CAN BUS order GSA38—GAD29—GSU25—GEA24---GDU460---G5---GDU465---GI260---GMA245---GTR20---GMU11---GSA38 1 2.

CAN BUS order GSA38—GAD29—GSU25—GEA24---GDU460---G5---GDU465---GI260---GMA245---GTR20---GMU11---GSA38 GSA 38 GDU 460 GDU 465 GAD 29 GEA 24 GSU 25 GI 260 GMU11 GTR 20 G 5 GMA 245

GTN 650 GPS CO Det GEA 24 eng anzlr GSU 25 ADHRS DVD GI 260 AOA Ind VPX Power Leads GAD 29 Data Conc. 24” 16” 16” 14” 14” 16” 12” Ground Leads 10” 24” 3 1/4” 3 1/2” 4 1/2” 5 1/2” 8 1/2” 12” 16” 18” 18” 18” 24” GMA 245 Audio 72” E Buss Power Leads G5 51” GDU 460 PFD GMC 307 A Pilot GDU 465 MFD Roll Trim interconnect 32” Headset/Mic feed 16” GSA 28 Roll Servo To Fuselage exit 89” GTX 45R ADSB Xpdr 6” GTR20 Comm Radio ELT 12” 13” 18” 58” 24” GMU 11 Magnatometer 32” GSA 28 Pitch Servo 32” 48” Pitch Trim interconnect

Engine/Airframe Sensors
GTX 45R ADSB in/Out Engine/Airframe Sensors RS-232 RS-232 GMC 307 A/P Controller GEA 24 Engine Anlzr GAP 26 Pitot/AOA Static Source GTP 59 Temp probe G5 Flight Display RS-232 RS-232 GMU 11 Magnetometer GI260 AOA Indicator AOA A429 Pitot GSU 25 ADAHRS GSA 28 Pitch servo GSA 28 Roll servo GTR 20 Com 2 GMA 245 Audio Panel GDU 460 PDF RS-232 CAN Bus RS-232 GPS/Com RS-232 RS-232 Connext RS-232 CO Det RS-232 GAD 29 Data Concen. (A429) GDU 465 MFD/XM ELT GTN 650 GPS/Nav RS-232 A429 Nav A429 GPS A429 Air Data Ethernet VPX-pro CAN BUS order GSA28—GAD29—GSU25—GEA24---GDU460---G5---GDU465---GI260---GMA245---GTR20---GMU11---GSA28

Notes: Symbol Designations:
Unless Otherwise noted, all stranded wire must conform to MIL—W-22759/16 or equivalent Unless Otherwise noted, all shielded wire must conform to MIL-C or equivalent. Unless otherwise noted, all wires are 24 gauge minimum. Unless otherwise noted, all shielded grounds must be made to the respective unit back shells. All other grounds should be terminated to aircraft ground as close to the respective unit as possible. Unless otherwise noted, multi conductor codes are White, White/Blue, White/Orange, White/Green from top to bottom as applicable. Unless Otherwise noted, Ethernet wire color codes are White/Blue, Blue. White/Orange, Orange Unless Otherwise noted, all co-axial cable must be RG-400, RG-142B or equivalent. Symbol Designations: Twisted Shielded Single Conductor Shield terminated to ground Twisted Shielded Single Conductor Shield floats Twisted Shielded Pair Shield terminated to ground Twisted Shielded Pair Shield floats Twisted Shielded 3 Conductor Shield terminated to ground Twisted Shielded 3 Conductor Shield floats Twisted Shielded 4 Conductor Shield terminated to ground Twisted Shielded 4 Conductor Shield floats Coaxial Cable Antenna Shield Block Ground Aircraft Ground Wire Splice Connection

