This page describes all avionics and any item that needs to be wired electrically.

Overview

Instead of a tradition wiring diagram a written wiring plan was created for N622JC instead. A wiring plan is not visual but much easier to create and maintain.

Documentation Sources

Key	Description
GIM	Garmin G3X/Garmin G3X Touch Installation Manual
GTPM	Garmin G3X/Touch Pilot Manual
GNXMM	Garmin G3X/GNX 375 Maintenance Manual
GTRIM	Garmin G3X/GTR 200 Installation Manual
ULIM	UL Power 350iS/Installation Manual

Basics

Breaker Setup

Where a device can be physically turned off, a normal non-pull-able breaker is used. If the device can not be physically turned off, then a pull-able breaker is used. Where devices specify a breaker size, that size is used otherwise the breaker is sized appropriately for the current that the wire is capable of delivering.

Breakers have undocumented pins

• 1 = Power In
• 2 = Power Out

Switch Setup

A single row of switches that are used during the start and end of flight will be placed in an out of the way location. These switches include Master, ECU, Ignition 1, Ignition 2 and AV Master. During the flight these switches will not need to be used except in an emergency.

In a more accessible location should be switches used during flight. These switches include Navigation/Strobe Lights, Taxi/Landing Lights, Boost and Pitot Heat. This does not account for the PFD and AP Master switches. These switches should generally be turned on and left on, even when the Master switch is turned off. Only in very rare circumstances would one wish to turn these off. Should these be pull-able breakers instead?

Switches should be considered by default On in the Up position and Off in the Down position. For two position switches the Up position should be considered the safest option. For example, Landing Lights should be Up and Recon Lights should be Down. If I go through in an emergency and flip this switch up, even if it is not what I meant, at least I have solid lights, not forced flashing lights on landing at night. “Alternate” or “Non-standard” should be down. Navigation/Strobe should be Up, Navigation Only should be Down. Again, most of the time you will want both Navigation and Strobe lights on.

Switches have undocumented pins

• 0 = Common
• 1 = Position 1
• 2 = Position 2

Landing/Recognition Lighting

We can configure this in one of two ways:

1. SPST – Landing On/Off and then let the G3X take care of turning on the wig-wag lighting with it’s airspeed detection.
2. SPDT – Landing/Off/Recognition. When in Landing, let the G3X take care of turning on the wig-wag lighting with it’s airspeed detection but if in the Recognition mode, it overrides the G3X and enables wig-wag continously.

Number 2 gives more flexibility. It would really become “Landing Light” and “Day Light”. One would use the “Recognition” lighting only in the day. At night you wouldn’t want to force the wig-wag mode and have it be cycling during touch down.

Power Distribution Wiring

The power distribution wiring is the wiring from the battery all the way to the breakers and switches that turn on an individual device. Once power gets to the switch, it becomes part of the “Avionics” wiring.

Power Distribution Parts

ID	Part #	Description	Notes
B:AP	W58XC4C12A5	Breaker – Auto Pilot and Elevator/Aileron Servos	5A
B:AUDIO	W58XC4C12A	Breaker – Garmin GMA 245R Audio Panel	5A
B:AUX	W58XC4C12A5	Breaker - Auxiliary Power	5A
B:COM1	W58XC4C12A10	Breaker – GTR 200B – Communications Radio	10A
B:ECU	W58XC4C12A15	Breaker – Engine Control Unit	15A
B:ELT	W58XC4C12A1	Breaker - ELT	1A
B:ESS	W58XC4C12A5	Breaker - ESS	5A
B:ESSB	W58XC4C12A1	Breaker - ESS Backup	10A
B:FLAP	W58XC4C12A5	Breaker – Flap Motor	5A
B:FUELB	W58XC4C12A15	Breaker – Boost Fuel Pump	15A
B:FUELP	W58XC4C12A15	Breaker – Primary Fuel Pump	15A
B:GNX	W58XC4C12A5	Breaker – GNX 375 – Transponder/GPS	5A
B:IPAD	W58XC4C12A5	Breaker – iPad Mount	5A
B:LANDL	W58XC4C12A5	Breaker – Landing Lights	5A
B:NAV1	W58XC4C12A2	Breaker – VAL Nav 2000 – VOR/ILS/GS	2A
B:NAVL	W58XC4C12A7	Breaker – Navigation Lights	7A
B:PITOT	W58XC4C12A15	Breaker – Pitot Heat	15A
B:TAXIL	W58XC4C12A5	Breaker – Taxi Lights	5A
B:TRIM	W58XC4C12A1	Breaker – Trim Motor (Elevator)	1A
B:YAW	W58XC4C12A?	Breaker – Yaw Servo	2A
R:FUELB		Relay – Boost Fuel Pump
R:FUELP		Relay – Primary Fuel Pump
R:MSTR	11-03161	Relay/Contactor – Master Battery Solenoid
RS:INST		Rheostat/Switch – Instrument Lights	10k
RS:INTER		Rheostat/Switch – Interior Lights	10k
RS:PANEL		Rheostat/Switch – Panel Lights	10k
S:AMSTR	SA-803	Switch – Avionics Master – Off/On	SPST, Guarded
S:AP	SA-803	Switch - Autopilot – Off/On	SPST
S:BOOST	SA-803	Switch – Boost Pump – Off/On	SPST
S:ECU	SA-803	Switch – ECU – Off/On	SPST, Guarded
S:EMERG		Push Button – Emergency – Momentary On	SPST
S:ESS	SA-803	Switch - ESS Bus	SPST
S:IGN1	SA-803	Switch – Ignition 1 – Off/On	SPST, Guarded
S:IGN2	SA-803	Switch – Ignition 2 – Off/On	SPST, Guarded
S:LAND	SA-804	Switch – Landing Light/Off/Recognition Light	SPDT
S:MDIS	SA-803	Switch - Motor Disconnect	SPST
S:MSTR	SA-803	Switch – Master – Off/On	SPST, Guarded
S:NAVL	SA-804	Switch – Navigation/Strobe Lights – Navigation/Off/Strobes and Navigation	SPDT
S:PITOT	SA-803	Switch – Pitot Heat – Off/On	SPST
S:PLAY		Push Button - Play Last ATC Transmission - Momentary On	SPST
S:TAXI	SA-803	Switch – Taxi Light – Off/On	SPST
S:TOGA		Push Button – Takeoff/Go-Around – Momentary On	SPST

Engine Wiring

The engine wiring is the battery contactor to the engine and all wires connecting to the engine including the ECU and sensors.

