-------------------------------------------------------------------------------| TITLE | BIT No. | VALUE | MEANING | |---------|---------|-------|-------------------------------------------------| | | 1 | | | | | 2 | | 275 : LIGHT STATUS | | | 3 | | | | LABEL | 4 | | Refresh rate 250 ms | | | 5 | | | | | 6 | | | | | 7 | | | | | 8 | | | |---------|---------|-------|-------------------------------------------------| | | 9 | | DMC 1 ( 1 DMC 2 ( 0 DMC 3 ( 1 | | SDI | 10 | | ( 0 ( 1 ( 1 | |---------|---------|-------|-------------------------------------------------| | | 11 | | SPARE | | | 12 | | ENG | | | 13 | | BLEED | | | 14 | | PRESS | | | 15 | | HYD | | | 16 | | ELEC | | | 17 | | FUEL | | | 18 | | APU | | | 19 | | COND | | DATA | 20 | | DOOR BIT 1 : LIGHT ON | | | 21 | | F/CTL | | | 22 | | WHEEL | | | 23 | | SPARE | | | 24 | | SPARE | | | 25 | | SPARE | | | 26 | | STS | | | 27 | | CLR | | | 28 | | SPARE | | | 29 | | SPARE | |---------|---------|-------|-------------------------------------------------| | SSM | 30 | | 0 ) FW 0 ) FT 1 ) NCD 1 ) NORMAL | | | 31 | | 0 ) 1 ) 0 ) 1 ) | |---------|---------|-------|-------------------------------------------------| | PARITY | 32 | | | -------------------------------------------------------------------------------
1EFF : ALL 1 31-56-00Page 14 1 1 Feb 01/98 1 1 1CES 1 ELECTRONIC INSTRUMENT SYSTEM (EIS) - DESCRIPTION AND OPERATION

______________________________________________________________
 1. General
_______
 The EIS (Electronic Instrument System) presents on Display Units (DUs):

 -EFIS (Electronic Flight Instrument System) information, (i.e. flight
 parameters and navigation data).

 -ECAM (Electronic Centralized Aircraft Monitor) information, (Ref.
 31-50-00) The layout of the 6 DUs and the breakdown of the information displayed on them is presented as follows: (Ref. Fig. 001)
 -
2 DUs are installed side by side in front of each pilot. They display flight and navigation data. On each main instrument panel, in normal configuration, the outer DU will be allocated to the Primary Flight Display (PFD) function, and the inner DU to the Navigation Display (ND) function. Each pilot is given the possibility to display ECAM information instead of navigation information on its inner DU, in order to cover ECAM DU failure cases.

 -
2 DUs are installed on the center instrument panel, one above the other. They display ECAM information.

 A.
 Information Presented on EFIS DUs (Ref. Fig. 002) The EFIS DUs enable display for the crew of flight path control and navigation data. It includes the primary flight dispplay (PFD) and the navigation display (ND). The PFD image presents the main information necessary for the control of the A/C arranged in the basic T configuration.

 Each pilot has at his disposal two CRT display units, one PFD and one ND, on which is displayed all the information that is usually presented by the following instruments:
 -Attitude Director Indicator
 -Horizontal Situation Indicator
 -Mach-Airspeed Indicator
 -Altimeter Indicator
 -Vertical Speed Indicator
 -Radio Altimeter Indicator
 -Weather Radar Indicator
 -Marker Beacon Indicator lights
 -Flight Mode Annunciator (autopilot/flight director modes).
 (1) The instrument Primary Flight Display (PFD) displays all the primary flight indications necessary for short-term aircraft control (hence its name), that is:
 -attitude (pitch, roll), lateral acceleration/side slip indication,
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 31-60-00Page 1 1201-299, 301-302, 1Config-1 May 01/05 1 1 1CES 1

 Presentation by Display Units in Normal Configuration
 Figure 001

R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 31-60-00Page 2 1201-299, 301-302, 1Config-1 May 01/05 1 1 1CES 1

 PFD and ND Image
 Figure 002

R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 31-60-00Page 3 1201-299, 301-302, 1Config-1 May 01/05 1 1 1CES 1

 -attitude protections, side stick orders on the ground,
 -flight path angle and drift angle (on pilot's request),
 -guidance (flight director or flight path orders),
 -magnetic heading and selected heading or track, plus A/C drift angle,
 -airspeed and associated selections (manual or automatic), plus all speed limits (flight envelope protection limits, high lift devices retraction/extension speeds, etc...),
 -baro altitude and associated selections (manual or automatic) and baro reference setting, plus flight profile deviation,
 -vertical speed,
 -TCAS indication (up and down advisories)
 -radio altitude and Decision Height,
　
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 7(4)