GDU 460 (PFD) VPX GMC 307 (Auto Pilot) GTX 45R (Xponder)
CM Ground CM Power CM Data CM Clock 49 17 50 33 1 4 3 2 GND VCC DATA CLK Config Module Blk Red Yel Wht RS232Rx 1 RS232 TX1 RS232 Gnd 1 S 47 48 37 PFD/VPX 1a #24 J1 VPX RS232 Tx RS232 Rx RS232 Gnd J1-20 J1-22 J1-21 57600 Baud communication Signal Gnd CDU System ID 27 10 Jumper identifies this Display as PFD RS232Rx 2 RS232 TX2 RS232 Gnd S 1430 44 PFD/GMC 1a #24 J3071 GMC 307 (Auto Pilot) RS232 Tx RS232 Rx 1 2 6 232Rx 3 232 TX3 232 Gnd 3 S 29 13 36 GTX/PFD 4a #24 GTX 45R (Xponder) 30 8 51 RS232Rx 2 RS232 TX2 RS232 Gnd 2 RS232Rx 4 RS232 TX4 RS232 Gnd 3/4 S 24 5 44 GTN/PFD 1a #24 P4X02 RS232 Rx4 RS232 Gnd 40 23 34 CONNEXT INTERFACE RS232Rx 3 RS232 TX3 25 6 GTN/PFD 2a #24 RS232 TX5 RS232 Rx5 41 35 MAPMX INTERFACE GTN 650 (GPS/Nav/Com) GMA245 (Audio) Audio Alert 3 In Hi Audio Alert 3 In Lo Audio Out Hi Audio Out Lo S 1 18 GMA/PFD 1a #24 29 43 P2401 Aircraft Power 1 Aircraft Power 2 Power Gnd 32 31 15 16 #22 14/28 Volt 5amp fuse Backup PFD P1a / VPX J12-9 PFD P2a / E Buss PFD gnd1 a PFD gnd2 a 46 45 S GEA24/PFD CAN#4 PFD/G5 CAN#5 CAN HI CAN LO CAN 4a CAN 5a GSU 25 (ADHRS) P4X01 J251 232Rx 1 232 Tx1 232 Gnd 1 S 5 4 6 PFD/GSU 1a (to GSU 25 J251) 232Tx 1 232 Rx 1 Garmin Instrument Data GPS Antenna GPS Antenna CAN BUS order GSA38—GAD29—GSU25—GEA24---GDU460---G5---GDU465---GI260---GMA245R---GTR20---GMU11---GSA38

GDU 465 (MFD/XM) GMA 245 (Audio) GEA 24 (Engn Alzr) CO Detector P4X02
Aircraft Power 1 Aircraft Power 2 Power Gnd 32 31 15 16 #20 #22 14/28 Volt 2amp fuse Backup (Opt) MFD/VPX J10-2 P1a PFD/E buss P2a PFD gnd1 a PFD gnd2 a 46 45 S G5/MFD CAN#6 MFD/GI260 CAN#7 CAN HI CAN LO CAN 6a CAN 7a Stereo Out Right Stereo Out Left Stereo Out Lo S 19 3 20 2 MFD/GMA 1a #24 J2402 GMA 245 (Audio) Music 2 In Right Music 2 In Left Music 2 In Lo 24 23 25 N/C Audio Alert 2 In Hi Audio Alert 2 In Lo Audio Out Hi Audio Out Lo S 1 18 GMA/MFD 2a #24 15 14 GEA 24 (Engn Alzr) RS232Rx 1 RS232 TX1 RS232 Gnd S 47 48 27 MFD/GEA 1a #24 RS232 Tx RS232 Rx 5 4 6 J241 S CO/MFD 1a #24 RS232 Tx Out RS232 TX In Gnd 7 8 x CO Detector RS232 2 Rx in RS232 2 Tx Out Signal Gnd 14 30 34 ELT Mini DIN P4X01 No Connections external camera Video input