Devices

ACK 406/121.5 E-04 ELT

• Description: 121.5/406 MHz ELT
• General Documentation: ACK/e04install.pdf
• Interconnect Drawings: GIM-27-25–A

JELT1

Documentation: Pg. 7-8

Pin	Description
1	Aircraft Power (10-30V)
2	RS-232 TX
3	Ground
4	RS-232 RX

Configuration

J1 and J2 should have no jumpers installed for 9600 BPS NMEA input. Pg. 7.

AeroLEDs Pulsar EXP Nav/Position/Strobe Lights

Pin 1 = Red -> W/O = Nav Pin 2 = Yellow -> W/B = Strobe Pin 3 = Green -> W = Sync Pin 4 = Black -> Shield

AeroLEDs SunSpot 36 HX Lighting

Bose LEMO Connector

6-pin stereo powered headset connector.

JBOS01

Pin	Description	Notes
1	Power	Red
2	Ground	Black
3	Audio Left	S2 (White)
4	Audio Right	S2 (Blue)
	Audio Shield	S2 (Black/White)
5	Mic Hi	S2 (White)
6	Mic Lo	S2 (Blue)
	Mic Shield	S2 (Black/White)

Comant Communications Antenna (CI-121)

Comant DME/Transponder Antenna (CI-105)

Garmin GAD 27 – Electronic Adapter Unit

Electronic flap position control, trim controller/mixer, configurable interior lighting, wig-wag lighting, and optional discrete inputs.

• General Documentation: GIM-3
• LRU Pin Documentation: GIM-26-1–9
• Interconnect Drawings:
  • GIM-27-15–A – Pitch Trim
  • GIM-27-16–A – Lighting Bus
  • GIM-27-16–B & GIM-27-16–D – Landing Lights/Recognition Lights
  • GIM-27-19 – Keep Alive Power

J271

Page: 26-1–2

Pin	Description	Notes
1	CAN Hi
2	CAN Lo
7	Aircraft Power
8	Ground
16	Motor Disconnect	Flap and Trim
18	Pilot Flap Up
19	Pilot Flap Down
20	Co-pilot Flap Up
21	Co-pilot Flap Down
24	Pilot Pitch Trim Up
25	Pilot Pitch Trim Down
26	Co-pilot Pitch Trim Up
27	Co-pilot Pitch Trim Down
34	Light 1 Switch
35	Light 2 Switch
36	Recognition Light Switch
37	Lighting 12v Source
38	Lighting Ground
39	Lighting Control In 1	Instruments
40	Lighting Control In 2	Cabin
41	Lighting Control In 3	Panel
42	Lighting Out DC	Cabin
43	Lighting Out DC	Panel
45	Lighting Out PWM	Instruments

J272

Page: 26-3

Pin	Description	Notes
1	Pitch Trim Power In
2	Pitch Trim Power Ground
11	Pitch Trim Out 1
12	Pitch Trim Out 2

TB273

Pin	Description	Wire	Notes
1	Keep Alive Power In		Aircraft power 2
2	Keep Alive Power Out		3.5A max output
3	Light 1 Power In		Left landing light
4	Light 2 Power In		Right landing light
5	Flap Power In		Breaker max of 10A
6	Flap Power Ground		Ground for flip input and output power
7	Flap Power Out 1		10A max output
8	Flap Power Out 2		10A max output
9	Light 1 Out		10A max output
10	Light 2 Out		10A max output

Notes

The GEA-24 must be used to monitor flap position for the 4-position flap switches to work.

Garmin GAD 29 – Navigation Data Adapter

IFR navigator interface to the G3X system.

• General Documentation: GIM-4
• LRU Pin Documentation: GIM-26-10–11
• Interconnect Drawings: GIM-27-37

J291

Page: 26-10

Pin	Description	Notes
1	CAN Hi
2	CAN Lo
6	Ground
7	Aircraft Power
9	Aircraft Ground

J292

Page: 26-10–11

Pin	Description	Notes
12	ARINC TX 1B
24	ARINC TX 1A
11	ARINC RX 1B
23	ARINC RX 1A

Garmin GAP 26 – Pitot/AOA Probe

Heated Pitot/AOA probe.

• General Documentation: GIM-5
• LRU Pin Documentation:
• Interconnect Drawings:

Garmin GDU 460 – Display Unit

Glass flush mounted primary flight display.

• General Documentation: GIM-8
• LRU Pin Documentation: GIM-26-19–27
• Interconnect Drawings:
  • GIM-27
  • GIM-27-4-A – Configuration Module
  • GIM-27-4-B – Setting as PFD1
  • GIM-27-4-C – GSU 25C

J4601

Pin	Description	Wire
1	CAN Bus Hi	22/S2
2	CAN Bus Lo	22/S2
4	RS-232 TX	22/S2
5	RS-232 RX	22/S2
6	Ground	22
7	Aircraft Power 1	22
8	Aircraft Power 2	22
9	Power Ground	22

J4602

Pin	Description	Wire	Notes
1	Mono Audio Out Hi	22/S1	Alert audio to Audio Panel
18	Mono Audio Out Lo	^	^
10	CDU System ID Program 1	24	Ground for PDF1

Garmin GEA 24 – EIS Interface

An input/output system used to monitor and power engine and airframe sensors.

