to 5.00 bar) | R | | param. 7A.1.166.01 | R |--------------|------------------------------------------------------| R | GLA | APU Generator Load | R | 999 | (0 to 256 %) | R | | param. 29.1.100.00 | R | | 29.2.100.00 | R +---------------------------------------------------------------------+
R (2) APU Shutdown Report Logic
R +----------------------------------------------------------------------+ R |Code|Item | |Progr.|Standard | R | No.|No. | Description of Function Item |MCDU |Value or | R | | | |GSE |Table TXY| R |----|------|-----------------------------------------|------|---------| R | |A | Report Format | | | R | |B | Parameter Table | | | R | |C | First three lines of Report | C | Blank | R | |D | Print Out Rules | C | | R | |E | Transfer to ACARS MU | C | Yes | R | |F | Increment of the report counter if the | C | 1 | R | | | report was triggered by a code number | | | R | | | > 1000; 1=yes, 0=no | | | R | |G | 'Y14.1' Average intervals for MES param.| C | 1 | R |----|------|-----------------------------------------|------|---------| R |1000|1 | Manual selection via MCDU | | | R |----|------|-----------------------------------------|------|---------| R |2000|2 | Flight phase dependent manual | | | R | | | selection via remote print button | | | R | | | if programmed. | | | R | |2.1 | Logic algorithm | | | R | |2.2 | Flight Phase (no standard programming) | C | 1 | R |----|------|-----------------------------------------|------|---------| R |3000|3 | Programmable Start Logic | | | R | |3.1 | Logic algorithm | C | | R | |3.2 | Logic criteria values | C | not | R | | | | | progr. | R |----|------|-----------------------------------------|------|---------| R |4000|4 | APU shutdown detected by ECB. The DMU | | | R | | | observes 7A.1.037.01.17 when this bit is| | | R | | | set to 1, then the reason for the shut | | | R | | | down is detected by one of the bits | | | R | | | describe as follows: | | |
R 1EFF : 159-199, 210-210, 1 31-37-49Page 33 1 1 May 01/05 1 1 1CES 1
+----------------------------------------------------------------------+
|Code|Item | |Progr.|Standard |
| No.|No. | Description of Function Item |MCDU |Value or |
| | | |GSE |Table TXY|
|----|------|-----------------------------------------|------|---------|
R | | | | | |
R |4110|4.1 | 7A.1.353.01.11 = 1 (NO FLAME) | C | |
R | | | or | | |
R |4120|4.2 | 7A.1.353.01.12 = 1 (REVERSE FLOW) | C | |
R | | | or | | |
R |4130|4.3 | 7A.1.353.01.13 = 1 (LOSS OF DC POWER) | C | |
R | | | or | | |
R |4140|4.4 | 7A.1.353.01.14 = 1 (HIGH OIL TEMPERAT.) | C | |
R | | | or | | |
R |4160|4.6 | 7A.1.353.01.17 = 1 (AIR INTAKE NOT OPEN)| C | |
R | | | or | | |
R |4170|4.7 | 7A.1.353.01.18 = 1 (GENERATOR HIGH OIL | C | |
R | | | TEMPERATURE) | | |
R | | | or | | |
R |4180|4.8 | 7A.1.353.01.20 = 1 (OVERTEMPERATURE) | C | |
R | | | or | | |
R |4190|4.9 | 7A.1.353.01.21 = 1 (SENSOR FAILURE) | C | |
R | | | or | | |
R |4200|4.10 | 7A.1.353.01.22 = 1 (NO ACCELERATION) | C | |
R | | | or | | |
R |4210|4.11 | 7A.1.353.01.23 = 1 (START TIME EXCEEDED)| C | |
R | | | or | | |
R |4220|4.12 | 7A.1.353.01.24 = 1 (OVERSPEED) | C | |
R | | | or | | |
R |4230|4.13 | 7A.1.353.01.25 = 1 (ECB FAILURE) | C | |
R | | | or | | |
R |4240|4.14 | 7A.1.353.01.26 = 1 (LOW OIL PRESSURE) | C | |
R | | | or | | |
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM 指示/記錄系統 4(133)