USB type B (Receptacle)
GTX 45R (XPDR) GTN650 (GPS) P3252 P1002 Ethernet In 1A Ethernet In 1B Ethernet Out 1A Ethernet Out 1B S 7 2 6 1 GTX/GTN 1a #24 Ethernet Out 3A Ethernet Out 3B Ethernet In 3A Ethernet In 3B 25 26 23 24 S GTX/GTN 2a #24 P3251 Audio Mute 37 GTX/GTN 2a #24 35 TAWS Audio Active Aircraft Gnd 20 41 GDX Gnd 1a #22 GDX Gnd 2a Aircraft Power 21 61 #22 14/28 Volt 3amp fuse Backup (Opt) GTX /VPX J1-1 P1a GTX P2a (unconnected) RS232Rx 1 RS232 Tx1 RS232 Gnd 1 S 31 9 52 GTX/GSU 3a #24 P252 GSU25 (ADHRS) RS232 TX3 RS232 Rx3 RS232 Gnd 10 11 Power Config Power Control 59 38 GDX Gnd 3a #22 RS232Rx 2 RS232 TX2 RS232 Gnd 2 S 30 8 51 GTX/PFD 4a #24 P4602 GDU 460 (PFD) RS232 TX3 RS232 Rx3 RS232 Gnd 13 29 36 GMA 245 (Audio) Audio Out Hi Audio Out Lo Audio In Hi Audio In Lo S 46 47 GTX/GMA 1a #24 J2401 31 32 USB type B (Receptacle) USB Vbus Power USB Data Hi USB Data Lo USB Gnd S 44 2 24 45 GTX/USB 6a #24 VBUS D+ D- Gnd SHIELD GAD 29 (Data Conc.) J 292 17 5 ARNIC 429 Rx 3A ARNIC 429 RX 3B S GTX/GAD 1a #24 6 ARNIC 429 Out A ARNIC 429 Out B 18 6 ARNIC 429 Tx 2A ARNIC 429 Tx 2B S GTX/GAD 2a #24 27 28 ARNIC 429 In 1A ARNIC 429 In 1B XPDR Ant XPDR Antenna

GMA 245 (Audio) GTN650 (Com 1) GPS 650 (Nav 1) GTR 20 (Com 2)
J2401 36 37 S GI260/GMA245 CAN#8 GMA245/GTR 20 CAN#9 CAN HI CAN LO CAN 8a CAN 9a Com 1 Audio In Hi Com 1 Audio Lo 9 10 GTN650 (Com 1) 500 ohm Com Audio Hi 500 ohm Com Audio Lo S 7 18 GTN/GMA 1a #24 P1003 11 Com 1 Mic Audio Out Hi Com Mic Audio Hi Com Mic Audio Lo Com Mic Key 5 20 Com 1 Mic Key Out 12 GTN/GMA 2a #24 GTN/GMA 3a #24 GPS 650 (Nav 1) Nav 1 Audio In Hi Nav 1 Audio In Lo Vloc Audio Out Hi Vloc Audio Out Lo S 16 17 GTN/GMA 4a #24 P1004 18 GTR 20 (Com 2) P2001 Com 2 Audio In Hi Com 2 Audio Lo 13 14 500 ohm Com Audio Hi 500 ohm Com Audio Lo S 10 29 GTR/GMA 1a #24 15 Com 2 Mic Audio Out Hi Com Mic Audio Hi Com Mic Audio Lo Com Mic Key 17 38 35 Com 2 Mic Key Out 30 GTR/GMA 2a #24 GTR/GMA 3a #24 GTX 45 (ADSB Xpdr) Audio Alert 1 In Hi Audio Alert 1 In Lo Audio Out Hi Audio Out Lo S 46 47 GTX/GMA 5a #24 P3251 31 32 Pilot Mic Audio In Lo Pilot Mic Audio In Hi Pilot PTT S 34 Pilot Mic /GMA 1a #24 Pilot Mic Key In 35 33 PTT Pilot/GMA 1a #24 1 2 3 S Headset/GMA 2a #24 Pass Headset Lo Pass Headset Out Right Pass Headset Out Left 42 41 40 Wire Pass Headsets in parallel 4 5 6 PFD P4X02 Audio Alert 3 In Hi Audio Alert 3 In Lo Audio Out Hi Audio Out Lo S 1 18 GMA/PFD 1a #24 29 43 MONO OUT AUDIO GROUND AUDIO SHIELD WHITE GREEN BLACK HEAT SHRINK GI260 (AOA) 44 43 Alert 4 Hi Alert 4 Lo S GMA/GI260 1a #24 CAN BUS order GSA38—GDU29—GSU25—GEA24---GDU460---G5---GDU465---GI260---GMA245---GTR20---GMU11---GSA38