• General Documentation: GIM-10
• LRU Pin Documentation: GIM-26-28–42
• Interconnect Drawings:

J241

Pin	Description	Notes
1	CAN Hi
2	CAN Lo
4	RS-232 Rx
5	RS-232 Tx
6	RS-232 Ground
7	Aircraft Power 1
8	Aircraft Power 2
9	Ground

J242

Pin	Description	Notes
6	CHT 4 Lo
18	CHT 4 Hi
8	CHT 3 Lo
20	CHT 3 Hi
10	CHT 2 Lo
22	CHT 2 Hi
12	CHT 1 Lo
24	CHT 1 Hi
7	EGT 4 Lo
19	EGT 4 Hi
9	EGT 3 Lo
21	EGT 3 Hi
11	EGT 2 Lo
23	EGT 2 Hi
13	EGT 1 Lo
25	EGT 1 Hi

J243

J244

• Interconnect Drawings: GIM-30-5

Pin	Description	Notes
40	Battery Fault	Discrete 1
41	Check Engine	Discrete 2
42	Low Voltage	Discrete 3
44	Master Warning	Red - Immediate Attention Needed
45	Master Caution	Yellow - Awareness, possible future correction needed

Garmin GMA 245R – Remote Mount Audio Panel

A high-fidelity digital audio panel that collects, processes, and distributes audio signals to crew and passengers.

• General Documentation: Garmin/GMA 245 and 245R Installation Manual.pdf
• LRU Pin Documentation: Pg. 4-1–10
• Interconnect Drawings: GIM-27-46
• Current Draw: 2.1A Max (Pg. 1-5)

J2401

Pin	Description	Notes
9	COM 1 Audio In – Hi – GTR 200
10	COM 1 Audio In – Lo – GTR 200
12	COM 1 Mic Key Out	Grounds on activation
17	NAV 1 Audio In – Hi – GNX 375?
18	NAV 1 Audio In – Lo – GNX 375?
19	NAV 2 Audio In – Hi – VAL NAV 2000?
20	NAV 2 Audio In – Lo – VAL NAV 2000?
31	Alert Audio In – Hi
32	Alert Audio In – Lo
33	Pilot Mic Audio In – Hi
34	Pilot Mic Key In	Ground to activate
35	Pilot Mic Audio In – Lo
36	Can Hi
37	Can Lo

J2402

Pin	Description	Notes
1	Pilot Headset Audio Out – Lo
2	Co-Pilot Headset Audio Out – Lo
3	Co-Pilot Headset Audio Out – Left
4	Co-Pilot Headset Audio Out – Right
8	Aircraft Power 1
10	Power Ground
16	Pilot Headset Audio Out – Left
22	Play Key	Ground to activate
23	Music 1 In – Left
24	Music 1 In – Right
25	Music 1 In – Lo
31	Pilot Headset Audio Out – Right
32	Co-Pilot Mic Audio In – Hi
33	Co-Pilot Mic Key – In	Ground to activate
34	Co-Pilot Mic Audio In – Lo
29	Alert Audio 2 Hi (Failsafe)	Connected if power is lost
14	Alert Audio 2 Lo (Failsafe)

Garmin GMC-507

Garmin Automatic Flight Control System (AFCS) Mode Controller.

• General Documentation: GIM-14
• LRU Pin Documentation: GIM-26-49–50
• Interconnect Drawings: GIM-27-10

J7001

Pin	Description	Notes
3	CAN Bus Hi
4	CAN Bus Lo
7	Aircraft Power 1
10	TO/GA Discrete In
11	Lighting Bus Hi
15	Power Ground

Garmin GMU-11

Remote mounted magnetometer.

• General Documentation: GIM-15
• LRU Pin Documentation: GIM-26-51–52
• Interconnect Drawings: GIM-27-

JXXX

Pin	Description	Notes
1	CAN Bus Hi
2	CAN Bus Lo
6	Signal Ground
7	Aircraft Power
9	Ground

Garmin GNX-375

• General Documentation: Garmin G3X/GNX 375 Maintenance Manual.pdf
• LRU Pin Documentation: 5-22–24
• Interconnect Drawings: GIM-27-37 – GSU 25C, GDU 460, GAD 29

NOTE: The GNX-375 has 5 RS-232 serial ports. Can it be used to drive the ACK ELT freeing up one RS-232 port on the G3X?

J3751

Pin	Description	Notes
20	Aircraft Ground
41	Aircraft Ground
38	Power Control	Ground to turn on GNX upon receiving power
21	Aircraft Power	All aircraft power tied through 5A breaker
42	Aircraft Power	All aircraft power tied through 5A breaker
1	Config Module Clock
22	Config Module Data
23	Config Module Ground
43	Config Module Power
9	RS-232 3 TX	Transponder Format 1 – GSU 25C
31	RS-232 3 RX	^
52	RS-232 3 Ground	^
27	ARINC 429 In 1A	EIS/AIRDATA – GAD 29
28	ARINC 429 In 1B	^
46	Audio Out
47	Audio Ground
15	Discrete In 1
16	Discrete I/O 2
36	Ident	Discrete In
37	Audio Mute	Discrete In
57	Air/Ground	Discrete In

J3752

Pin	Description	Notes
30	Aircraft Ground
44	Aircraft Power	All aircraft power tied through 5A breaker
1	ARINC 429 Out 1A	GAMA Format 1 – GAD 29C
2	ARINC 429 Out 1B	^
5	RS-232 1 TX	MAPMX Format 1 – GDU 460
20	RS-232 1 RX	^
34	RS-232 1 Ground	^
6	RS-232 2 TX	CONNEXT 5700 – GDU 460
21	RS-232 2 RX	^
35	RS-232 2 Ground	^
14	Discrete In 2
15	Remote Go Around

Garmin GSA-28 – (P/R/Y)

A direct drive flight-control auto pilot servo.

• General Documentation: GIM-18
• LRU Pin Documentation: GIM-26-56–58
• Interconnect Drawings: GIM-27-10

J281 (P/R/Y)

Pin	Description	Notes
1	CAN Bus Hi
2	CAN Bus Lo
5	ID Strap 1
6	ID Strap 2
7	ID Strap 3
8	ID Strap 4
9	Aircraft Ground
10	Aircraft Power
11	Trim In 1	Up
12	Trim In 2	Down
13	Trim Out 1	Maximum 1A
14	Trim Out 2	Maximum 1A
15	CWS/Disconnect

• ID Strap Jumpers
  • Roll Servo – No Jumper
  • Pitch Servo – ID Strap 1 (5) -> ID Strap 4 (8)
  • Yaw Servo – ID Strap 2 (6) -> ID Strap 3 (7)

Garmin GSU-25C

Supply AHRS and Air Data information to the G3X system.

