52.0A
total current draw
27
device(s)
Justin's Vans RV-10
Electrical Load Planning and VP-X Config
Aircraft Overview - Devices

The following devices represent your aircraft, and will be used to generate your personalized
electrical diagram,
VP-X pinout and electrical build
buying guide.
Instruments/Avionics
GTX 45R
|
pin name | actual current draw | circuit breaker value | min wire size |
VP-X pin | backup? | current fault detect? | switch | bank preference |
Transponder/ADSB |
1.3A |
3.0A | 20g |
J8-8 |
none |
Yes |
Avionics Master |
Bank A or B |
GMA 245
|
Audio Panel |
0.3A |
5.0A | 20g |
J8-3 |
none |
No |
Avionics Master |
Bank A or B |
G5 w/Battery
|
G5 (BU EFIS) |
0.8A |
5.0A | 20g |
J10-2 |
none |
Yes |
Avionics Master |
Bank B |
notes: Backup EFIS & ADAHRS |
GMU 11
|
Magnetometer |
0.5A |
1.0A | 20g |
J10-7 |
none |
No |
always on |
Bank A or B |
GTN 650
|
GTN 650 Nav |
2.2A |
10.0A | 18g |
J12-1 |
none |
Yes |
Avionics Master |
Bank A |
GTN 650 Comm |
0.5A |
8.0A | 18g |
J12-3 |
none |
Yes |
Avionics Master |
Bank A |
Autopilot
|
AFCS |
4.1A |
5.0A | 20g |
J8-1 |
none |
No |
Avionics Master |
Bank A or B |
notes: AFCS Mode Controller GMC 507, Pitch & Roll Servos |
GEA 24
|
EIS |
0.4A |
5.0A | 20g |
J8-4 |
Method C |
Yes |
always on |
Bank A or B |
notes: Engine Indication System (EIS) |
Accessory Block
|
AccBlock12 |
3.0A |
5.0A | 18g |
J12-8 |
none |
No |
always on |
Bank A or B |
notes: Cowl Flaps, Ram Air, Oil Damper, Stall Warning, Switch Lights, Overhead Lights, Lemo, CO2 Monitor |
GAD 29
|
ARINC 429 |
0.2A |
2.0A | 20g |
J12-10 |
none |
Yes |
Avionics Master |
Bank A or B |
notes: ARINC 429 Interface |
GSU 25
|
ADAHRS |
0.2A |
2.0A | 20g |
J1-1 |
Method C |
Yes |
always on |
Bank A |
notes: Primary ADAHRS |
GTR 20
|
Comm#2 |
0.6A |
8.0A | 18g |
J10-3 |
none |
Yes |
Avionics Master |
Bank B |
notes: Comm #2 - 7.5 Max, .6 receiving... 3.0 transmitting |
G3X GDU 460
|
G3X (PFD) |
2.0A |
5.0A | 20g |
J8-5 |
Method C |
No |
Avionics Master |
Bank A |
G3X GDU 460
|
G3X (MFD) |
2.0A |
5.0A | 20g |
J12-9 |
Method C |
No |
always on |
Bank A |
GAP 26 (-20)
|
Pitot/AOA |
0.5A |
15.0A | 14g |
J12-2 |
none |
Yes |
Pitot Heat |
Bank A or B |
notes: Heated Pitot/AOA (4 - 12 amps) |
Lights
Strobes
|
pin name | actual current draw | circuit breaker value | min wire size |
VP-X pin | backup? | current fault detect? | switch | bank preference |
Strobes |
6.0A |
10.0A | 18g |
J10-6 |
none |
No |
Strobe Lt |
Bank A or B |
notes: AeroLEDs Pulsar NS/Suntail |
Nav Lights (LED)
|
Nav Lights |
1.5A |
2.0A | 20g |
J10-8 |
none |
Yes |
Nav Lt |
Bank A or B |
notes: AeroLEDs Pulsar NS/Suntail |
Landing Lt Left
|
Landing Lt Left |
4.3A |
10.0A | 18g |
J8-2 |
none |
Yes |
Land Lt |
Bank A |
notes: AeroLEDs Aerosun VX |
Taxi Light (LED)
|
Taxi Lights |
3.4A |
5.0A | 18g |
J8-6 |
none |
Yes |
Taxi Lt |
Bank B |
notes: AeroLEDs Aerosun VX |
Landing Lt Right
|
Landing Lt Right |
4.3A |
10.0A | 18g |
J12-7 |
none |
Yes |
Land Lt |
Bank A |
notes: AeroLEDs Aerosun VX |
Accessories/Ignition/Other
Boost Pump (inj)
|
pin name | actual current draw | circuit breaker value | min wire size |
VP-X pin | backup? | current fault detect? | switch | bank preference |
BoostPump |
4.5A |
10.0A | 14g |
J10-5 |
none |
No |
Boost Pump |
Bank A or B |
notes: Airflow Performance Pump |
Garmin GSA 28
|
AP Yaw Servo |
2.8A |
3.0A | 20g |
J8-7 |
none |
No |
Avionics Master |
Bank A or B |
TCW 6ah IBBS
|
Backup Battery |
4.0A |
10.0A | 18g |
J12-12 |
none |
No |
always on |
Bank A or B |
notes: Pass-through power to two Dual USB chargers. |
Electrical System
B&C Pri Alt
|
pin name | actual current draw | circuit breaker value | min wire size |
VP-X pin | backup? | current fault detect? | switch | bank preference |
Alternator Field |
2.5A |
5.0A | 20g |
J12-11 |
none |
No |
Alternator |
Bank A |
Alternator Vsense |
0.1A |
2.0A | 20g |
J1-2 |
none |
No |
always on |
Bank A |
SD-20 BU Alt
|
Alt - BU - Field |
2.5A |
5.0A | 20g |
J10-4 |
none |
No |
BU Alternator |
Bank B |
Alt - BU - Vsense |
0.1A |
2.0A | 20g |
J10-10 |
none |
No |
always off |
Bank B |
VP-X Pinout and Configuration
Currently configuring
VP-X Pro, 14 volt.