GMA 245 (Audio) GDU465 (MFD) DVD Player J2402 Aircraft Power 8 9 #22
14/28 Volt 3amp fuse (Not installed) GMA/VPX J P1a GMA (Unconnected) P2a Aircraft Gnd 10 11 GMA Gnd 1a #22 GMA Gnd 2a Co-Pilot Mic Audio In Lo Co-Pilot Mic Audio In Hi Pilot PTT S 33 Co-Pilot Mic/GMA 2a #24 Co-Pilot Mic Key In 34 32 PTT Co-Pilot/GMA 2a #24 7 8 9 S Headset/GMA 3a #24 Pilot Headset Out Lo Pilot Headset Out Right Pilot Headset Out Left 1 31 16 10 11 12 S Headset/GMA 4a #24 Co-Pilot Headset Out Lo Co-Pilot Headset Out Right Co-Pilot Headset Out Left 2 4 3 13 24 25 S Headset/GMA 5a #24 Pass 1 Mic Audio In Lo Pass 1 Mic Audio In Hi 36 35 15 16 17 S Headset/GMA 6a #24 Pass 2 Mic Audio In Lo Pass 2 Mic Audio In Hi 38 37 18 19 S Speaker/GMA 7a #24 Speaker Audio Out Hi Speaker Audio Out Lo 44 43 + - Cabin Speaker Stereo Out Right Stereo Out Left Stereo Out Lo S 19 3 20 2 MFD XM/GMA 1a #24 P4X02 GDU465 (MFD) Music 1 In Right Music 1 In Left Music 1 In Lo 24 23 25 N/C Audio Alert 2 In Hi Audio Alert 2 In Lo Audio Out Hi Audio Out Lo S 1 18 GMA/MFD 2a #24 15 14 DVD out right DVD out Left DVD Lo S Xx DVD/GMA 1a #24 xxx DVD Player Music 2 In Right Music 2 In Left Music 2 In Lo 27 26 28 DVD/VPX J8-3 P1a DVD/GND 1a

GTN 650 (GPS/Nav/Com) GAD 29 (data Concen.) GDU 460 (PFD) G5 ELT
23 11 ARNIC 429 Rx 1A (GPS) ARNIC 429 RX 1B (GPS) S GTN/GAD 2a #24 10 29 ARNIC 429 Out 1A ARNIC 429 Out 1B 24 12 ARNIC 429 Rx 1A (Air Data) ARNIC 429 RX 1B (Air Data) S GTN/GAD 3a #24 48 67 ARNIC 429 In 1A ARNIC 429 In 1B Aircraft Power 19 20 #22 14/28 Volt 3amp fuse Backup (Opt) GPS/VPX J P1a GPS/Ebuss P2a RS232Rx 4 RS232 TX4 RS232 Gnd 3/4 S 24 5 44 GTN/PFD 1a #24 P4X02 GDU 460 (PFD) RS232 Rx4 RS232 Gnd 40 23 34 CONNEXT INTERFACE RS232Rx 3 RS232 TX3 25 6 GTN/PFD 2a #24 RS232 TX5 RS232 Rx5 41 35 MAPMX INTERFACE Aircraft Gnd 77 78 GPS Gnd 1a #22 GPS Gnd 2a TAWS Audio Active 35 GTX/GTN 2a #24 (to GTX P3251 pin 37) G5 P51 RS232Rx 1 RS232 TX1 RS232 Gnd S 4 5 6 G5/GTN 1a #24 RS232 TX2 RS232 Rx2 7 26 45 MAPMX INTERFACE S ELT/GTN 1a #24 RS232 Tx Out RS232 TX In Gnd 2 4 3 ELT RS232 1 Rx in RS232 1 TX Out Signal Gnd 1 27 8 46 GDX 45R (XPDR) P1002 P3252 S Ethernet 1A Ethernet 1B Ethernet Out 1A Ethernet Out 1B S 7 2 6 1 GTX/GTN 1a #24 Ethernet Out 3A Ethernet Out 3B Ethernet In 3A Ethernet In 3B 25 26 23 24 GTX/GTN 2a #24 P1003 Aircraft Power 43 44 #22 14/28 Volt 3amp fuse Backup (Opt) GPS/VPX J10-5 P3a GPS/E buss P4a Com 1 Audio In Hi Com 1 Audio Lo 9 10 500 ohm Com Audio Hi 500 ohm Com Audio Lo S 7 18 GTN/GMA 1a #24 11 Com 1 Mic Audio Out Hi Com Mic Audio Hi Com Mic Audio Lo Com Mic Key 5 20 Com 1 Mic Key Out 12 GMA 245 (Audio) J2401 GTN/GMA 2a #24 GTN/GMA 3a #24 Aircraft Gnd 37 38 GPS Gnd 3a #22 GPS Gnd 4a