• General Documentation: GIM-19
• LRU Pin Documentation: GIM-26-59–62
• Interconnect Drawings:
  • GIM-27-4-C – GDU 460
  • GIM-27-4-D – GTP 59 Temperature Probe
  • GIM-27-37-B – GNX 375

J251

Pin	Description	Notes
1	CAN Bus Hi
2	CAN Bus Lo
4	RS-232 1 RX	GDU Backup Communications
5	RS-232 1 TX	^
6	Ground
7	Aircraft Power 1
8	Aircraft Power 2
9	Ground

J252

Pin	Description	Notes
1	OAT Power
2	OAT Hi
3	OAT Lo
9	RS-232 3 TX	GTX pressure altitude data
10	RS-232 3 RX	^
11	RS-232 3 Ground	^

Garmin GTR-200B

Communications Radio

• General Documentation: Garmin G3X/GTR 200 Installation Manual.pdf
• LRU Pin Documentation: 4-1–7
• Interconnect Drawings:

Ray Allen G407

7 switch stick grip.

JRAG407 (P & C)

• P: Pilot Stick Grip
• C:Co-pilot Stick Grip

Pin	Description	Wire	Notes
1	Red - Elevator Trim Down	24
2	Orange -Flap Up	24
3	Green - Elevator Trim Up	24
4	Blue - Flap Down	24
5	Yellow - AP Disconnect	24
6	Gray - CWS	24
7	Black - Ground	24
8	White - PTT	24

Ray Allen T2-7A

Pitch Trim Motor

Wired to 5 conductor cable to tail.

Servo Wire Color	Cable Color	Rear Connector Pin	Description
Gray	Black	1	Motor Power (+/-)
White	White	2	Motor Power (+/-)
Orange	Red	3	+5 V
Blue	Brown	4	Signal (wiper)
Green	Green	5	Ground

Pins 1 and 2 move the motor. Changing polarity causes the motor to run in the opposite direction.

VAL Avionics NAV-2000

VOR/ILS/GS Receiver

• General Documentation: VAL Avionics/NAV 2000 Installation Manual.pdf
• LRU Pin Documentation: Pg 19

JV2000

Pin	Description	Wire	Notes
1	Power	22
2	Ground	22
3	Serial Ground	24/S3
4	RS-232 RX	24/S3
5	RS-232 TX	24/S3
20	Audio Ground	24/S2
23	Audio Out	24/S2

28 Pin Bulkhead Connector

CHT/EGT Probe Red (-) and Yellow (+).

BLK01

Pin	Description	Wire	Notes
1	Battery Fault
2	CHT 1 +	HEAT/2/Y
3	CHT 1 GND	HEAT/2/R
4	CHT 2 +	HEAT/2/Y
5	CHT 2 GND	HEAT/2/R
6	CHT 3 +	HEAT/2/Y
7	CHT 3 GND	HEAT/2/R
8	Master Switch	22
9	CHT 4 +	HEAT/2/Y
10	CHT 4 GND	HEAT/2/R
11	EGT 1 +	HEAT/2/Y
12	EGT 1 GND	HEAT/2/R
13	EGT 2 +	HEAT/2/Y
14	EGT 2 GND	HEAT/2/R
15	EGT 3 +	HEAT/2/Y
16	EGT 3 GND	HEAT/2/R
17	EGT 4 +	HEAT/2/Y
18	EGT 4 GND	HEAT/2/R
19	Shunt Hi	22
20	Shunt Lo	22
21	Start Switch	22
22	Start Power 1	22
23	Start Power 2	22
24	Start Indicator	24
25	Boost Pump Indicator	24

Device Configuration

Garmin GDU-460 Configuration

Flap Configuration

See GIM-26-6, GIM-35-4-14

RS-232 Configuration

See GIM-35-131–134

J4601 contains a dedicated RS-232 port for backup communication with the GSU 25C (AHRS). It does not have to consume one of the 5 configurable RS-232 ports below.

RS-232 Port Configurations:

1. NMEA Out – ACK ELT

ARINC 429 Configuration

See GIM-35-135–136

Audio Panel Configuration

See GIM-35-143–146

• “Audio Panel Type”: “GMA 245R”
• “On-Screen Controls”: “Show”
• “Intercom 3D Audio”: “Enable”
• “Speaker”: “Disable”

COM Radio Configuration

See GIM-35-147–148

• “COM1”
  • “Connect on”: “Network Radio LRU 1”

NAV Radio Configuration

See GIM-35-150

• “NAV Radio Sources”: “NAV 1 + 2”

TODO: How do we configure the VAL Nav 2000 and GTX 375 as both NAV radios.

Transponder Configuration

See GIM-35-151–153

• “Transponder Type”: “GNX 375”

See GIM-27-37

GEA 24 – Trim/Flap Position Configuration

See GIM-35-175–176

GEA 24 – Discrete Inputs Configuration

See GIM-35-183–185

• “Discrete 1”: “AFCS TO/GA” ?

Exgternal Lights Configuration

See GIM-35-193

• “Flash Selection”: “Flash Both Lights”
• “Automatic Flashing”: “57kts” – 65 MPH
• “Light Priority”: “Switch”

GNX 375 Crossfill Configuration

See GIM-35-206

Garmin GNX-375 Configuration

See GIM-35-200–203, GIM-35-206

Garmin GTR-200B Configuration

Device Communication Wiring

CAN BUS

X	Source	Source Label	Description
X	GDU 460	GDUGAD7	(Flight Display)
X	GAD 27	GAD7GEA	(Electrical Control Module)
X	GEA 24	GEAGTR	(Engine Information System)
X	GTR 200	GTRGAD9
X	GAD 29	GAD9GMA	(ARINC Navigation Data Translator)
X	GMA 245	GMAGMC	(Audio Panel)
X	GMC 507	GMCGSAR	(Auto Pilot Control Head)
	GSA 28/R	GSARGSAP	(Roll AP Servo)
	GSA 28/P	GSAPGSAY	(Pitch AP Servo)
X	GSU 25C	GSUGMU	(AHRS)
X	GMU 11		(Magnetometer)

• Labels should be reversed on destination side of the wire.

