When STD baro setting is selected on FCU, standard altitude
 (label 203) from ADIRU 1 is used.
 When QFE baro setting is selected on FCU (assuming QFE option
 activated), the altitude is computed:

 -
during take off, using standard altitude (label 203) from ADIRU 1 and landing elevation,

 -
during approach, using standard altitude (label 203) from ADIRU 1 and QNH baro correction entered by the crew via the MCDU. On the MCDU, a prompt comes into view adjacent to the line key related to QNH information for input when < 180 NM from destination. (Ref. Fig. 017) Other aircraft inputs include aircraft heading (from the IR), roll attitude (from IR) and flight path angle (Gamma, derived by the Enhanced GPWC).

 2 Control Inputs
_ Installations provide discrete terrain display select pushbutton switches (TERR ON ND) in the cockpit for each display. These are momentary-action pushbutton switches that are processed by the Enhanced GPWS input processing and signal selection block as input to display control logic. Additionally, for aircraft with predictive windshear radar capability (if WR/PWS installed), a windshear override boolean is computed using alert level bits from label 077 on WXR hazard bus for the display control logic.
 **ON A/C 105-105,
 (Ref. Fig. 004)
 **ON A/C 001-049, 051-099, 101-104, 151-199, 201-228, 301-302,

 Post SB 34-1147 For A/C 001-004,051-060,
 Post SB 34-1193 For A/C 001-049,051-060,101-104,

 (Ref. Fig. 004A)
 **ON A/C 001-049, 051-099, 101-105, 151-199, 201-228, 301-302,
 Post SB 34-1193 For A/C 001-049,051-060,101-104,
 This boolean allows the Enhanced GPWC to manage priority between Enhanced GPWC alerts and PWS alerts. The installation requires input of cockpit-selected range scales provided by the FCU for each ND.
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 34-48-00Page A15 1201-228, 301-302, 1Config-1 Aug 01/05 1 1 1CES 1

 (b)
 Local Terrain Processing The local terrain processing block extracts and formats local topographic data and terrain features from the related data bases creating a set of digital elevation matrix overlays for use by the terrain threat detection and display processing functions. Additionally, data for the nearest runway are also extracted for use by the terrain threat detection and display processing functions. Processing for each topographic data base and the runway data base are described in the following sub-sections.

 (c)
 Terrain Threat Detection The terrain threat detection and display processing block performs the threat analysis on the terrain data within computed caution and warning envelope boundaries below and forward of the aircraft path. Results of these threat assessments are combined with background terrain data and data for the nearest runway and formatted into a terrain display image which can be displayed on

 1_ Terrain Surface Data
 Local terrain processing of topographic surface data updates a
 set of digital elevation matrix overlays that are positioned
 with respect to aircraft position. Each matrix element
 contains the highest terrain altitude with respect to mean sea
 level in that element area. Elements where terrain data are
 not available are marked invalid. These unknown data are
 displayed in magenta low density on ND whatever the altitude.
 2_ Obstacle Data
 In addition to terrain surface data, provisions are made for
 future use of an obstacle data base providing obstacle data in
 the vicinity of major airports. Local terrain processing will
 update a dedicated overlay within the digital elevation matrix
 overlays with local obstacle altitude data.
 3_ Nearest Runway Data
 Data for the nearest runway are extracted and processed for
 use by the terrain threat detection and display processing
 functions. Data are extracted from the same airport data base
 used by the Terrain Clearance Floor functions (Ref. para.
 D.(2)). This data base contains data on all hard-surface
 runways 3500 ft. or more in length with published coordinates.
 The contents of the data base are processed by the local
 terrain processing into nearest runway center position,
 nearest runway threshold position, and nearest runway altitude
 for use by the Enhanced GPWS. These data are updated when the
 terrain threat detection and display processing functions are
 performed.

R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 34-48-00Page A16 1201-228, 301-302, 1Config-1 Aug 01/05 1 1 1CES 1 Navigation Display in place of the weather image. In the event of terrain caution or warning conditions, a specific audio alert is triggered and the terrain display image is enhanced to highlight each of the types of terrain threats.
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM NAVIGATION 導航4(27)