Garmin GPS 500, Руководство по установке

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500 SERIES INSTALLATION MANUAL Page 5-3
190-00181-02 Rev Q
DATA OUT
Selection Description
Off
No unit(s) connected to ARINC 429 output
ARINC 429 Standard ARINC 429 output data (non-GAMA).
GAMA 429
ARINC 429 data as defined by the General Aviation Manufacturers’
Association (GAMA) General Aviation Subset, 2
nd
Edition . The output
data includes navigation and flight plan information to the following
systems:
Garmin GAD 42 Interface Adapter
Bendix/King EFS 40/50
Sandel SN3308
Collins EFIS 84
Garmin GTX 330
Certain other versions of Collins EFIS may also be compatible with this
format.
GAMA 429
Graphics ARINC 429 data as defined by the GAMA General Aviation Subset, 2
nd
Edition including GAMA Graphics Protocol ‘A’. This format outputs
intersection symbols as generic waypoint symbols. The output data
includes navigation and flight plan information (including graphical
representation of flight plan procedures) to the following EFIS systems:
Honeywell Primus 1000
GAMA 429
Graphics w/Int ARINC 429 data as defined by the GAMA General Aviation Subset, 2
nd
Edition including GAMA Graphics Protocol ‘A’. The output data
includes navigation and flight plan information (including graphical
representation of flight plan procedures).
GAMA 429
Pro Line 21 ARINC 429 data as defined by the GAMA General Aviation Subset, 2
nd
Edition . The output data includes navigation and flight plan information
to the following EFIS systems:
Collins Pro Line 21
GAMA 429 Sextant ARINC 429 data as defined by the GAMA General Aviation Subset, 2
nd
Edition . The output data includes navigation and flight plan information
to the following EFIS systems:
Sextant SMD 45
SDI
Selection Description
Common
Common long-range navigator (only 429 data with SDI=0 is used)
LNAV 1 Number 1 (Pilot) long-range navigator. Only 429 data with SDI=0 or
SDI=1 is used.
LNAV 2
Number 2 (Copilot) long-range navigator. Only 429 data with SDI=0
or SDI=2 is used.
5.2.2 MAIN RS-232 CONFIG Page
Select the MAIN RS-232 CONFIG Page (see Figure 5-2).
If necessary, change the selectable RS-232 inputs and/or
outputs to match that of the equipment installed in the
aircraft.
Figure 5-2. MAIN RS-232 CONFIG Page