RS-232

• GDU 460 -> GSU 25C (RS-232 on J4601 – Garmin Instrument Data – Always Set)
• GDU 460 -> GEA 24 (RS-232 1 – Garmin Instrument Data)
• GDU 460 -> ACK E-04 (RS-232 2 – NMEA)
• GDU 460 -> VAL NAV 2000 (RS-232 3 – Garmin Nav/Comm)
• GDU 460 -> GTX 375 (RS-232 4 – MAPMX)
• GDU 460 -> GTX 375 (RS-232 5 – CONNEXT)

Antenna Wiring List

X	Source	Connector	Connector	Destination	Notes
X	GDU 460	BNC	N/A	GA-27C	GPS
X	GTR 200	BNC	BNC	CI-121	Communications 118-136Mhz
X	GNX 375	BNC	BNC	CI-105	Transponder 1.5GHz
X	GNX 375	TNC	TNC	GA 35	GPS 1.15GHz
	NAV 2000	BNC	?	?	VOR/ILS/GS

Master Avionics Status

X	Device	Notes
X	GMC 507
X	VAL NAV 2000
X	GNX 375
X	GDU 460
X	GTR 200B
/	ELT	Need to mount antenna
X	CO Detector

Wing Wiring

Common Wiring

Connector 1 (12-pin)

Pin	Purpose
1	Strobe/Nav Light Ground - Shield
2	Strobe Light Positive - W/B
7	Strobe Sync Line - W
8	Nav Light Positive - W/O
3	Wing Ground
9	Fuel Line Sense

Left Wing

Connector 1 - Special Connections (12-pin)

Pin	Purpose
4	Magnetometer Positive
5	Magnetometer Negative
11	Magnetometer CAN BUS Shield
6	Magnetometer CAN BUS LO
12	Magnetometer CAN BUS HI

Connector 2 - Pitot Heat (2-pin)

Pin	Purpose
1	Pitot Positive
2	Pitot Negative

Right Wing

Connector 1 - Special Connections (12-pin)

Pin	Purpose
11	Taxi Light Positive
5	Taxi Light Negative
12	Landing Light Positive
6	Landing Light Negative