GTN 650 (GPS/Nav/Com) cont. GMA 245 (Audio)
Nav 1 Audio In Hi Nav 1 Audio In Lo Vloc Audio Out Hi Vloc Audio Out Lo S 16 17 GTN/GMA 4a #24 J2401 18 P1004 GAD 29 (data Concen.) P292 22 10 ARNIC 429 Rx 2A (NAV) ARNIC 429 RX 2B (NAV) S GTN/GAD 1a #24 24 23 ARNIC 429 Out A ARNIC 429 Out B Aircraft Power 51 52 #22 14/28 Volt 3amp fuse Backup (Opt) GPS/VPX J1-2 P5a GPS/ E Buss P6a Aircraft Gnd 61 62 GTN Gnd 5a #22 GTN Gnd 6a GAD 29 (Data Concen.) J291 Aircraft Power 7 8 #22 14/28 Volt 3amp fuse E Buss 3 amp fuse GAD/VPX J8-5 P1a GAD/E Buss P2a Aircraft Gnd 6 9 GAD Gnd 1a #22 GAD Gnd 2a 1 2 S GSA38 Pitch/GAD29 CAN#1 GAD29/GSU25 CAN#2 CAN HI CAN LO J292 GTN 650 (GPS) P1004 22 10 ARNIC 429 Rx 2A (NAV) ARNIC 429 RX 2B (NAV) S GTN/GAD 1a #24 24 23 ARNIC 429 Out A ARNIC 429 Out B P1001 23 11 ARNIC 429 Rx 1A (GPS) ARNIC 429 RX 1B (GPS) S GTN/GAD 2a #24 10 29 ARNIC 429 Out 1A ARNIC 429 Out 1B 24 12 ARNIC 429 Tx 1A (Air Data) ARNIC 429 Tx 1B (Air Data) S GTN/GAD 3a #24 48 67 ARNIC 429 In 1A ARNIC 429 In 1B GTX 45R (ADSB Xpdr) P3251 17 5 ARNIC 429 Rx 3A ARNIC 429 RX 3B S GTX/GAD1a #24 6 ARNIC 429 Out A ARNIC 429 Out B 18 6 ARNIC 429 Tx 2A ARNIC 429 Tx 2B S GTX/GAD 2a #24 27 28 ARNIC 429 In 1A ARNIC 429 In 1B

GTR 20 (Com 2) GMA 245 (Audio) GMU 11 (Magnatometer) CAN BUS order
P2001 Com 2 Audio In Hi Com 2 Audio Lo 13 14 Receiver Audio Out Hi Receiver Audio Lo S 10 29 GTR/GMA 1a #24 15 Com 2 Mic Audio Out Hi Com Mic Audio In Hi Com Mic Audio In Lo Com Mic Key 17 36 35 Com 2 Mic Key Out 30 GMA 245 (Audio) J2401 GTR/GMA 2a #24 GTR/GMA 3a #24 Aircraft Power 1 20 GTR 20/VPX J P 1a #20 14/28 Volt 7.5amp fuse GTR 20 Gnd 1a #20 8 27 Jumper to identify Com 2 7 6 S GMU11/GTR CAN#10 GMA245/GTR 20 CAN#9 CAN HI CAN LO CAN 10a CAN 9a P2002 GTR 20 Antenna Com Antenna GMU 11 (Magnatometer) J441 Aircraft Power 7 8 #22 14/28 Volt 3amp fuse Backup (Opt) GMU/VPX P1a GMU/E Buss P2a Aircraft Gnd 9 GMU Gnd 1a #22 1 2 S GTR/GMU CAN#10 GMU/GSA pitch CAN#11 CAN HI CAN LO CAN BUS order GSA28—GDU29—GSU25—GEA24---GDU460---G5---GDU465---GI260---GMA245---GTR20---GMU11---GSA28

