Garmin G5 Electronic Flight Instrument Part 23 AML STC Installation Manual 190-01112-10Rev. 19

Page 144

5.12 G5 (ADI) with GPS/VHF Navigator

Figure 5-14 G5(ADI) with GPS/VHF Navigator

Like E Mag System for redundancy

Page D-4 GTN 625/635/650 TSO Installation Manual Rev. C 190-01004-02

GTN 650

P1001

1

2140

2

4160

MAIN OBS ROTOR C

MAIN OBS STATOR DMAIN OBS STATOR E GND

MAIN OBS STATOR FMAIN OBS STATOR G GND

MAIN OBS ROTOR H GND

4968

MAIN LATERAL +LEFTMAIN LATERAL +RIGHT

1130

MAIN +TO OUTMAIN +FROM OUT

5069

MAIN LATERAL +FLAG OUTMAIN LATERAL -FLAG OUT

5170

MAIN VERTICAL +FLAG OUTMAIN VERTICAL -FLAG OUT

1231

MAIN VERTICAL +UP OUTMAIN VERTICAL +DOWN OUT

s

s

s

s

s

s

s

s

NAVIGATIONINDICATOR

OBS RESOLVER {H/A}OBS RESOLVER {C}

OBS RESOLVER {D}OBS RESOLVER {E}

OBS RESOLVER {F}OBS RESOLVER {G}

CDI+ LCDI+ R

+TO FLAG+FROM FLAG

NAV+ FLAGNAV- FLAG

G/S- FLAGG/S+ FLAG

+ UP+ DOWN

NAV/GPS

AIRCRAFT POWERAIRCRAFT POWER

ESSENTIAL BUS22 AWG2019

AIRCRAFT GNDAIRCRAFT GND 78

77 22 AWG AIRCRAFTGROUND

LIGHTING BUS 1 HILIGHTING BUS 1 LO TO AIRCRAFT

LIGHTING BUS

1817

LIGHTING BUS 2 LOLIGHTING BUS 2 HI 61

42

AUDIO PANEL

COM 1 MIC AUDIO HICOM 1 MIC KEY OUT

COM 1 AUDIO HICOM 1 AUDIO LO

NAV 1 AUDIO HINAV 1 AUDIO LO

500 VOR/LOC AUDIO OUT HI500 VOR/LOC AUDIO OUT LO

P10041617

MIC AUDIO IN LO

COM MIC 1 KEYCOM MIC 1 AUDIO IN HI

500 COM AUDIO LO500 COM AUDIO HI 7

18

511

20

P1003

AIRCRAFT POWERAIRCRAFT POWER 43

30

AIRCRAFT GNDAIRCRAFT GND 38

37

44

40

ESSENTIAL BUS

AIRCRAFT POWER

AIRCRAFT GND

COM

20 AWG (5A C/B, 28VDC)18 AWG (10A C/B, 14 VDC)

AIRCRAFTGROUND

20 AWG (5A C/B, 28VDC)18 AWG (10A C/B, 14 VDC)

P1006GPS/WAASANTENNA

P1007COM

ANTENNAP1008

NAVANTENNA

TRANSPONDER

RS-232 OUT 1RS-232 IN 1GROUND

s

27RS-232 IN 1RS-232 OUT 1 8

46RS-232 GND 1

AIRCRAFT GND 61

GPS/WAAS ANTENNA

COM ANTENNA

NAV ANTENNA

AIRCRAFT POWER 51 ESSENTIAL BUS22 AWG

NAV

AUDIO OUT LOAUDIO OUT HI

23HILO

ALERT 1AUDIO IN

P1001

4

RS-232 INRS-232 OUT

RS-232 OUT 2RS-232 IN 2

726

RS-232 GND 2 45s

s

s

s

s

s

CONFIG MODULE POWERCONFIG MODULE GND

CONFIG MODULE DATACONFIG MODULE CLOCK

REDBLKYELWHT

65646263 4

5

FAN POWER OUT (12 VDC) 59FAN GROUNDFAN TACH IN 58

43

FAN

REDBLACKYELLOW

Figure D-2. GTN 650 Typical Installation Sheet 1 of 2

Figure C-1 GTX 35R/45R Typical Interconnect

GTX 35R/45R P3251

P325-XPDR

GSU 25P252

GDU 4XXP4602/J3701

Figure C-6 GTX 35R - GNS 400W/500W Series Interconnect

Figure C-7 USB Programming Interface (Garmin Dealers Only)

