曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

R 1EFF : 001-049, 051-099, 101-149, 151-158, 1 31-37-49Page 25 1201-209, 211-299, 301-399, 401-499, 1Aug 01/05 1 1 1CES 1 +---------------------------------------------------------------------+ | Value | Content Description | |--------------|------------------------------------------------------| | | 15 7A.1.351.01.15 = 1 High Oil Temp Switch Failed| | | 16 7A.1.351.01.16 = 1 Oil Temp Sensor Failed | | | 17 7A.1.351.01.17 = 1 Fuel Control Torq. Motor | | | Failed | | | 18 7A.1.351.01.18 = 1 Surge Valve Torq. Motor | | | Failed | | | 19 7A.1.351.01.19 = 1 EGT Rake No.1 Failed | | | 20 7A.1.351.01.20 = 1 EGT Rake No.2 Failed | | | 21 7A.1.351.01.21 = 1 IGV Actuator Failed | | | 22 7A.1.351.01.22 = 1 Ignition Unit Failed | | | 23 7A.1.351.01.23 = 1 Deoil Solenoid Failed | | | 24 7A.1.351.01.24 = 1 Gen. Oil Temp Sensor Failed| | | 25 7A.1.351.01.25 = 1 ECS Demand Signal Failed | | | 26 7A.1.351.01.26 = 1 APU Starter Failed | | | 27 SPARE | | | 28 SPARE | | | 28 SPARE | |--------------|------------------------------------------------------| | ACW4 | APU Control Word 4 | | 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 | | | --------------------------------------------| | | DMU, composed of several ECU discrete labels as | | | defined below. | | | 0D.1.070.00 | | | Bit Label Parameter Description | | | 11 7A.1.351.01.27 = 1 Oil Pressure Switch Failed | | | 12 7A.1.351.01.28 = 1 P2 Sensor Failed | | | 13 7A.1.351.01.29 = 1 ECB Failed | | | 14 7A.1.352.01.12 = 1 Load Valve Solenoid Failed | | | 15 7A.1.352.01.13 = 1 LCDT Sensor Failed | | | 16 7A.1.352.01.14 = 1 LCIT Sensor Failed | | | 17 7A.1.352.01.15 = 1 Fuel Solenoid Failed | | | 18 7A.1.352.01.16 = 1 Starter Contactor Failed | | | 19 7A.1.352.01.17 = 1 Back Up Starter Cont.Failed| | | 20 7A.1.352.01.18 = 1 APU S/N Encoder Failed | | | 21 7A.1.352.01.20 = 1 Air Intake Actuator Failed | | | 22 7A.1.352.01.22 = 1 IGV LVDT Failed |

R 1EFF : 106-149, 211-299, 301-399, 401-499, 1 31-37-49Page 26 1 1 Aug 01/05 1 1 1CES 1 +---------------------------------------------------------------------+ | Value | Content Description | |--------------|------------------------------------------------------| | | 23 SPARE | | | 24 SPARE | | | 25 7A.1.037.01.13 = 1 APU Low Fuel Pressure | | | 26 7A.1.037.01.20 = 1 APU Low Oil Level | | | 27 SPARE | | | 28 SPARE | | | 29 SPARE | |--------------|------------------------------------------------------| | NA | APU Rotation Speed | | 9999 | (0 to 120.0 %rpm) | | | param. 7A.1.176.01 | |--------------|------------------------------------------------------| | EGTA | APU Exhaust Gas Temperature | | X999 | (-50 to 1000 Degrees C) | | | param. ECB 7A.1.175.01 | |--------------|------------------------------------------------------| | OTA | APU Oil Sump Temperature | | X99 | (-55 to 200 Degrees C) | | | param. ECB 7A.1.247.01 | | | Report line V1 shows the value from previous APU | | | start. | |--------------|------------------------------------------------------| | IGV | IGV Position | | X99 | (-14 to 90 deg) | | | param. ECB 7A.1.130.01 | |--------------|------------------------------------------------------| | WB | Bleed Air Flow | | 999 | (0.5 to 2.00 kg/sec) | | | param. ECB 7A.1.123.01 | |--------------|------------------------------------------------------| | LCIT | Load Compressor Inlet Temperature | | X999 | (-70 to 128 Degrees C) | | | param. ECB 7A.1.110.01 | | | Report line V1 shows the value from previous APU | | | start. | |--------------|------------------------------------------------------| | PT | Bleed Air Pressure | | 999 | (1 to 5.00 bar) | | | param. ECB 7A.1.166.01 | |--------------|------------------------------------------------------| | GLA | APU Generator Load | | 999 | (0 to 256 %) | | | param. SDAC 29.1.100.00 | | | 29.2.100.00 |

R 1EFF : 106-149, 211-299, 301-399, 401-499, 1 31-37-49Page 27 1 1 Aug 01/05 1 1 1CES 1 +---------------------------------------------------------------------+ | Value | Content Description | |--------------|------------------------------------------------------| +---------------------------------------------------------------------+

 (2) APU Shutdown Report Logic <14>
 +----------------------------------------------------------------------+ |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 | | | | |G | 'Y14.1' Average intervals in seconds | 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 | | | | | | progr. | |----|------|-----------------------------------------|------|---------| | |4 | APU shutdown detected by ECB. The DMU | | | | | | observes 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 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 | | |
　
中國航空網 www.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(tǒng) 4(130)