GSU 25 (ADHRS) GDU 460 (PFD) GTX 45R (XPDR) GTP Temp Probe CO Detector
Aircraft Power 7 8 #22 14/28 Volt 2amp fuse Backup (Opt) GSU/VPX J8-4 P1a GSU/E Buss P2a Aircraft Gnd 9 GSU Gnd 1a #22 1 2 S GAD29/GSU25CAN#2 GSU25/GEA24CAN#3 CAN HI CAN LO CAN 2a CAN 3a GDU 460 (PFD) P4X01 232Rx 1 232 Tx1 232 Gnd 1 S 5 4 6 PFD/GSU 1a (to GSU 25 J251) 232Tx 1 232 Rx 1 Garmin Instrument Data GTX 45R (XPDR) P252 RS232Rx 1 RS232 Tx1 RS232 Gnd 1 S 31 9 52 GTX/GSU 3a #24 RS232 TX3 RS232 Rx3 RS232 Gnd 10 11 P3251 S Power Sense Low S GSU/GTP 1a #24 Temp Probe Power out Temp Probe In Hi Temp Probe In Lo 1 2 3 GTP Temp Probe CO Detector 353 Aircraft Power 1 #22 14/28 Volt 3amp fuse CO/Batt Switched Buss P1a S CO/MFD 1a #24 RS232 Tx Out RS232 TX In Gnd 7 8 x GDU 465 (MFD) RS232 Tx in RS232 TX Out Signal Gnd 14 30 34 Aircraft Gnd 5 CO Gnd 1a #22 S ELT/GTN 1a #24 RS232 Tx Out RS232 TX In Gnd 2 4 3 ELT RS232 1 Rx in RS232 1 TX Out Signal Gnd 1 27 8 46 GTN 650 (GPS) Aircraft Power 1 #22 14/28 Volt 1amp fuse ELT/Batt Switched Buss P1a ELT Mini DIN

GMC 307 (Auto Pilot) GDU 460 (PFD) GSA 28 (Roll Servo)
RS232Rx 2 RS232 TX2 RS232 Gnd S 1430 44 PFD/GMC 1a #24 RS232 Tx RS232 Rx 1 2 6 J3071 P4X02 CONFIGURE TO GARMIN INSTRUMENT DATA S Aircraft Power 7 9 #22 14/28 Volt 2amp fuse Backup (Opt) GMC/VPX J10-8 P1a GMC (Unconnected) P2a Aircraft Gnd 5 15 GMC Gnd 1a #22 GMC Gnd 2a GSA 28 (Roll Servo) RS232Rx 2 RS232 TX2 S 8 7 GSA/GMC 1a #24 RS232 Tx RS232 Rx RS232 Gnd 3 4 GSA 28 (Roll Servo) J281 1 2 3 4 S GSA28/GAD29 CAN#1 CAN HI CAN LO CAN TERM CAN 1a Connect both servos and GMC 307 to single power source ( per G5 Install manual p 59) GMC 307 (Auto Pilot) J3071 RS232 Rx RS232 TX S 8 7 - GSA/GMC 1a #24 RS232 2 Tx RS Rx RS232 Gnd 3 4 5 Aircraft Power 10 #22 14/28 Volt 2amp fuse GSA Roll/VPX J8-7 1a Aircraft Gnd 9 GSA Roll Gnd 1a #22 Set to Garmin Instrument Data 15 Autopilot Disconnect Connect to active low pushbutton switch (both Roll and Pitch Servo together) Trim In 1 Trim In 2 Trim Out 1 Trim Out 2 11 12 13 14 Line 1 in from trim switch Line 2 in from Trim Switch Line 1 Out to Trim Motor Line 2 Out to Trim Motor

