A320飞机维护手册 AMM 指示/记录系统 3(75)

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 1EFF : 106-149, 211-299, 301-399, 401-499, 1 31-36-00Page 86 1 1 Config-2 Aug 01/05 1 1 1CES 1 +---------------------------------------------------------------------+ | Value | Content Description | |--------------|------------------------------------------------------| | 9999 | | |--------------|------------------------------------------------------| | BLEED STATUS| Discrete and numeric coded information | | 99 | is the LH Pack Flow param. 8E.1.126.11 | | | | | 1 | LH Wing AI/V Pos. param. 29.1.001.11.18 | | | Close=0 param. 29.2.001.11.18 | | | | | 1 | ENG1 NAC. AI Pos. param. 5D.2.061.10.28 | | | Open=1 | | | | | 1 | ENG 1 PRV Pos. param. 6F.1.067.01.17 | | | Fully Closed=0 param. 6F.2.067.10.17 | | | | | 1 | ENG 1 HPV Pos. param. 6F.1.067.01.15 | | | Fully Closed=0 param. 6F.1.067.10.15 | | | | | 1 | Cross Feed V. Pos. param. 29.1.055.01.16 | | | Fully Closed=0 param. 29.2.055.01.16 | | | | | 1 | ENG 2 HPV Pos. param. 6F.2.066.01.15 | | | Fully Closed=0 param. 6F.2.066.10.15 | | | | | 1 | ENG 2 PRV Pos. param. 6F.2.066.01.17 | | | Fully Closed=0 param. 6F.2.066.10.17 | | | | | 1 | ENG.2 Nac. AI Pos. param. 5D.2.061.27 | | | Open=1 | | | | | 1 | RH Wing AI/V Pos. param. 29.1.001.00.18 | | | Closed=0 param. 29.2.001.00.18 | | | | | 99 | RH Pack Flow param. 8E.2.126.00 | | | 0 to 1.0 kg/sec | +---------------------------------------------------------------------+ | 1 | APU Bleed V. State param. 7A.1.037.01.11 | | | APU Bleed Valve Open =1 | +---------------------------------------------------------------------+

 Line 15:
R 1EFF : 106-149, 211-299, 301-399, 401-499, 1 31-36-00Page 87 1 1 Config-2 Aug 01/05 1 1 1CES 1 +---------------------------------------------------------------------+ | Value | Content Description | |--------------|------------------------------------------------------| | TAT | Total Air Tempearture | | X999 | For positive values 'N' is replaced by '0'. | | | param. 06.1.211.01 | | | 06.2.211.10 | |--------------|------------------------------------------------------| | ALT | Standard Altitude (1013mbar) | | X9999 | param. 06.1.203.01 | | | 06.2.203.10 | |--------------|------------------------------------------------------| | CAS | Computed Air Speed | | 999 | param. 06.1.206.01 | | | 06.2.206.10 | |--------------|------------------------------------------------------| | MN | Mach Number | | 999 | param. 06.1.205.01 | | | 06.2.205.10 | |--------------|------------------------------------------------------| | GW | Gross Weight | | 9999 | param. 02.1.075.00 | | | 02.2.075.00 | |--------------|------------------------------------------------------| | CG | Center of Gravity | | 999 | param. 02.1.077.00 | | | 02.2.077.00 | |--------------|------------------------------------------------------| | DMU/SW | DMU Ident Code | | XXXXXX | X = Engine Type C = CFMI, I = IAE | | | X = Engine Version 1 ...8 | | | XX = Hardware Vers. A100, A200 | | | XX = Software Version (001 ...999) | +---------------------------------------------------------------------+

R 1EFF : 106-149, 211-299, 301-399, 401-499, 1 31-36-00Page 88 1 1 Config-2 Aug 01/05 1 1 1CES 1

 INTENTIONALLY BLANK

R 1 1

31-36-00Page 89
1 1 Config-2 Aug 01/05 1 1 1CES 1

 **ON A/C 151-199, 201-210,

 +----------------------------------------------------------------------+ | Log. | Item | Description of Function Item |Prog. | | No. | No. | |MCDU | |------|-------|------------------------------------------------|------| | | | The DMU uses the FWC flight phases (parameter | | | | | 26.1.126.01 bit 11 to 14 to perform the AIDS | | | | | flight phases as shown in Table 11) | | | | | | | | | A | Parameter | | | | | | | | | B | Logic algorithm | | | | | | | | | B.1 | ALT 1 = 10000 ft | AI/C | | | | | | | | B.2 | ALT 2 = 10000 ft | AI/C | | | | | | | | B.3 | IVV 1 = 400 ft/min | AI/C | | | | | | | | B.4 | IVV 2 = -400 ft/min | AI/C | | | | | | | | B.5 | IVV 3 = 400 ft/min | AI/C | |----------------------------------------------------------------------| | AI = Programmable by Airbus Industrie | | C = Programmable by Customer | +----------------------------------------------------------------------+
 Flight Phase Detection Logic - Table 12
 D. General AIDS Function The AIDS functionality is divided into the following major functions:
 -AI AIDS Reports,
 -Smart Access Recorder (SAR) Function,
 -Digital AIDS Recorder (DAR) Function,
 -Input/Output User Function,
 E. AI AIDS Reports The AI AIDS Reports are AIDS monitor functions which have fixed trigger mechanism, fixed data collection and fixed output formatting. These reports perform the basic aircraft monitoring functions which are required. These monitoring functions collect parameters for trend analysis of the engines, the aircraft and the APU. Aircraft data are also collected and automatically output during times of aircaft operational anomalies (e.g. engine over-temperature).
 1EFF : 151-199, 201-210, 1 31-36-00Page 90 1 1 Config-2 Aug 01/05R 1 1 1CES 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 3(75)