Master Wiring List

X	Device	Source	S. Label	Wire	D. Label	Destination
-	Power
X		BAT+				R:MSTR.IN
X		S:MSTR.1		24		Ground
X		S:MSTR.2		24		R:MSTR.SIG
X		R:MSTR.OUT		12		MBUS
X	AV Master	MBUS	MBUS	16	S:AVMSTR	S:AVMSTR.0
X		S:AVMSTR.1	BS:AVMSTR	16	AVMSTR +	BS:AVMSTR (breakers)
X	ESS	MBUS		16		S:ESS.0
X		S:ESS.1		20		B:ESS.1
X		S:ESS.1		20		B:ESSB.1
X	FUEL PUMPS	MBUS	FP:PRI +	14	MBUS	B:FUELP.1
X		B:FUELP.2	FUELP +	14	FUELP +	R:FUELP.1
X		MBUS	FP:BOOST +	14	MBUS	B:FUELB.1
X		B:FUELB.2	FUELB +	14	FUELB +	R:FUELB.1
X	GAD 27	B:ESS.2	GAD7 +1	22	B:ESS +	J271.7
X		B:ESSB.2	GAD7 +2	22	B:ESSB +	TB273.1
X		Ground	GAD7 Ground	22	Ground	J271.8
X	GAD 29	B:GNX	GAD9 +1	22	B:GNX +	J291.7
X		Ground	GAD9 Ground	22	Ground	J291.9
X	GDU 460	B:ESS.2	GDU +1	22	B:ESS +	J4602.32
X		TB273.2	GDU +2	22	ESSB +	J4602.31
X		Ground	GDU Ground	22	Ground	J4602.15
X	GEA 24	B:ESS.3		22		J241.7
X		TB273.2	GEA +2	22	ESSB +	J241.8
X		Ground	GEA Ground	22	Ground	J241.9
X	GMA 245	B:AUDIO.2	GMA +1	22	B:AUDIO +	J2402.8
X		B:AUDIO.2	GMA +1	22	B:AUDIO +	J2402.9
X		Ground	GMA Ground	22	Ground	J2402.10
X		Ground	GMA Ground	22	Ground	J2402.11
X	GMC 507	B:AP.2	GMC +1	22	B:AP +	J7001.7
X		Ground	GMC Ground	22	Ground	J7001.15
X	GNX 375	B:GPS.2	GNX Power	22	B:GPS +	J3751.21
X		J3751.21	GNX Power	22	B:GPS +	J3751.42
X		J3751.21	GNX Power	22	B:GPS +	J3752.44
X		Ground	GNX Ground	22	Ground	J3751.20
X		J3751.20	Ground	22	Ground	J3751.41
X		J3751.20	Ground	22	Ground	J3752.30
X		J3751.20	Ground	22	Power Control	J3751.38
X	GSU 25C	B:ESS.2	GSU 25C +1	22	B:ESS+	J251.7
X		TD273.2	GSU 25C +2	22	ESSB +	J251.8
X		Ground	GSU Ground	22	Ground	J251.9
X	GTR 200B	B:COM1.2	COM1 +	22	B:COM1 +	J2001.1
X		Ground	COM1 Ground	22	Ground	J2001.20
X	NAV 2000	BS:AVMSTR	BS:AVMSTR	22	B:NAV1	B:NAV1.1
X		B:NAV1.2	B:NAV1	22	NAV1 +	JV2000.1
X		Ground	NAV1 GND	22	GND	JV2000.2
X	FLAPS	MBUS	Flap PWR	16	Flap PWR	B:FLAPS.1
X		B:FLAPS.2	Flap PWR	16	Flap PWR	TB273.5
X		AIRFRAME	Flap GND	16	Flap GND	TB273.6
X		TB273.7	Flap PWR 1	16	Flap PWR 1	FMTR.RED
X		TB273.8	Flap PWR 2	16	Flap PWR 2	FMTR.BLACK
X	USB	B:AUX.2	USB PWR	16	USB PWR	USB.PWR
X		GND	USB GND	16	USB GND	Airframe
-	CAN Bus
X	ULP ECU				GEA (HI)	J244.17
X					^(LO)	J244.33
X					^(GND)	J244.2
-	RS-232
X	GEA 24	J241.5	GDU 232-1 (RX)	24/S3(W/B)	GEA 232 (TX)	J4602.47
X		J241.4	GDU 232-1 (TX)	^(W/O)	GEA 232 (RX)	J4602.48
X		J241.6	GDU 232-1 (GND)	^(W/G)	GEA 232 (GND)	J4602.44
X		J241.Block		^(SHIELD)		J4602.Block
X	GSU 25C	J251.5	GDU 232-0 (RX)	24/S3(W/B)	GSU 232 (TX)	J4601.5
X		J251.4	GDU 232-0 (TX)	^(W/O)	GSU 232 (RX)	J4601.4
X		J251.6	GDU 232-0 (GND)	^(W/G)	GSU 232 (GND)	J4601.6
X		J251.Block		^(SHIELD)		J4601.Block
X	ELT	NC	GDU 232-2 (RX)	24/S3(W/B)	ELT 232 (TX)	J4602.14
X		JELT.4	GDU 232-2 (TX)	^(W/O)	ELT 232 (RX)	J4602.30
X		JELT.3	GDU 232-2 (GND)	^(W)	ELT 232 (GND)	J4602.36
X		NC		^(SHIELD)		J4602.Block
X	NAV 2000	JV2000.5	GDU 232-3 (RX)	24/S3(W/B)	NAV 232 (TX)	J4602.29
X		JV2000.4	GDU 232-3 (TX)	^(W/O)	NAV 232 (RX)	J4602.13
X		JV2000.3	GDU 232-3 (GND)	^(W)	NAV 232 (GND)	J4602.27
X		J251.Block		^(SHIELD)		J4602.Block
X	GNX 375 (MAPMX)	J3752.5	GDU 232-4 (RX)	24/S3(W/B)	GTX 232-1 (TX)	J4602.23
X		J3752.20	GDU 232-4 (TX)	^(W/O)	GTX 232-1 (RX)	J4602.40
X		J3752.34	GDU 232-4 (GND)	^(W)	GTX 232-1 (GND)	J4602.34
X		J3752.Block		^(SHIELD)		J4602.Block
X	GNX 375 (CONNEXT)	J3752.6	GDU 232-5 (RX)	24/S3(W/B)	GTX 232-2 (TX)	J4602.24
X		J3752.21	GDU 232-5 (TX)	^(W/O)	GTX 232-2 (RX)	J4602.41
X		J3752.35	GDU 232-5 (GND)	^(W)	GTX 232-2 (GND)	J4602.35
X		J3752.Block		^(SHIELD)		J4602.Block
X	GNX 375 (GSU)	J252.9	XPDR Data (TX)	24/S3(W/B)	XPDR Pressure Data (RX)	J3751.31
X		J252.10	^ (RX)	^(W/O)	^ (TX)	J3751.9
X		J252.11	^ (Ground)	^(W)	^ (Ground)	J3751.52
X	ELT	B:ELT	ELT +	22	ELT +	JELT.1
X		J4602.13	ELT GPS TX (3)	24/S2(W/B)	GPS RX	JELT.4