GSA 28 (Pitch Servo) GEA 24 (Engn Alzr) GDU 465 (MFD) Red Cube J281 1
3 4 S GSA28/GMU11 CAN#11 CAN HI CAN LO CAN TERM CAN 11a Aircraft Power 10 #22 14/28 Volt 2amp fuse GSA Pitch/VPX J a Aircraft Gnd 9 GSA Pitch Gnd 1a #22 5 8 Pitch Servo ID 15 Autopilot Disconnect Connect to active low pushbutton switch (both Roll and Pitch Servo) Trim In 1 Trim In 2 Trim Out 1 Trim Out 2 11 12 13 14 Line 1 in from trim switch Line 2 in from Trim Switch Line 1 Out to Trim Motor Line 2 Out to Trim Motor GEA 24 (Engn Alzr) J241 1 2 S GSU25/GEA24CAN#3 GEA24/GDU460CAN#4 CAN HI CAN LO CAN 3a CAN 4a Aircraft Power 7 8 #22 14/28 Volt 2amp fuse Backup (Opt) GEA/VPX J P1a GEA (Unconnected) P2a GDU 465 (MFD) RS232Rx 1 RS232 TX1 RS232 Gnd S 47 48 27 MFD/GEA 1a #24 RS232 Tx RS232 Rx 5 4 6 Aircraft Gnd 9 GMC Gnd 1a #22 P4X02 J242 All Engine in data …. See page 333 for pin out J243 Red Cube Red xxx S GEA/Red Cube 1a #24 Fuel XDCR +12V Fuel XDCR Gnd Fuel Flow 24 20 23 All Engine in data …. See page 334 for pin out J244 All Engine in data …. See page 335 for pin out

G5 GTN650 (GPS) GI 260 (AOA Indicator) GMA245 (Audio)
1 2 S PFD/G5 CAN#5 G5/MFD CAN#6 CAN HI CAN LO CAN 5a CAN 6a Aircraft Power 7 8 #22 14/28 Volt 5amp fuse Backup (Opt) G5/VPX J8-6 P1a G5/E Buss P2a Aircraft Gnd 9 G5 Gnd 1a #22 RS232Rx 1 RS232 TX1 RS232 Gnd S 4 5 6 G5/GTN 1a #24 P1001 GTN650 (GPS) RS232 TX2 RS232 Rx2 7 26 45 MAPMX INTERFACE Pitot Static ???? GI 260 (AOA Indicator) GI260/VPX J12-10 P1a GI260 Gnd1a AIRCRAFT POWER POWER GROUND CAN HI BLUE CAN LO VIOLET SHIELD GND RS-232 RX RS-232 TX DC LIGHTING BUS MONO OUT AUDIO GROUND AUDIO SHIELD RED BLACK BLUE VIOLET BLACK HEAT SHRINK YELLOW BROWN GRAY WHITE GREEN 4 5 1 2 S MFD/GI 260 CAN#7 GI260/GMA245 CAN#8 CAN 7a CAN 8a n/used GMA245 (Audio) J2401 45 44 Alert 4 Hi Alert 4 Lo S 3 7 6 GMA/GI260 1a #24 3 Additional VPX Pins Heated Pitot Power Landing Light Heated Seats Light Speed Ignition #2 Interior Light Buss Exterior Light Buss Rudder Trim (Avionics 3) Pri Alternator field BU Alternator field J10-6 J12-1 J8-2 J8-1 J10-3 J12-12 J12-2 J12-11 J10-7

+ 12 V 12 V in Gnd In 5V Reference Servo Front On/off + - ctrl
5 V 3A lin reg 12V in 5V out gnd Texas Inst PN LM1085IT-5.0/NOPB + 12 V red 5V Reference gr blk blu Servo Front On/off ctrl wht gnd Reference or red gr blu or ctrl Servo Front L/R Front on/off Front L/R Servo Rear On/off ctrl Rear L/R Rear on/off ctrl Servo Rear L/R

