R 1EFF : 106-149, 211-299, 301-399, 401-499, 1 31-37-51Page 25 1 1 Aug 01/05 1 1 1CES 1 +----------------------------------------------------------------------+ |Code|Item | |Progr.|Standard | | No.|No. | Description of Function Item |MCDU |Value or | | | | |GSE |Table TXY| |----|------|-----------------------------------------|------|---------|
|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) is taken depending on if an | | |
| | | aircraft is equipped with or without ACT| | |
| | | (Additional Center Tanks). | | |
| | | | | |
| | | Logic for ACT detection | | |
| | | GW | | |
| | | FWC 26.1.276.01.26 26.1.276.01.27 Limit| | |
| | | 26.1.276.10.26 26.1.276.10.27 | | |
| | | | | |
| | | 0 0 GWL1 | | |
| | | 1 0 GWL2 | | |
| | | 0 1 GWL3 | | |
| | | 1 1 GWL4 | | |
| | | | | |
| | | or | | |
| | | | | |
|4900| | GW > GWL (at landing) and VRTA > VRTALG | | |
| | | (during +/- 0.5 sec before and after | | |
| | | landing). | | |
| | | The appropriate GW (GWL1, GWL2, GWL3 or | | |
| | | GWL4) is taken depending on if an | | |
| | | aircraft is equipped with or without ACT| | |
| | | (Additional Center Tanks). Logic for ACT| | |
| | | detection like Code No. 4800. | | |
| | | | | |
|4500| | Report will be generated if one of the | | |
| | | following logic items is present during | | |
| | | the bouncing: | | |
| | | | | |
| | | VRTA > VRTAL1.2 during +/- 0.5 sec at | | |
| | | landing (1st touchdown) | | |
| | | | | |
| | | or | | |
| | | | | |
| | | VRTA > VRTAL1.3 during +/- 0.5 sec at | | |
| | | landing (2nd touchdown). | | |
|----|------|-----------------------------------------|------|---------|
| |4.1 | RALRL limit (ft/sec) A320 | C | -9.0 |
R 1EFF : 106-149, 211-299, 301-399, 401-499, 1 31-37-51Page 26 1 1 Aug 01/05 1 1 1CES 1 +----------------------------------------------------------------------+ |Code|Item | |Progr.|Standard | | No.|No. | Description of Function Item |MCDU |Value or | | | | |GSE |Table TXY| |----|------|-----------------------------------------|------|---------| | | | A321 | C | -9.0 | | | A319 | C | -9.0 | | | A318 | C | -9.0 | | |4.2 | RALT | | | | |4.2.1 | RALTL1 limit (ft) A320 | C | 150.0 | | | | A321 | C | 150.0 | | | | A319 | C | 150.0 | | | | A318 | C | 150.0 | | |4.3 | RALR | | | | |4.3.1 | D geometrical correction factor for | | | | | | ROLR (ft/deg) A320 | C | 0.0 | | | | A321 | C | 0.0 | | | | A319 | C | 0.0 | | | | A318 | C | 0.0 | | |4.3.2 | DX lever arm correction (x-axis) | | | | | | for R/A RALT (ft) A320 | C | 18.0 | | | | A321 | C | 28.8 | | | | A319 | C | 18.5 | | | | A318 | C | 16.8 | | |4.3.3 | DZ lever arm correction (z-axis) | | | | | | for R/A RALT (ft) A320 | C | 7.1 | | | | A321 | C | 7.8 | | | | A319 | C | 7.2 | | | | A318 | C | 7.6 | | |4.3.4 | DXTPIR lever arm correction (x-axis) | | | | | | for PTCH (ft) A320 | C | 39.0 | | | | A321 | C | 53.1 | | | | A319 | C | 33.8 | | | | A318 | C | 29.5 | | | | | | | | |4.3.5 | FC filter frequency (Hz) A320 | C | 0.3 | | | | A321 | C | 0.3 | | | | A319 | C | 0.3 | | | | A318 | C | 0.3 | | | | | | | | |4.3.6 | K1 filter constant A320 | C | 5.2 | | | | A321 | C | 5.2 | | | | A319 | C | 5.2 | | | | A318 | C | 5.2 | | | | | | | | |4.3.7 | K2 filter constant A320 | C | 25.0 | | | | A321 | C | 25.0 |
R 1EFF : 106-149, 211-299, 301-399, 401-499, 1 31-37-51Page 27
1 1 Aug 01/05 1 1 1CES 1 +----------------------------------------------------------------------+ |Code|Item | |Progr.|Standard | | No.|No. | Description of Function Item |MCDU |Value or | | | | |GSE |Table TXY| |----|------|-----------------------------------------|------|---------| | | | A319 | C | 25.0 | | | | A318 | C | 25.0 | | | | | | | | |4.3.8 | K3 filter constant A320 | C | 5.0 | | | | A321 | C | 5.0 | | | | A319 | C | 5.0 | | | | A318 | C | 5.0 | | | | | | | | |4.3.9 | THETA0 (deg) A320 | C | 6.0 | | | | A321 | C | 4.5 | | | | A319 | C | 2.0 | | | | A318 | C | 6.0 | | | | | | | | |4.3.10| S1 (sample) A320 | C | -4.0 | | | | A321 | C | -4.0 | | | | A319 | C | -4.0 | | | | A318 | C | -4.0 | | | | | | | | |4.3.11| S2 (sample) A320 | C | 4.0 | | | | A321 | C | 4.0 | | | | A319 | C | 4.0 | | | | A318 | C | 4.0 | | | | | | | | |4.4 | VRTAL1.1 limit at landing (g) A320 | C | 2.6 | | | | A321 | C | 2.6 | | | | A319 | C | 2.6 | | | | A318 | C | 2.6 | | | | | | | | |4.4.1 | S3 (sample) A320 | C | -16 | | | | A321 | C | -16 | | | | A319 | C | -16 | | | | A318 | C | -16 | | | | | | | | |4.4.2 | S4 (sample) A320 | C | 16 | | | | A321 | C | 16 | | | | A319 | C | 16 | | | | A318 | C | 16 | | | | | | | | |4.5 | VRTAL1.2 limit at landing (1st touchdown| | | | | | ) from bounced land/event (g) A320 | C | 2.6 | | | | A321 | C | 2.6 | | | | A319 | C | 2.6 | 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 4(145)
