R 1EFF : 159-199, 210-210, 1 31-37-73Page A72 1 1 May 01/05 1 1 1CES 1
+---------------------------------------------------------------------+
| Value | Content Description |
|--------------|------------------------------------------------------|
R | | 1 0 1 0 0 | K |
R | | 1 0 1 0 1 | L |
R | | 1 0 1 1 0 | M |
R | | 1 0 1 1 1 | N |
R | | 1 1 0 0 0 | O |
R | | 1 1 0 0 1 | P |
R | | 1 1 0 1 0 | Q |
R | | 1 1 0 1 1 | R |
R | | 1 1 1 0 0 | S |
R | | 1 1 1 0 1 | T |
R | | 1 1 1 1 0 | U |
R | | 1 1 1 1 1 | V |
R | | |
R |--------------|------------------------------------------------------|
R | REASON | Reason for Exceedance |
R | XXXXXXXXXX | DMU |
R | XXXXXXXXXX | Up to 20 Characters |
R | | EGT Code: 4110, 4120, 4130 and 4140 |
R | | TN Code: 4150, 4160, 4170 and 4180 |
R | | If the report was not triggered by a limit |
R | | exceedence then this field contains blanks. |
R +---------------------------------------------------------------------+
R **ON A/C 001-049, 051-099, 101-105, 151-158, 201-209,
(2) Engine Divergence Report Logic <09> (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 | | |
|----|------|-----------------------------------------|------|---------|
|1000|1 | Manual selection via MCDU | | |
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 31-37-73Page A73 1201-210, 1May 01/05 1 1 1CES 1 +----------------------------------------------------------------------+ |Code|Item | |Progr.|Standard | | No.|No. | Description of Function Item |MCDU |Value or | | | | |GSE |Table TXY| |----|------|-----------------------------------------|------|---------| |----|------|-----------------------------------------|------|---------| |2000|2 | Flight phase dependent manual | | | | | | selection via remote print button | | | | | | if programmed. | | | | |2.1 | Remote Print Button assignment. | C | not | |----|------|-----------------------------------------|------|---------| |3000|3 | Programmable Start Logic | | | | |3.1 | Trigger condition | C | not | |----|------|-----------------------------------------|------|---------| | |4 | If during flight phase climb and cruise | | | | | | (5.1 and 6) the condiiton as defined | | | | | | under item 4.2 are met the EGT Divergen-| | | | | | ce and TN Divergence monitoring function| | | | | | are performed as defined under item 4.3 | | | | | | to 4.4. | | | | | | A divergence report is generated at each| | | | | | time when the value of EGTdiv or TNdiv | | | | | | exceeds the defined threshold values | | | | | | defined below. | | | | |4.1 | Threshold values: | | | |4110|4.1.1 | EGTdivT1 limit in C | C | T22/T23 | |4120|4.1.2 | EGTdivT2 limit in C | C | T22/T23 | |4130|4.1.3 | EGTdivT3 limit in C | C | T22/T23 | |4140|4.1.4 | EGTdivT4 limit in C | C | T22/T23 | |4150|4.1.5 | TNdivT1 limit in C | C | T22/T23 | |4160|4.1.6 | TNdivT2 limit in C | C | T22/T23 | |4170|4.1.7 | TNdivT3 limit in C | C | T22/T23 | |4180|4.1.8 | TNdivT4 limit in C | C | T22/T23 | | | | | | | | |4.2 | Divergence Monitoring Condiitons | | | | | | 1. N1 actual of both engines > N1L1 | | | | | | 2. N1 actual of both engines < N1L2 | | | | | | 3. N1 actual of both engines is within | | | | | | N1L3 of each other. | | | | | | 4. Bleed loads for both engines are | | | | | | symmetrical and crossfeed valve is | | | | | | closed. | | | | | | 5. IVV stable within IVVL, only valid | | | | | | during PH 6. | | | | | | 6. ALT < ALTL, only valid during PH 5.1.| | | | | | 7. Delta TAT within TATL. | | | | | | 8. N1rate within N1RL | | | 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320飞机维护手册 AMM 指示/记录系统 5(56)