Alternator field (5A #18) J12-11
Back up Alternator (30 amp) Primary Alternator (60 amp) Starter Firewall Alternator field (5A #18) J12-11 BU Alternator field (5A #18) J10-7 Starter Annunciator #20 to J2-11 Keyed Ignition VPX-Pro #20 J10-1 #20 VPX Power #6 BU Alternator VPX switch input #22 J2-6 Primary Batt + feed #2 #2 Pri Alternator VPX switch input #22 J2-1 Master Switch + Pri/BU Alt Switch #22 #22 Battery Avionics 1 VPX switch input #22 J2-3 _ Battery Relay Batt Buss feed #14 E Buss (BU Power to Avionics 1) Switched Batt Buss feed #16 Battery Buss feed #18 PFD GTN650 ADAHR Magnitometer Elec Ign #2 ARNIC 429 G5 Battery Buss (Switched ) Battery Buss (always on) E Buss feed #18 Fuel Pump Electronic Ignition 1 Inst Lights Overhead lights Door entry lights Baggage light E Buss on/off E Buss feed #14 #22 Avionics 1 On/off

+ + + Alt 2 Field Avionics 1 J2-3 Fuel Pump Off E Buss Off Alt 1 Field
Blue feed from 6b buss (unswitched bat buss) feed to E buss Fuel Pump Off E Buss Off Alt 1 Field + J2-1 white from Buss 6a to Fuel pump + J2-6 orange feed to buss 6a (switched bat buss) On On Alt 2 Field J2-7 Black Master On Avionics 1 On Avionics 2 On Avionics 3 On to Master relay yellow J2-8 Red Off Off Off Off green feed from battery +

+ Pitot Heat Exterior Lights Buss Heated Seats Buss
Interior Lights Buss 610 ohm 610 ohm + On On On Off #1 Off #2 Off #3 Off #4 On To Switch Dimmer VPX J10-6 VPX J12-12 VPX J8-2 VPX J10-3 LED On = green Off = red Load

+ + Nav Lights Strobes Wig Wag Beacon Landing Lights On On On On On
610 ohm 610 ohm On On On On On + Off #1 Off #2 Off #3 Off #4 Off #5 To Switch Dimmer J12-1 To Fly LED Control Board To Fly LED Control Board To Fly LED Control Board To tail Beacon control board + To Exterior Lights Buss LED On = green Off = red Load

+ feed from Heated Seat Buss 5a
Left Door Right LED LED Front Pin Limit Switch Rear Pin Limit Switch Front Pin Limit Switch Rear Pin Limit Switch To 555 timer chip flasher + from ex light buss Flap Up Down Flap up J2-14 Flap down J2-15 LED LED heated seat + feed from Heated Seat Buss 5a heated seat

See Reading Light Circuit
610 ohm 610 ohm Map White Map Red Inst Panel Over Head Foot well + To Switch Dimmer + Power feed from Interior Light Buss LED Light LED Light 10 ohm 10 ohm To Panel lights To Overhead lights To Foot well lights 610 ohm 610 ohm Reading Master Door Override Defrost Fans Tunnel Fan Power feed from Interior Light Buss + + To Switch Dimmer See Door Circuit See Reading Light Circuit See Fan Circuit See Fan Circuit Up is on = green LED Load

+ + Light Hue Inst Dim Switch Dim Red Green Blue White 610 ohm
Power feed to all other switch tip groups Inst Dim Switch Dim Light Hue Red Green Blue White + + To Inst requiring +12 V to dim Power feed from Interior Light Buss Power feed from Interior Light Buss Power feed to switch groups

+ + + + Reading Reading Light L Light R Heat Heat L/R LED LED 10 ohm
5V from Arduino Power feed from Switch tip dimmer + 610 ohm 610 ohm + Heat L/R Power feed from Switch tip dimmer 5V from Arduino + Refrence to Arduino + Power feed from Interior Light Buss Power feed from Interior Light Buss Refrence to Arduino Load

Power feed from Door Overide
+ Door Limit Switch

CAN BUS order GSA38—GAD29—GSU25—GEA24---GDU460---G5---GDU465---GI260---GMA245---GTR20---GMU11---GSA38 1 2.

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CAN BUS order GSA38—GAD29—GSU25—GEA24---GDU460---G5---GDU465---GI260---GMA245---GTR20---GMU11---GSA38 1 2.

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Presentation on theme: "CAN BUS order GSA38—GAD29—GSU25—GEA24---GDU460---G5---GDU465---GI260---GMA245---GTR20---GMU11---GSA38 1 2."— Presentation transcript:

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