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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| |----|------|-----------------------------------------|------|---------| | | | A320 | | 32 | | | | A321 | | 32 | | | | A319 | | 32 | | | | | | | | |4.11 | 'Y15.7' landing gear compress time | | | | | | (2nd touchdown) (sample) A320 | | 320 | | | | A321 | | 320 | | | | A319 | | 320 | |----|------|-----------------------------------------|------|---------| | |5 | Report shall be generated if one of the | | | | | | flight (PH5, 5.1, 6, 7, 7.1). There | | | | | | shall be a spacing time TURBWAIT .sec. | | | | | | to enable the trigger logic again after | | | | | | the previous report generation. | | | | | | | | | |5100|5.1 | VRTA > VRTAL2.1 if FLAPL < 0.5 deg | | | | | | | | | |5200|5.2 | VRTA < VRTAL2.2 if FLAPL < 0.5 deg | | | | | | | | | |5300|5.3 | VRTA > VRTAL2.3 if FLAPL >/= 0.5 deg or | | | | | | VRTA < VRTAL2.4 if FLAPL >/= 0.5 deg | | | | | | | | | | | | Limitation for Code 5100, 5200, 5300: | | | | | | W15 TURBWAIT spacing time for re-| | | | | | activating the trigger logic after the | | | | | | previous report generation within the | | | | | | same flight leg. | | | | | | | | | |5400|5.4 | If one of the 5 spoiler excursion | | | | | | counters has an overflow (999 is | | | | | | reached). | | | | | | | | | | |5.5 | VRTAL2.1 limit (g) A320 | C | 2.5 | | | | A321 | C | 2.5 | | | | A319 | C | 2.5 | | | | | | | | |5.6 | VRTAL2.2 limit (g) A320 | C | -1.0 | | | | A321 | C | -1.0 | | | | A319 | C | -1.0 | | | | | | | | |5.7 | VRTAL2.3 limit (g) A320 | C | 2.0 | | | | A321 | C | 2.0 |
R 1EFF : 001-049, 051-099, 101-105, 151-158, 1 31-37-51Page 15
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| |----|------|-----------------------------------------|------|---------| | | | A319 | C | 2.0 | | | | | | | | |5.8 | VRTAL2.4 limit (g) A320 | C | 0.0 | | | | A321 | C | 0.0 | | | | A319 | C | 0.0 | | | | | | | | |5.9 | TURBWAIT (sec.) A320 | C | 10 | | | | A321 | C | 10 | | | | A319 | C | 10 | | | | | | | | |5.10 | FLAPL (deg) A320 | C | 0.5 | | | | A321 | C | 0.5 | | | | A319 | C | 0.5 | |----------------------------------------------------------------------| | AI = Programmable by Airbus Industrie | | C = Programmable by Customer | +----------------------------------------------------------------------+
R **ON A/C 106-149, 211-299, 301-399, 401-499,
(1) Load Report Data Field Description <15>
+---------------------------------------------------------------------+ | Value | Content Description | |--------------|------------------------------------------------------| | ESN | Engine Serial Number | | 999999 | (000000 to 999999) | | | ECU Eng 1 param. 7C.1.046.01 digit 3, 2, 1 | | | 7C.1.047.01 digit 6, 5, 4 | | | Eng 2 param. 7C.2.046.10 digit 3, 2, 1 | | | 7C.2.047.10 digit 6, 5, 4 | |--------------|------------------------------------------------------| | EHRS | Engine Flight Hours | | 99999 | (00000 to 99999 hours) | | | DMU Engine 1 0D.1.060.01 | | | Engine 2 0D.1.060.10 | | | | | | Time between "Main (LH and RH) Landing Gear| | | Decompressed" and "Main (LH and RH) Landing Gear| | | "Compressed". The EHRS is set to zero if a new ESN | | | is regonized by the DMU. It is possible to set the |
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1201-209, 211-299, 301-399, 401-499, 1Aug 01/05 1 1 1CES 1 +---------------------------------------------------------------------+ | Value | Content Description | |--------------|------------------------------------------------------| | | EHRS via the MCDU, e.g. if the DMU is changed on| | | the A/C. | |--------------|------------------------------------------------------| | AP | Auto Pilot Status | | 99 | (00 to 24) | | | FMGC 1 and 2 (FGC part) for Auto Pilot AP1 and AP2 | |--------------| -------------------|-------------------|------------ | | Auto Pilot | AP1 | AP2 | | | Status | Report Line EC: | Report Line EE: | Difinition: | |--------------| -------------------|-------------------|------------ | |00 | -------------------| ------------------| No Mode Act.| |--------------| -------------------|-------------------|------------ | |01 | 01.1.275.00.11 = 1 | 01.2.275.00.11 = 1|RUNWAY Mode | |--------------| -------------------|-------------------|------------ | |02 | 01.1.275.00.12 = 1 | 01.2.275.00.12 = 1|NAV Mode | |--------------| -------------------|-------------------|------------ | |03 | 01.1.275.00.13 = 1 | 01.2.275.00.13 = 1|LOC CAPTURE | | | | |Mode | |--------------| -------------------|-------------------|------------ | |04 | 01.1.275.00.14 = 1 | 01.2.275.00.14 = 1|LOC TRACK | | | | |Mode | |--------------| -------------------|-------------------|------------ | |05 | 01.1.275.00.15 = 1 | 01.2.275.00.15 = 1|Roll GO | | | | |AROUND Mode | |--------------| -------------------|-------------------|------------ | |06 | 01.1.275.00.16 = 1 | 01.2.275.00.16 = 1|HEADING Mode | |--------------| -------------------|-------------------|------------ | |07 | 01.1.275.00.17 = 1 | 01.2.275.00.17 = 1|TRACK Mode | |--------------| -------------------|-------------------|------------ | |08 | 01.1.274.00.15 = 1 | 01.2.274.00.15 = 1|PITCH TO Mode| |--------------| -------------------|-------------------|------------ | |09 | 01.1.274.00.16 = 1 | 01.2.274.00.16 = 1|PITCH GA Mode| |--------------| -------------------|-------------------|------------ | |10 | 01.1.274.00.17 = 1 | 01.2.274.00.17 = 1|V/S Mode | |--------------| -------------------|-------------------|------------ | |11 | 01.1.274.00.18 = 1 | 01.2.274.00.18 = 1|FPA Mode | |--------------| -------------------|-------------------|-------------| |12 | 01.1.274.00.19 = 1 | 01.2.274.00.19 = 1|ALT Mode | | | AND | AND | | | | 01.1.274.00.20 = 1 | 01.2.274.00.20 = 1| | |--------------| -------------------|-------------------|------------ | |13 | 01.1.274.00.19 = 1 | 01.2.274.00.19 = 1|ALT ACQ | | | AND | AND |Mode | | | 01.1.274.00.21 = 1 | 01.2.274.00.21 = 1| | 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(141)