Garmin GPSMAP 800 Series Pilot'S Manual Addendum Download Page 10

1.4  AURAl AleRTS

A TA consists of a displayed traffic symbol (solid yellow circle) and an aural alert.  

The aural alert announces “traffic”, followed by the intruder aircraft’s position, altitude 
relative  to  own  aircraft  (“high”,  “low”,  or  “same  altitude”),  and  distance  from  own 
aircraft; e.g. “traffic, 12 o’clock, high, 3 miles”.

1.5  Self-TeST

The  GTS  8XX  automatically  performs  a  self-test  upon  power  up.    The  self-test 

checks internal parameters and calibrates components of the GTS 8XX.  The self-test 
can also be initiated by the user during normal operation.

Check for the following test criteria on the Traffic Page during power-up:

•  If the GTS 8XX passes the power-up test; and the aircraft both has a squat 

switch and is on the ground, the Standby Screen is displayed (Figure 2).

•  If the GTS 8XX passes the power-up test and the aircraft both has a squat 

switch and is airborne, the Traffic Page is displayed on the 6-nm display range 
and in the normal altitude display mode.

•  If the GTS 8XX passes the power-up test and the aircraft does not have a squat 

switch, the Standby Screen is displayed (Figure 2).

•  If the GTS 8XX fails the power-up test (as indicated by a FAILED screen), 

the GTS 8XX is inoperable, see the GTS 8XX Installation Manual for detailed 
information on Failure Response.

 

NOTE: 

The FAILED message is displayed when the system detects an error 

that prohibits further traffic display operation.

 

NOTE:   

When  the  system  is  in  standby,  the  GTS  8XX  does  not  transmit, 

interrogate, or track intruder aircraft.

400/500 Pilot’s Guide Addendum for GTS 8XX Interface

190-00140-78  Rev. A 

4

GTS 8XX Interface

Summary of Contents for GPSMAP 800 Series

Page 1: ...400 500 Series GTS 8XX Interface Pilot s Guide Addendum...

Page 2: ......

Page 3: ...r Taipei County Taiwan Tel 886 02 2642 9199 Fax 886 02 2642 9099 Web Site Address www garmin com Except as expressly provided herein no part of this manual may be reproduced copied transmitted dissemi...

Page 4: ...should be compared with other navigation sources WARNING For safety reasons 4XX 5XX operational procedures must be learned on the ground WARNING The United States government operates the Global Positi...

Page 5: ...on is subject to the following two conditions 1 this device may not cause harmful interference and 2 this device must accept any interference received including interference that may cause undesired o...

Page 6: ...Between Standby and Operating Modes 6 1 8 Traffic Page 7 1 9 Traffic Page Display Range 7 1 10 Altitude Display Mode 8 1 11 Traffic Warning Window 10 1 12 Map Page Traffic Banner 10 1 13 Configuring T...

Page 7: ...t computes the responding aircraft s range bearing relative altitude and closure rate The GTS 8XX then determines the advisory status of the target and sends the location information and alert status...

Page 8: ...gh 3 miles Out of Range Traffic Advisory This solid yellow half circle appears on the outer range ring under the same conditions and has the same urgency as a TA Its appearance differs from the TA onl...

Page 9: ...less than 30 seconds of vertical and horizontal separation Or Intruder range is within 0 55 nm and vertical separation is within 800 feet B No Intruder closing rate is less than 20 seconds Table 2 TA...

Page 10: ...switch and is on the ground the Standby Screen is displayed Figure 2 If the GTS 8XX passes the power up test and the aircraft both has a squat switch and is airborne the Traffic Page is displayed on...

Page 11: ...teria are identical to the power up self test although the user initiated test is concluded by an aural pass fail message NOTE A user initiated test can only be performed when in standby or failed mod...

Page 12: ...S 8XX switches out of standby into the 6 nm display range NOTE The GTS 8XX will automatically switch out of standby 8 to 10 seconds after takeoff which is determined by ground speed or by a transition...

Page 13: ...splayed if more than one TA with no bearing info is active while the TA of most immediate threat is displayed in text below the banner Figure 4 Traffic Page Orientation Source Traffic Advisory with no...

Page 14: ...ging the Altitude Display Mode 1 From the Traffic Page press the small right knob to activate the cursor and highlight the current mode Figure 6 2 Turn the small right knob to cycle through the option...

Page 15: ...when using the small right knob Figure 6 Unrestricted UNR Mode Selected Altitude Display Mode 3 Press the small right knob to turn the cursor off after the selection is made 400 500 Pilot s Guide Adde...

Page 16: ...age NOTE TheTrafficWarningWindow is disabled when the aircraft ground speed is less than 30 knots or when an approach is active Figure 7 Traffic Warning Window 1 12 Map Page Traffic Banner A Traffic b...

Page 17: ...ll right knob to select the Map Page 2 Press the MENU Key to display the Page Menu 3 Turn the small right knob to select Setup Map 4 Press the ENT Key The flashing cursor highlights the GROUP field 5...

Page 18: ...NU Key to display the Page Menu 3 Turn the small right knob to select Change Fields 4 Press the ENT Key 5 Turn the large right knob to select one of the three fields 6 Turn the small right knob to sel...

Page 19: ...n and panning the map display 1 Press the small right knob to activate the panning target pointer Figure 11 Figure 11 Panning the Map Display 2 Turn the small right knob clockwise to move up or counte...

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Page 22: ...U K p 44 0 870 8501241 f 44 0 870 8501251 Garmin Corporation No 68 Jangshu 2nd Road Shijr Taipei County Taiwan p 886 2 2642 9199 f 886 2 2642 9099 www garmin com Garmin International Inc 1200 East 15...

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