X		J4602.34	^ (Ground)	^(W)	^ (Ground)	JELT.3
X	Pilot Grip	JRAG407P.1	P:Pitch T Dn	24	P:Pitch T Dn	J271.25
X		JRAG407P.2	P:Flap Up	24	P:Flap Up	J271.18
X		JRAG407P.3	P:Pitch T Up	24	P:Pitch T Up	J271.24
X		JRAG407P.4	P:Flap Dn	24	P:Flap Dn	J271.19
/		JRAG407P.5	P:Left	24	P:Left	AP DISC
X		JRAG407P.6	P:Right	24	P:Right	J271.10
X		JRAG407P.7	P:GND	24	P:GND	GND
X		JRAG407P.8	P:PTT	24(W)	P:PTT	J2401.34
X	Co-Pilot Grip	JRAG407C.1	CP:Pitch T Dn	24	CP:Pitch T Dn	J271.27
X		JRAG407C.2	CP:Flap Up	24	CP:Flap Up	J271.20
X		JRAG407C.3	CP:Pitch T Up	24	CP:Pitch T Up	J271.26
X		JRAG407C.4	CP:Flap Dn	24	CP:Flap Dn	J271.21
X		JRAG407C.5	CP:Left	24	CP:Left	J271.11
/		JRAG407C.6	CP:Right	24	CP:Right	AP DISC
X		JRAG407C.7	CP:GND	24		GND
X		JRAG407C.8	PTT	24(W)		J2402.33
X	LEMO Pilot	B:GMA	Pilot Headset Power	24	Power	JBOS01P.1
X		Ground	Pilot Headset Ground	24	Ground	JBOS01P.2
X	LEMO Co-Pilot	B:GMA	Co-Pilot Headset Power	24	Power	JBOS01C.1
X		Ground	Co-Pilot Headset Ground	24	Ground	JBOS01C.2
-	GAD 27
X	Lighting	J271.42	LIT REF1	24	LIT REF1	J2001.3, J3751.19, J7001.11
X		J3751.40	LIT GND	24	LIT GND	GND
X		J271.43	LIT REF2	24	LIT REF2	J4602.43
		J271.45	PLB 1	24	PLB 1	MAP LIGHT PWR
		GND	GND	24	GND	MAP LIGHT GND
		J271.46	PLB 2	24	PLB 2	PANEL RED LED PWR
		GND	GND	24	GND	PANEL RED LED GND
X	Switches	S:MDISABLE.1	GND	24	GND	GND
X		S:MDISABLE.2	GAD	24	S:MDIS	J271.16
X		S:LNDGL.1	LNDG LIT	24	LNDG LIT	J271.34
X		S:LNDGL.2	GND	24	GND	GND
X		S:LNDGL.3	RECN LIT	24	RECN LIT	J271.36
X		S:TAXIL.1	GND	24	GND	GND
X		S:TAXIL.2	TAXI LIT	24	TAXI LIT	J271.35
X		BLK01.24	START IND	24	START IND	J271.13
X		BLK01.25	BPUMP IND	24	BPUMP IND	J271.14
X		S:PITOT.2	PITOT IND	24	PITOT IND	J271.49
X	External Lights	BS:MSTR	B:LNDG	20	BS:MSTR	B:LNDG.1
X		B:LNDG.2	GAD LNDG	20	B:LNDG	TB273.3
X		TB273.9	LNDG PWR	20	LNDG PWR	RWING.1
X		BS:MSTR	B:TAXI	20	BS:MSTR	B:TAXI.1
X		B:TAXI.2	GAD TAXI	20	B:TAXI	TB273.4
X		TB273.10	TAXI PWR	20	TAXI PWR	RWING.2
	Elev Trim	B:ELEVT.2	ELEV TRIM PWR	24	ELEV TRIM PWR	J272.1
		GND	ELEV TRIM GND	24	ELEV TRIM GND	J272.2
/		J272.11	ELEV TRIM ONE	24	ELEV TRIM ONE
/		J272.12	ELEV TRIM TWO	24	ELEV TRIM TWO
-	GDU 460
X		J4602.27	PFD1 Set	24		J2402.10
-	GEA 24
		S:BOOST.2	BOOST PUMP IND	24	BOOST PUMP IND	J244.43
/	Elev Trim Pos	J244.18	ELE TPOS +5	24	ELE TPOS +5
/		J244.19	ELE TPOS SIG	24	ELE TPOS SIG
/		J244.20	ELE TPOS GND	24	ELE TPOS GND
X	Flap Pos	J244.21	FLP POS (+5)	24	FLP POS (+5)	Orange
X		J244.22	FLP POS (SIG)	24	FLP POS (SIG)	Green
X		J244.23	FLP POS (GND)	24	FLP POS (GND)	Blue
X	Fuel Senders		FUEL L PWR	24	FUEL L PWR	J244.5 (1)
X			FUEL L SIG	24	FUEL L SIG	J244.6
X			FUEL R PWR		FUEL R PWR	J244.8 (2)
X			FUEL R SIG		FUEL R SIG	J244.9
-	GMA 245
X	Miscellaneous	J2402.22	S:PLAY.2	24	GMA PLAY	S:PLAY.2
X		S:PLAY.1	S:PLAY GND	24	GND	GND
X	Speaker	J2402.44	Speaker (Hi)	24/S2(W/B)	GMA Speaker	Speaker +
X		J2402.43	Speaker (Lo)	24/S2(W)	^ (Lo)	Speaker -
X	CO DETECTOR		ALRT AUD	24/S2(W/B)	GDU AUD	J2401.29
X				^(W)	^	J2401.43
X				^(SHIELD)	^	J2401.Block
X	GDU	J4602.1	ALRT AUD	24/S2(W/B)	GDU AUD	J2402.15
X		J4602.18		^(W)	^	J2402.14
X				^(SHIELD)	^	J2402.Block
X	GNX	J3751.46	ALRT AUD	24/S2(W/B)	GNX AUD	J2401.31
X		J3751.47		^(W)	^	J2401.32
X		J3751.Block		^(SHIELD)	^	J2401.Block
X	GTR	J2001.10	GMA AUD	24/S2(W/B)	COM1 AUD	J2401.9
X		J2001.29		^(W)	^	J2401.10 (CHAIN)
X				^(SHIELD)	^	J2401.Block
X		J2001.17	GMA MIC	24/S2(W/B)	COM1 MIC	J2401.11
X		J2001.36		^(W)	^	J2401.10 (CHAIN)
X				^(SHIELD)	^	J2401.Block
X		J2401.12	COM1 KEY	24	GMA KEY	J2001.35
X	NAV2000	JV2000.23	AUD	24/S2(W/B)	NAV1 AUD	J2401.19
X		JV2000.20		^(W)	^	J2401.20
X				^(SHIELD)	^	J2401.Block
X	Pilot	J2401.33	Pilot Mic (Hi)	24/S2(W)	Pilot Mic (Hi)	JBOS01P.5
X		J2401.35	^ (Lo)	^(W/B)	^ (Lo)	JBOS01P.6
X		J2401.Block	^ (Shield)	(^SHIELD)	^ (Shield)	JBOS01P.Shield
