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 G. VOR (Ref. Fig. A009) The PFD uses the Marker information from the VOR bus. The CAPT PFD can only display marker indications from the VOR 1 and the F/O PFD those from VOR 2.
 H. DME (Ref. Fig. A010) The PFD displays the DME distance when the DME station is co-located to an ILS station. The PFD displays DME distance which is delivered on the FMGC-EIS bus. The CAPT PFD can only display DME1 data, when the F/O PFD displays DME2 data.
 J. TCAS (Ref. Fig. A011) The PFD display the forbidden vertical speeds on the vertical speed scale. The DMC1 and DMC3 receive the channel 1 parameters (CAPT PFD). The DMC2 receives the channel 2 parameters (F/O PFD). In case of channel invalidity, the related PFD displays the red TCAS flag.
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R  EIS Acquisitions : FCU Figure A008 
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R  EIS Acquisitions : VOR Figure A009
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R  EIS Acquisitions : DME Figure A010
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R  Interface with TCAS Figure A011
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 NAVIGATION DISPLAY (ND) - DESCRIPTION AND OPERATION
___________________________________________________
 1. General
_______
 The Navigation Display (ND) is normally presented in front of each pilot, on the inner display unit. It provides medium term flight information necessary to locate the aircraft with respect to navigation aids, map data and Flight Management System flight plans.
 2. Component location
__________________

R **ON A/C 106-149, 303-399, 401-499,
 (Ref. Fig. 001)
 **ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302,
 (Ref. Fig. 002)
 **ON A/C ALL
 -------------------------------------------------------------------------------FIN FUNCTIONAL DESIGNATION PANEL ZONE ATA REF
 -------------------------------------------------------------------------------3WT1 DU-ND, CAPT 3VU 211 31-60-00 3WT2 DU-ND, F/O 5VU 212 31-60-00 1WT1 DMC-1 85VU 127 31-60-00 1WT2 DMC-2 86VU 128 31-60-00
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 INTENTIONALLY BLANK

R 1 1

31-65-00Page 2
1 1 May 01/01 1 1 1CES 1

 Navigation Display - Navigation Component Location
 Figure 001

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1

 Navigation Display - EIS Component Location
 Figure 002

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 A. Color Choice Seven different colors are used for EFIS system, plus two particular colors for sky and earth (blue and brown). An exhaustive list of all the ND indications with their color assignment is given in the following pages. The general rules for color choice below are followed:
 -red : used for the flight envelope limit indications, and for the failure indications concerning the various sensors.
 -amber : used for information or messages requiring attention but not quick action or decision.
 -yellow : used for aircraft references (e.g.: aircraft symbol, lubber line...)
 -white :
 used for scales, for VOR indications.

 -green : used for current values (e.g.: ground speed, track). cyan : used for selectable values (e.g.: selectable speed, armed mode, tuned navaids), and units (e.g.: NM).
 -magenta :
 used for ILS. (LOC and GLIDE SLOPE) deviations, and optional
 information displayed on the map: VOR-D, NDB, ARPT,...

 (1) List of elements per color
 (a) Red :
 -flags
 -NAV receiver unserviceable (VOR, ADF2,...)
 -WXR: precipitation 12-50 mm/hr. failure messages corresponding to the loss of WXR image.
 (b) Amber :
 -caution messages (e.g. CHECK HDG) or message requiring crew attention
 -constraint (altitude, speed,...) on the active flight plan, and which cannot be satisfied (because the A/C is too high, or too low...)
 -WXR failure messages with WXR image not removed.
 (c) Yellow :
 -fixed reference symbols (A/C position, A/C heading reference)
 -Temporary flight plan, OFFSET or EOSID when not active : way points and legs (in dotted line except for EOSID in continuous line)
 -WXR: precipitation 4 to 12 mm/hr
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 (d) Magenta :
 -LOC and glide deviation
　
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