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时间:2011-04-12 10:04来源:蓝天飞行翻译 作者:航空
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 (d)  
Current track is indicated by a track line on both the expanded format and the full rose format.

 

 (2)  
Selected VOR course is displayed by a pointer which rotates around the fixed airplane symbol. This selected course is also displayed digitally in the upper, right corner.

 (3)  
Course deviation indication is provided by a deviation bar displaced on a dot scale. The dot scale is orthogonal to the selected course pointer and rotates about the airplane reference symbol.

 (a)  
The course deviation bar is displaced from the center of the pointer to indicate the difference between the input VOR omnibearing and the selected course. Full scale deflection corresponds to 11.6 degrees course deviation.

 (b)  
The polarity of the deflection results in a "fly to" indication to achieve the selected course.

 

 (4)  
A TO/FROM indication is provided by the label "TO" or "FROM" for the expanded format, and by a pointer for the full rose format.

 (5)  
The upper, right corner contains the decoded identifier for the tuned VOR if a valid ground identifier is received.


 (a)  If a valid identifier is not received, then the identifier will be replaced by the tuned frequency.
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

MAG/TRU ANNUNCIATOR SOURCE
SOURCE GROUND SPEED FREQUENCY

SELECTED
COURSE WIND SPEED AND DIRECTION
DME DISTANCE
COMPASS ROSE OTHER
SELECTED
COURSE HEADING
WEATHER RADARTRACK RETURNLINE
RANGE  RESOLUTION ADVISORY
TO/FROM ANNUNCIATOR
RADIO SELECTION IDENT/FREQ RADIO DME DISTANCE COURSE AIRPLANE DME DISTANCEDEVIATION
REFERENCE
VOR Mode - Expanded
Figure 15

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
E24220
A
747-400
MAINTENANCE MANUAL

SOURCE ANNUNCIATOR
GROUND SPEED
SELECTED COURSE WIND SPEED

DME AND DIRECTION DISTANCE
DRIFT ANGLE POINTER
TO/FROM
ADF/VOR POINTER
POINTER

SELECTED COURSE
COURSE
DEVIATION AIRPLANE REFERENCE
RADIO SELECTION
RADIO IDENT/FREQ SELECTION IDENT/FREQ
DME DME
TO/FROMDISTANCE DISTANCE
ANNUNCIATOR
VOR Mode - Full
Figure 16

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

IRS HEADING

LEFT
VOR
ADF
VOR
VOR Mode Failure Flags
Figure 16A

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 ú  08  Page 68
 ú  Feb 10/92 

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

 (b)  
The selected course is displayed below the identifier/frequency field.

 (c)  
The distance received from a DME co-located with the tuned VOR is displayed below the selected course field.


 (6)  
The source annunciation (VOR L,R) for the radio data is displayed at the upper, right corner between the heading readout and the identifier/frequency display.

 (7)  
The lower corners contain the ADF/VOR radio navigation aid information.
 
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