R 1EFF : 001-049, 051-099, 101-105, 151-158, 1 31-37-73Page 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| |----|------|-----------------------------------------|------|---------| |6004| | 'X01' is not zero (once per leg only). | | | |6005| | Each time when a Eng. Cruise Rep. <01> | | | | . | | was generated by this logic, the num-| | | | . | | ber 'X01' are decremented until zero is | | | | . | | reached. | | | | . | | | | | |600X| | The start value of 'X01' is programmable| | | | | | | | | | | | In case of change engine serial number, | | | | | | 'X01' is automatically set to 5. | | | | | | | | | | |6.1 | Number 'X01' for consecutive reports up | | | | | | to 9. | C | T22/T23 | |----|------|-----------------------------------------|------|---------| |7000|7 | In case the ENGINE DIVERGENCE REPORT | | | | | | <09> was generated, the stable frame | | | | | | search logic for the ENGINE CRUISE REP. | | | | | | <01> is started immediately independent | | | | | | of the best stable frame logic and the | | | | | | report is generated with code 7000. | | | | | | | | | | | | In case that there are further Diver-| | | | | | gence Reports are generated before a | | | | | | Cruise Report is initiated, it is only | | | | | | be one Eng. Cruise Report. | | | |----|------|-----------------------------------------|------|---------| |8100|8.1 | ACARS MU uplink request with IMI 'REQ01'| | | | | | The report <01> is immediately generated| | | | | | and transmitted to the ACARS MU. | | | |----|------|-----------------------------------------|------|---------| |8200|8.2 | ACARS MU uplink request with IMI 'G01' | | | | | | The report <01> is generated as soon as | | | | | | stable frame criteria are met, i.e. the | | | | | | DMU is immediately start searching for | | | | | | stable frame criteria independing from | | | | | | any other logic. | | | |----------------------------------------------------------------------| | AI = Programmable by Airbus Industrie | | C = Programmable by Customer | +----------------------------------------------------------------------+

R
R 1EFF : 001-049, 051-099, 101-105, 151-158, 1 31-37-73Page 16 1201-209, 1May 01/05 1 1 1CES 1

R **ON A/C 106-149, 211-299, 301-399, 401-499,

 (1) Engine Cruise Report Data Field Description <01> (Engine Type CFMI with Advanced EVMU)
 +---------------------------------------------------------------------+ | Value | Content Description | |--------------|------------------------------------------------------| | ESN | Engine Serial Number | | 999999 | (000000 to 999999) | | | ECU Engine 1 7C.1.046.01 digit 3, 2, 1 | | | 7C.1.047.01 digit 6, 5, 4 | | | Engine 2 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 and Engine 2 | |--------------|------------------------------------------------------| | ERT | Engine Running Time | | 99999 | (00000 to 65536 hours) | | | ECU 7C.1.050.01 Engine 1 | | | 7C.2.050.10 Engine 2 | |--------------|------------------------------------------------------| | ECYC | Engine Cycle | | 99999 | (00000 to 99999) | | | DMU Engine 1 | | | Engine 2 | |--------------|------------------------------------------------------| | AP | Auto Pilot Status | | 99 | Number of respective status (00 to G8) | | | FMGC 1 and 2 (FGC part) for Auto Pilot AP1 and AP2 | | | | | | XX Auto Pilot Modes: | | | || | | | ||__Lateral Modes: 0 = NO MODE | | | | 1 = HEADING | | | | 2 = TRACK | | | | 3 = NAV | | | | 4 = LOC CAPTURE | | | | 5 = LOCK TRACK | | | | 6 = LAND TRACK | | | | 7 = RUNWAY | | | | 8 = ROLL GO AROUND | | | | | | | |__Longitudinal Modes: 0 = NO MODE |
R 1EFF : 106-149, 211-299, 301-399, 401-499, 1 31-37-73Page 17 1 1 Aug 01/05 1 1 1CES 1 +---------------------------------------------------------------------+ | Value | Content Description | |--------------|------------------------------------------------------| | | 1 = PITCH G/A | | | 2 = PITCH TO | | | 3 = G/S TRACK | | | 4 = G/S CAPTURE | | | 5 = V/S | | | 6 = FPA | | | 7 = ALT | | | 8 = ALT ACQ | | | 9 = OPEN CLB | | | A = OPEN DES | | | B = IM CLB | | | C = IM DES | | | D = CLB | | | E = DES | | | F = FINAL DES | | | G = EXPEDITE | | | | | | Parameter for AP1 | Parameter for AP2 | | | Report Line EC: | Report Line EE: |Definition: | | | -------------------|-------------------|------------ | | | / | / |No Mode Act. | | | -------------------|-------------------|------------ | | | 01.1.275.00.11 = 1 | 01.2.275.00.11 = 1|RUNWAY Mode | | | -------------------|-------------------|------------ | | | 01.1.275.00.12 = 1 | 01.2.275.00.12 = 1|NAV Mode | | | -------------------|-------------------|------------ | | | 01.1.275.00.13 = 1 | 01.2.275.00.13 = 1|LOC CAPTURE | | | | |Mode | | | -------------------|-------------------|------------ | | | 01.1.275.00.14 = 1 | 01.2.275.00.14 = 1|LOC TRACK | | | | |Mode | | | -------------------|-------------------|------------ | | | 01.1.275.00.15 = 1 | 01.2.275.00.15 = 1|Roll GO | | | | |AROUND Mode | | | -------------------|-------------------|------------ | | | 01.1.275.00.16 = 1 | 01.2.275.00.16 = 1|HEADING Mode | | | -------------------|-------------------|------------ | | | 01.1.275.00.17 = 1 | 01.2.275.00.17 = 1|TRACK Mode | | | -------------------|-------------------|------------ | | | 01.1.274.00.15 = 1 | 01.2.274.00.15 = 1|PITCH T/O | | | | |Mode | | | -------------------|-------------------|------------ | | | 01.1.274.00.16 = 1 | 01.2.274.00.16 = 1|PITCH GA Mode| | | -------------------|-------------------|------------ |
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM 指示/記錄系統 4(163)