A320飞机维护手册 AMM 指示/记录系统 4(139)

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 |  |E  | Transfer to ACARS MU  (yes/no)  | C  | No  |
 |  |  |  |  |  |
 |  |F  | Increment of the report counter (yes/no)|  | Yes  |
 |  |  |  |  |  |
 |  |G  | Inhibit report triggers  (yes/no)  | C  | No  |
 |  |  |  |  |  |
 |  |H  | 'Y15.0' sec before land/event  A320| C  |  1  |
 |  |  |  A321| C  |  1  |
 |  |  |  A319| C  |  1  |
 |  |  |  |  |  | 

R 1EFF : 001-049, 051-099, 101-105, 151-158, 1 31-37-51Page 9

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| |----|------|-----------------------------------------|------|---------| | |I | 'Y15.1' sec before land/event A320| C | 1 | | | | A321| C | 1 | | | | A319| C | 1 | | | | | | | | |J | 'Y15.2' sec after land/event A320| C | 3 | | | | A321| C | 3 | | | | A319| C | 3 | | | | | | | | |K | 'Y15.3' sec before bounced A320| C | 1 | | | | A321| C | 1 | | | | A319| C | 1 | | | | | | | | |L | 'Y15.4' sec before bounced A320| C | 1 | | | | A321| C | 1 | | | | A319| C | 1 | | | | | | | | |M | 'Y15.5' sec after bounced A320| C | 3 | | | | A321| C | 3 | | | | A319| C | 3 | | | | | | | | |N | N dataset time sample at landing | C | 1 | | | | to check for RALR trigger | | | | | | Note: -N dataset time is programmable | | | | | | from 0 to 5. | | | | | | -1 sample is 1/16 second (16 Hz) | | | |----|------|-----------------------------------------|------|---------| |1000| | Not applicable | | | |----|------|-----------------------------------------|------|---------| |2000| | Not applicable | | | |----|------|-----------------------------------------|------|---------| |3000|3 | Programmable Start Logic | | | | |3.1 | Logic algorithm | C | | | |3.2 | Logic criteria values | C |not prog.| | | | | | | | | | The parameters which are used for logic | | | | | | items described as follows shall be | | | | | | observed with a rate of 16 Hz. | | | | | | Exceptions: | | | | | | At landing (0.5 sec before and 0.5 sec | | | | | | after landing or bounce), the non-| | | | | | filtered acceleration VRTA and the non- | | | | | | filtered landing gear status (see to | | |

R 1EFF : 001-049, 051-099, 101-105, 151-158, 1 31-37-51Page 10 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| |----|------|-----------------------------------------|------|---------| | | | item no. 4.7) shall be observed with | | | | | | a rate of 32 Hz. | | | |----|------|-----------------------------------------|------|---------|

 |  |4  | Report will be generated if one of the |  |  |
 |  |  | following logic items is present during |  |  |
 |  |  | landing: |  |  |
 |4100|  | RALR < RALRL |  |  |
 |  |  | calculated between Start Sample Number |  |  |
 |  |  | S1 and Stop Sample Number S2 |  |  |
 |  |  | or |  |  |
 |4400|  | VRTA > VRTAL1.1 |  |  |
 |  |  | (during +/- 0.5 seconds before and after|  |  |
 |  |  | landing) calculated between Start |  |  |
 |  |  | Sample Number S3 and Stop Samble |  |  |
 |  |  | Number S4 |  |  |
 |  |  | or |  |  |
 |4800|  | GW > GWL (at landing) and RALR < RALRLG |  |  |
 |  |  | (at dataset time at landing (see item |  |  |
 |  |  | no. L)). |  |  |
 |  |  | The appropriate GW (GWL1, GWL2, GWL3 or |  |  |
 |  |  | GWL4) shall be taken depending if an |  |  |
 |  |  | aircraft is equipped with or without ACT|  |  |
 |  |  | (Additional Center Tanks). |  |  |
 |  |  | |  |  |
 |  |  | Logic for ACT detection |  |  |
 |  |  | |  |  |
 |  |  | FWC 26.1.276.01 Bit 26 Bit 27 GW Limit|  |  |
 |  |  | 26.2.276.10 26 27 |  |  |
 |  |  | 0 0 GWL1 |  |  |
 |  |  | 1 0 GWL2 |  |  |
　
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