A320飞机维护手册 AMM 指示/记录系统 4(154)_航空信息_民用航空_通用航空

曝光台注意防骗网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

R | | | 6D.1.021.01 Bit 14 = 1 (RH gear) | | |
R | | | | | |
R | |4.8 | Bounced landing detection | | |
R | | | A bounced landing is detected when in | | |
R | | | PH7 or PH8 parameter 6D.1.021.01 Bit 11 | | |
R | | | is set to 1 for longer than 'Y15.5' | | |
R | | | seconds and | | |
R | | | then one or both of 6D.1.021.01 Bit 13 | | |
R | | | or Bit 14 is set to 0 for longer than | | |
R | | | 'Y15.6' seconds and | | |
R | | | then the one which was set to 0 or the | | |
R | | | first one of 6D.1.021.01 Bit 13 or | | |
R | | | Bit 14 is set to 1 again within 'Y15.7' | | |
R | | | seconds. | | |
R | | | | | |
R | |4.9 | 'Y15.5' landing gear compress time | | |
R | | | (1st touchdown) (sample) A320 | | 16 |
R | | | A321 | | 16 |
R | | | A319 | | 16 |
R | | | | | |
R | |4.10 | 'Y15.6' time between bounces (sample) | | |
R | | | A320 | | 32 |

R 1EFF : 159-199, 210-210, 1 31-37-51Page 42

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 | | | A321 | | 32 | R | | | A319 | | 32 | R | | | | | | R | |4.11 | 'Y15.7' landing gear compress time | | | R | | | (2nd touchdown) (sample) A320 | | 320 | R | | | A321 | | 320 | R | | | A319 | | 320 | R | | | NOTE: 1 sample is 1/32 second (32 Hz) | | | R |----|------|-----------------------------------------|------|---------| R | |5 | Report shall be generated if one of the | | | R | | | flight (PH5, 5.1, 6, 7, 7.1). There | | | R | | | shall be a spacing time TURBWAIT .sec. | | | R | | | to enable the trigger logic again after | | | R | | | the previous report generation. | | | R | | | | | | R |5100|5.1 | VRTA > VRTAL2.1 if FLAPL < 0.5 deg | | | R | | | | | | R |5200|5.2 | VRTA < VRTAL2.2 if FLAPL < 0.5 deg | | | R | | | | | | R |5300|5.3 | VRTA > VRTAL2.3 if FLAPL >/= 0.5 deg or | | | R | | | VRTA < VRTAL2.4 if FLAPL >/= 0.5 deg | | | R | | | | | | R | | | Limitation for Code 5100, 5200, 5300: | | | R | | | W15 TURBWAIT spacing time for re-| | | R | | | activating the trigger logic after the | | | R | | | previous report generation within the | | | R | | | same flight leg. | | | R | | | | | | R |5400|5.4 | If one of the 5 spoiler excursion | | | R | | | counters has an overflow (999 is | | | R | | | reached). | | | R | | | | | | R | |5.5 | VRTAL2.1 limit (g) A320 | C | 2.5 | R | | | A321 | C | 2.5 | R | | | A319 | C | 2.5 | R | | | | | | R | |5.6 | VRTAL2.2 limit (g) A320 | C | -1.0 | R | | | A321 | C | -1.0 | R | | | A319 | C | -1.0 | R | | | | | | R | |5.7 | VRTAL2.3 limit (g) A320 | C | 2.0 | R | | | A321 | C | 2.0 |
R 1EFF : 159-199, 210-210, 1 31-37-51Page 43 1 1 May 01/05 1 1 1CES 1

R **ON A/C 001-049, 051-099, 101-105, 151-158, 201-209,

B. Report Limits for Load Report <15>.
(1) IAE Engines V2500-A1, V2527-A5.
+-----------------------------------------------------------------------------+ |Limit | Description of Report Item |V2500- |V2527- |SPARE |SPARE | Unit | |No | |A1 |A5 | | | | |------|--------------------------------|-------|-------|-------|------|------| | 301 | Reserved | 0 | 0 | | | | |------|--------------------------------|-------|-------|-------|------|------| | 302 | Reserved | 0 | 0 | | | | |------|--------------------------------|-------|-------|-------|------|------| | 303 | Reserved | 0 | 0 | | | | |------|--------------------------------|-------|-------|-------|------|------| | 304 | Reserved | 0 | 0 | | | | |------|--------------------------------|-------|-------|-------|------|------| | 305 | Reserved | 0 | 0 | | | | |------|--------------------------------|-------|-------|-------|------|------| | 306 | Reserved | 0 | 0 | | | | |------|--------------------------------|-------|-------|-------|------|------| | 307 | Reserved | 0 | 0 | | | | |------|--------------------------------|-------|-------|-------|------|------| | 308 | Reserved | 0 | 0 | | | | |------|--------------------------------|-------|-------|-------|------|------| | 309 | Reserved | 0 | 0 | | | | |------|--------------------------------|-------|-------|-------|------|------| | 310 | Reserved | 0 | 0 | | | | |------|--------------------------------|-------|-------|-------|------|------| | 311 | Reserved | 0 | 0 | | | | |------|--------------------------------|-------|-------|-------|------|------| | 312 | Reserved | 0 | 0 | | | | |------|--------------------------------|-------|-------|-------|------|------| | 313 | Reserved | 0 | 0 | | | | |------|--------------------------------|-------|-------|-------|------|------| | 314 | Reserved | 0 | 0 | | | | |------|--------------------------------|-------|-------|-------|------|------| | 315 | Reserved | 0 | 0 | | | | |------|--------------------------------|-------|-------|-------|------|------| | 316 | Reserved | 0 | 0 | | | | |------|--------------------------------|-------|-------|-------|------|------| | 317 | Reserved | 0 | 0 | | | | |------|--------------------------------|-------|-------|-------|------|------| | 318 | Reserved | 0 | 0 | | | | |------|--------------------------------|-------|-------|-------|------|------|
　
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(154)