X		J2402.16	Pilot Audio (Left)	24/S2(W)	Pilot Audio (Left)	JBOS01P.3
X		J2402.31	^ (Right)	^(W/B)	^ (Right)	JBOS01P.4
X		J2402.Block	^	^ (SHIELD)	^	N/C
X		B:AUD.2	HEADSET PWR	22	HEADSET PWR	JBOS01P.1, JBOS01C.1
X		J2402.Block	HEADSET GND	22	HEADSET GND	JBOS01P.2, JBOS01C.2
X	Co-Pilot	J2402.32	Co-Pilot Mic (Hi)	24/S2(W)	Co-Pilot Mic (Hi)	JBOS01C.5
X		J2402.34	^ (Lo)	^(W/B)	^ (Lo)	JBOS01C.6
X		J2402.Block	^ (Shield)	(^SHIELD)	^ (Shield)	JBOS01C.Shield
X		J2402.3	Co-Pilot Audio (Left)	24/S3(W)	Co-Pilot Audio (Left)	JBOS01C.3
X		J2402.4	^ (Right)	^(W/B)	^ (Right)	JBOS01C.4
X		J2402.Block	^	^ (SHIELD)	^	N/C
X	GMC 507	S:TOGA.1	GND	24	S:TOGA GND	Ground
X		S:TOGA.2	S:TOGA	24	S:TOGA	J7001.10
X	GNX 375	J3751.43	Config Power	24		CFG.Red
X		J3751.23	Config Ground	^		CFG.Blk
X		J3751.22	Config Data	^		CFG.Yel
X		J3751.1	Config Clock	^		CFG.Wht
X		J3751.15	S:TOGA	24	S:TOGA	S:TOGA.2
X		J3752.29	S:DEMO	24	S:DEMO.2
X		S:DEMO.1	GND	24	S:DEMO GND	GND
X		J3752.43	S:TEST	24	S:TEST.2
X		S:TEST.1	GND	24	S:TEST GND	GND
X	GAD9	J292.24	Air Data TX (TX 1A)	24/S2(W/B)	Air Data RX (1A)	J3751.27
X		J292.12	^ (TX 1B)	^(W)	^ (1B)	J3751.28
X		J292.Block		^(Shield)		J3751.Block
X		J3752.1	GPS Data RX (1A)	24/S2(W/B)	GPS Data TX (1A)	J292.23
X		J3752.2	^ (1B)	^(W)	^ (1B)	J292.11
X		J3752.Block		^(Shield)		J292.Block
-	FW Block
X		CHT1.Y	CHT 1(+)	24	CHT 1(+)	BLK01.2
X		CHT1.R	^(-)	24	^(-)	BLK01.3
X		CHT2.Y	CHT 2(+)	24	CHT 2(+)	BLK01.4
X		CHT2.R	^(-)	24	^(-)	BLK01.5
X		CHT3.Y	CHT 3(+)	24	CHT 3(+)	BLK01.6
X		CHT3.R	^(-)	24	^(-)	BLK01.7
X		CHT4.Y	CHT 4(+)	24	CHT 4(+)	BLK01.9
X		CHT4.R	^(-)	24	^(-)	BLK01.10
X		EGT1.Y	EGT 1(+)	24	EGT 1(+)	BLK01.11
X		EGT1.R	^(-)	24	^(-)	BLK01.12
X		EGT2.Y	EGT 2(+)	24	EGT 2(+)	BLK01.13
X		EGT2.R	^(-)	24	^(-)	BLK01.14
X		EGT3.Y	EGT 3(+)	24	EGT 3(+)	BLK01.15
X		EGT3.R	^(-)	24	^(-)	BLK01.16
X		EGT4.Y	EGT 4(+)	24	EGT 4(+)	BLK01.17
X		EGT4.R	^(-)	24	^(-)	BLK01.18
X		SHUT.1	SHUNT (+)	22	SHUNT (+)	BLK01.19
X		SHUT.2	^ (-)	22	^(-)	BLK01.20
X		BATTERY.FAULT	BAT FAULT	22	BAT FAULT	BLK01.1
X		BLK01.24	START IND	24	START IND	R:START.1
X		BLK01.25	BPUMP IND	24	BPUMP IND	R:BPUMP.1
/		BLK01.26	CONST PWR	22	CONST PWR
-	GEA 24
X		J244.44	Warn GND	24	GEA GND	Warn.-
X		MBUS		24	MBUS PWR	Warn.+
X		J244.45	CAUT GND	24	GEA GND	Caut.-
X		MBUS		24	MBUS PWR	Caut.+
X		BLK01.2	CHT 1(+)	24	CHT 1(+)	J242.24
X		BLK01.3	^(-)	24	^(-)	J242.12
X		BLK01.4	CHT 2(+)	24	CHT 2(+)	J242.22
X		BLK01.5	^(-)	24	^(-)	J242.10
X		BLK01.6	CHT 3(+)	24	CHT 3(+)	J242.20
X		BLK01.7	^(-)	24	^(-)	J242.8
X		BLK01.9	CHT 4(+)	24	CHT 4(+)	J242.18
X		BLK01.10	^(-)	24	^(-)	J242.6
X		BLK01.11	EGT 1(+)	24	EGT 1(+)	J242.25
X		BLK01.12	^(-)	24	^(-)	J242.13
X		BLK01.13	EGT 2(+)	24	EGT 2(+)	J242.23
X		BLK01.14	^(-)	24	^(-)	J242.11
X		BLK01.15	EGT 3(+)	24	EGT 3(+)	J242.21
X		BLK01.16	^(-)	24	^(-)	J242.9
X		BLK01.17	EGT 4(+)	24	EGT 4(+)	J242.19
X		BLK01.18	^(-)	24	^(-)	J242.7
X		BLK01.1	BAT FAULT	22	BAT FAULT	J244.40
X		ECU (Y/W/W)	CHK ENG	22		J244.41
X		ECU (Y/W/B)	ECU BAT VLOW	22		J244.42
X		BLK01.19	SHUNT (+)	24	SHUNT (+)	J243.36
X		BLK01.20	^ (-)	24	^ (-)	J243.37
X		BLK01.21	START TRIGGER	22	START TRIGGER	S:START.2
X		BLK01.22	START RELAY +1	22	START RELAY +1	R:START +
X		BLK01.23	START RELAY +2	22	START RELAY +2	R:START +
X		R:START + OUT	START TRIGGER OUT	16	START TRIGGER OUT	R:START OUT
	Panel Misc
X	Nav/Strobes	BS:MSTR	B:STRBS PWR	20	BS:MSTR	B:STRBS.1
X		B:STRBS.2	SW:STRBS	20	B:STRBS	SW:STRBS.2
X		SW.STRBS.3	STRBS PWR	20	STRBS PWR	WING L/R
X		SW.STRBS.1	NAV PWR	20	NAV PWR	WING L/R
X		BS:MSTR	B:PITH.1	16	BS:MSTR
X	Pitot Heat	B:PITH.2	PITOT HEAT PWR	16
X	Fuel Sel

Programming

Gauge Setup

[ ] Battery Fault [ ] Check Engine [ ] ECU Battery Low [ ] CHT [ ] EGT [ ] Fuel Pressure [ ] Fuel Flow [ ] Oil Pressure [ ] Oil Temperature [ ] RPM

GP1 = Elevator Trim Position Sensor GP2 = Flap Trim Position Sensor