
Av. Kit Install. Manual
190-00066-02 Rev. J
Page 14
4.2
INSTALLATION CONFIGURATION
4.2.1 SELECTED COURSE CALIBRATION
Select the test page displaying the selected course input. Using an extremely
accurate input source, input 150° to the GPS 165. The input course will indicate
close to 150° and a Calib? field will appear in the lower right corner. Selecting
the Calib? field will calibrate the GPS 165 to match the input source. Verify
OBS operation by checking that the bearing displayed on the GPS 165 is within
2° of the selected bearing. Do this for every multiple of 30° around the OBS.
4.2.2 I/O CHANNEL 1
Select the I/O CHANNEL 1 Test Page. Change the selectable input and output to
match that of the installed equipment. The available options are:
Input:
Field
Description
off
No units connected to Channel 1 input
icarus-alt
Serial altitude received from:
Icarus, Model 3000, Mode C Serializer
shadin-alt
Serial altitude received from:
Shadin 9000T Serializer System (Non-TSO'd)
Shadin 9200T Series Serializer System (Non-TSO'd) Shadin
8800T Series Encoder System (TSO'd)
shadin-fuel
Fuel information received from:
Shadin 91204XT Digital Fuel Management System (TSO'd)
Shadin 91053XT Digital Fuel Management System (TSO'd)
arnav/ei-fuel Fuel information received from:
Arnav, Model FC-10, Fuel Computer (TSO'd)
Arnav, Model FT-10, Fuel Totalizer (TSO'd)
Electronics International, Model FP-5L, Fuel Flow Com-
puter (non-TSO'd)
shadin-fac
Fuel/Air data information received from:
Shadin, Model 962801 Fuel/Airdata Computer (TSO'd)
Note: Verify with manufacturer of data input device that unit supports GARMIN
interface.
Output: Field
Description
off
No units connected to Channel 1 input
aviation
Serial position, velocity and navigation data to:
Argus, Model 3000, Moving Map
Argus, Model 5000, Moving Map
Argus, Model 7000, Moving Map
Stormscope, Series II with Navaid, Moving Map
Shadin, 91204X[T] Digital Fuel Management System (TSO'd)
Shadin, 91053X[T] Digital Fuel Management System (TSO'd)
Shadin, 962801 Fuel/Airdata Computer (TSO'd)
Содержание GPS 165
Страница 22: ...Av KitInstall Manual 190 00066 02 Rev J Page22 FIGURE 1 1 PINOUT DEFINITION 37 PIN DSUB ...
Страница 23: ...Av Kit Install Manual 190 00066 02 Rev J Page 23 FIGURE 1 2 PINOUT DEFINITION 26 PIN HD DSUB ...
Страница 24: ...Av KitInstall Manual 190 00066 02 Rev J Page24 FIGURE 1 3A INTERCONNECT SCHEMATIC ...
Страница 25: ...Av Kit Install Manual 190 00066 02 Rev J Page 25 FIGURE 1 3B INTERCONNECT SCHEMATIC ...
Страница 26: ...Av KitInstall Manual 190 00066 02 Rev J Page26 FIGURE 1 3C INTERCONNECT SCHEMATIC ...
Страница 28: ...Av KitInstall Manual 190 00066 02 Rev J Page28 FIGURE 3 1 REMOTE BATTERY PACK ASSEMBLY ...
Страница 29: ...Av Kit Install Manual 190 00066 02 Rev J Page 29 FIGURE 3 2 GA 56 ANTENNA INSTALLATION ...
Страница 30: ...Av KitInstall Manual 190 00066 02 Rev J Page30 FIGURE 3 3 FLANGE MOUNT GA 56 ANTENNA INSTALLATION ...
Страница 31: ...Av Kit Install Manual 190 00066 02 Rev J Page 31 FIGURE 3 4 COAX CABLE INSTALLATION ...
Страница 32: ...Av KitInstall Manual 190 00066 02 Rev J Page32 FIGURE 3 5 GPS 165 FACE DIMENSIONS ...
Страница 33: ...Av Kit Install Manual 190 00066 02 Rev J Page 33 FIGURE 3 6 AVIATION RACK INSTALLATION ...
Страница 40: ...FIGURE C 2 INTERCONNECT SCHEMATIC Av Kit Install Manual 190 00066 02 Rev J Page 40 ...
Страница 41: ...FIGURE C 3 SWITCH ANNUNCIATOR LAYOUT Av Kit Install Manual 190 00066 02 Rev J Page 41 ...
Страница 43: ...Av Kit Install Manual 190 00066 02 Rev J Page 43 ...