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时间:2011-03-25 12:29来源:蓝天飞行翻译 作者:admin
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 in a specified altitude area above or below the aircraft are
 displayed. This area is selected by means of the ABOVE/N/BELOW switch
 of the ATC/TCAS control unit.
 (ABOVE : -2700 ft to +9900 ft max., N (normal) : +/- 2700 ft,BELOW :
 +2700 ft to -9900 ft max).

 The traffic indications provide a view of the situation in the
 surveillance area. The aircraft present in this area are represented
 by symbols and associated tags. The position of the symbols on the
 display enables to determine the distance (range) and the bearing in
 the airspace. Both color and shape of the symbols are used to
 discriminate traffic according to the level of threat. The tags
 indicate relative altitude and vertical trend.
 The various symbols used according to the type of intruder are
 presented below:
 (Ref. Fig. 051)

 -Other traffic for intruders with a range greater than 6NM or a vertical distance of at least +/- 1200 ft.
 -Proximate Traffic for intruders which do not enter in the Traffic Advisory (TA) or Resolution Advisory (RA) categories. Their range is within 6NM. Proximate traffic intruders and other traffic intuders can be displayed :
 1EFF : ALL 1 31-65-00Page A7 1 1 Aug 01/05 1 1 1CES 1


R  ND - TCAS Indications Figure 049
 1EFF : 1 1 1CES  ALL  1 111 31-65-00 Page A8 Feb 01/05

 

R  ND - TCAS Indications Figure 050
 1EFF : 1 1 1CES  ALL  1 111 31-65-00 Page A9 Feb 01/05

 

R  ND - TCAS Symbology Figure 051
 1EFF : 1 1 1CES  ALL  1 111 31-65-00 Page A10 Feb 01/05

 

 -permanently if the FULL TIME DISPLAY function is selected on the ATC/TCAS control unit. or
 - only when a RA or TA type intruder is detected
 -Resolution Advisory (RA) .corrective : the pilot must modify present vertical speed .preventive : the pilot must avoid certain vertical speed ranges. Trajectory correction or holding visual orders are accompanied by synthesized voice announcements generated by the TCAS computer.
 -Traffic Advisory (TA) for intruders near the aircraft, which do not represent an immediate threat but may become a collision threat. Off scale intruders are represented by a half-symbol displayed at the edge of the ND mask (Ref. Fig. 052)
 NOTE : The lower section of this mask can show different
____ configurations to display FM or TCAS messages.
 A white range ring is displayed around the aircraft symbol at 2.5 NM
 (Ref. Fig. 053)
 Only the eight most dangerous intruders can be displayed.

 (2) TCAS test A test can be initiated to check the TCAS computer. During this test the ND shows a specific image on which four intruders are displayed :
R (Ref. Fig. 054)
 **ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302,
 (Ref. Fig. 055)
 **ON A/C ALL
 -an other traffic aircraft
 -
a proximate traffic aircraft

 -
a traffic advisory aircraft

 -
a resolution advisory aircraft.


 1EFF : ALL 1 31-65-00Page A11 1 1 Aug 01/05 1 1 1CES 1


R  ND - TCAS Off Scale Intruders Figure 052
 1EFF : 1 1 1CES  ALL  1 111 31-65-00 Page A12 Feb 01/05

 

R  ND - TCAS Display Figure 053
 1EFF : 1 1 1CES  ALL  1 111 31-65-00 Page A13 Feb 01/05

 

 ND - TCAS Test Figure 054 
R 1EFF : 1 1 1CES  ALL  1 111 31-65-00 Page A14 Aug 01/05

 

 ND - TCAS Test
 Figure 055

R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 31-65-00Page A15 1201-299, 301-302, 1May 01/05 1 1 1CES 1 **ON A/C ALL


 Post SB 34-1147 For A/C 001-004,051-060,
 J. GPS Primary Function
 (Ref. Fig. 056)


R **ON A/C 106-149, 303-399, 401-499,
 (Ref. Fig. 057)
 **ON A/C ALL
 Post SB 34-1147 For A/C 001-004,051-060,
 GPS (Global Positionning System) is considered as "primary" when its A/C position is delivered with appropriate accuracy and integrity. In such a case, a cross-check with other means of navigation is no longer required and GPS position is then used for autopilot operation and display. For the GPS primary function, the ND displays the GPS approaches when appropriate and the status GPS PRIMARY or not.
 1EFF : ALL 1 31-65-00Page A16 1 1 Aug 01/05 1 1 1CES 1


R  Navigation Display - GPS Primary Function Figure 056
 1EFF : 1 1 1CES  ALL  1 111 31-65-00 Page A17 Feb 01/05

 

 Navigation Display - GPS Primary Function
 Figure 057
 
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