GNS 400W/500WP4001/P5001GTX 35R

GTX 35R with Single 400W/500W SERIES

P3251

P3251GTX 35R/45R

P325-XPDR

S

USB TYPE BRECEPTACLE

190-01115-01 G3X/G3X Touch Installation Manual - G3X w/GSU 25 and/or GAD 29 DrawingsRev. AK Page 27-23

Figure 27-2.6 GDU 37X/4XX - External LRU Interconnect Examples (page 1 of 2)

GDU 4XX/37X

SEE NOTES 6 AND 11

CONFIGURATION GUIDANCE1. GDU 4XX/37X TO SL40, GTR 200, OR GTR 225

A. ON THE GDU 4XX/37X RS-232 CONFIG MODE PAGESET CONNECTED GDU 4XX/37X RS-232 CHANNEL FORMAT TO "GARMIN VHF COMM"

B. NO SL40 OR GTR 200 CONFIGURATION REQUIREDC. CONFIGURE GTR 225 SERIAL PORT IO MODE TO "NMEA" ON SYS CONFIGURATION PAGE

2. GDU 4XX/37X TO SL30 OR GNC 255A. ON THE GDU 4XX/37X COMM CONFIG MODE PAGE

SET CONNECTED GDU 4XX/37X RS-232 CHANNEL FORMAT TO "GARMIN VHF NAV/COMM"B. ON THE SL30 NAV SETUP PAGES

SET INDICATOR HEAD TYPE TO "SERIAL"C. ON THE GNC 255 CONFIGURATION PAGES

SET CDI INDICATOR TYPE TO "SERIAL" ON NAV CONFIGURATION PAGESET SERIAL PORT IO MODE TO "NMEA" ON SYS CONFIGURATION PAGE

3. GDU 4XX/37X TO VERTICAL POWER VP-X OR VP-200A. ON THE GDU 4XX/37X RS-232 CONFIG MODE PAGE

SET CONNECTED GDU 4XX/37X RS-232 CHANNEL FORMAT TO "VERTICAL POWER"B. ON THE GDU 4XX/37X EIS CONFIG MODE PAGE

SET THE "VOLTS 1" AND "VOLTS 2" INPUTS TO ONE OF THE FOLLOWING BASED ON WHATINPUTS HAVE BEEN CONNECTED TO THE VP-X OR VP-200:

- NONE- VERTICAL POWER MAIN BATT VOLTS- VERTICAL POWER AUX BATT VOLTS- VERTICAL POWER BUS 1 VOLTS- VERTICAL POWER BUS 2 VOLTS

SET THE "SHUNT 1" AND "SHUNT 2" INPUTS TO ONE OF THE FOLLOWING BASED ON WHATINPUTS HAVE BEEN CONNECTED TO THE VP-X OR VP-200:

- NONE- VERTICAL POWER MAIN BUS AMPS- VERTICAL POWER BUS 1 AMPS- VERTICAL POWER BUS 2 AMPS

C. REFERENCE VERTICAL POWER DOCUMENTATION FOR ADDITIONAL INSTALLATION AND CONFIGURATION GUIDANCE

NOTE: THIS INTERFACE EXAMPLE DRAWING IS NOT SUFFICIENT FOR INSTALLATION OF ANSL 30, SL 40, GTR 225, OR GNC 255. CONTACT A LOCAL GARMIN AVIONICSDEALER FOR COMPLETE INSTALLATION INFORMATION.

RS-232 OUT 230SIGNAL GROUND44RS-232 IN 214WHT

BLUORN

S

RS-232 OUT 20SIGNAL GROUND 21

RS-232 IN 22

WHTBLUORN

VERTICAL POWER

SEE NOTE 7

281029

J1 J3

VP-X VP-200