All device pins assigned!
J8 |
| pin |
bank |
VP-X pin name |
power pin name | current draw |
wire size | circuit breaker | switch |
current fault detect |
|
|
1 |
A |
5A-1 output |
AFCS
|
4.1
|
20
|
5.0
|
Avionics Master
|
No
|
|
power pin notes: AFCS Mode Controller GMC 507, Pitch & Roll Servos |
|
2 |
A |
10A-1 output |
Landing Lt Left
|
4.3
|
18
|
10.0
|
Land Lt
|
Yes
|
|
power pin notes: AeroLEDs Aerosun VX |
|
3 |
A |
5A-2 output |
Audio Panel
|
0.3
|
20
|
5.0
|
Avionics Master
|
No
|
|
|
4 |
A |
5A-3 output |
EIS
|
0.4
|
20
|
5.0
|
always on
|
Yes
|
|
power pin notes: Engine Indication System (EIS) |
|
5 |
A |
5A-4 output |
G3X (PFD)
|
2.0
|
20
|
5.0
|
Avionics Master
|
No
|
|
|
6 |
B |
5A-5 output |
Taxi Lights
|
3.4
|
18
|
5.0
|
Taxi Lt
|
Yes
|
|
power pin notes: AeroLEDs Aerosun VX |
|
7 |
B |
5A-6 output |
AP Yaw Servo
|
2.8
|
20
|
3.0
|
Avionics Master
|
No
|
|
|
8 |
B |
5A-7 output |
Transponder/ADSB
|
1.3
|
20
|
3.0
|
Avionics Master
|
Yes
|
|
J10 |
| pin |
bank |
VP-X pin name |
power pin name | current draw |
wire size | circuit breaker | switch |
current fault detect |
|
|
1 |
A|B |
Starter Switch |
|
|
|
|
|
|
|
|
2 |
B |
5A-8 output |
G5 (BU EFIS)
|
0.8
|
20
|
5.0
|
Avionics Master
|
Yes
|
|
power pin notes: Backup EFIS & ADAHRS |
|
3 |
B |
10A-2 output |
Comm#2
|
0.6
|
18
|
8.0
|
Avionics Master
|
Yes
|
|
power pin notes: Comm #2 - 7.5 Max, .6 receiving... 3.0 transmitting |
|
4 |
B |
5A-9 output |
Alt - BU - Field
|
2.5
|
20
|
5.0
|
BU Alternator
|
No
|
|
|
5 |
B |
10A-3 output |
BoostPump
|
4.5
|
14
|
10.0
|
Boost Pump
|
No
|
|
power pin notes: Airflow Performance Pump |
|
6 |
B |
15A-1 output |
Strobes
|
6.0
|
18
|
10.0
|
Strobe Lt
|
No
|
|
power pin notes: AeroLEDs Pulsar NS/Suntail |
|
7 |
B |
5A-10 output |
Magnetometer
|
0.5
|
20
|
1.0
|
always on
|
No
|
|
|
8 |
B |
5A-11 output |
Nav Lights
|
1.5
|
20
|
2.0
|
Nav Lt
|
Yes
|
|
power pin notes: AeroLEDs Pulsar NS/Suntail |
|
9 |
|
To GND block |
|
|
|
|
|
|
|
|
10 |
B |
5A-12 output |
Alt - BU - Vsense
|
0.1
|
20
|
2.0
|
always off
|
No
|
|
J12 |
| pin |
bank |
VP-X pin name |
power pin name | current draw |
wire size | circuit breaker | switch |
current fault detect |
|
|
1 |
A |
10A-4 output |
GTN 650 Nav
|
2.2
|
18
|
10.0
|
Avionics Master
|
Yes
|
|
|
2 |
A |
15A-2 output |
Pitot/AOA
|
0.5
|
14
|
15.0
|
Pitot Heat
|
Yes
|
|
power pin notes: Heated Pitot/AOA (4 - 12 amps) |
|
3 |
A |
10A-5 output |
GTN 650 Comm
|
0.5
|
18
|
8.0
|
Avionics Master
|
Yes
|
|
|
4 |
|
To GND block |
|
|
|
|
|
|
|
|
5 |
B |
Flap motor |
enabled
|
|
|
5
|
|
|
|
|
6 |
B |
Flap motor |
enabled
|
|
|
|
|
|
|
|
7 |
A |
10A-6 output |
Landing Lt Right
|
4.3
|
18
|
10.0
|
Land Lt
|
Yes
|
|
power pin notes: AeroLEDs Aerosun VX |
|
8 |
A |
5A-13 output |
AccBlock12
|
3.0
|
18
|
5.0
|
always on
|
No
|
|
power pin notes: Cowl Flaps, Ram Air, Oil Damper, Stall Warning, Switch Lights, Overhead Lights, Lemo, CO2 Monitor |
|
9 |
A |
EFIS power output |
G3X (MFD)
|
2.0
|
20
|
5.0
|
always on
|
No
|
|
|
10 |
A |
3A-1 output |
ARINC 429
|
0.2
|
20
|
2.0
|
Avionics Master
|
Yes
|
|
power pin notes: ARINC 429 Interface |
|
11 |
A |
Alternator Field |
Alternator Field
|
2.5
|
20
|
5.0
|
Alternator
|
|
|
|
12 |
A |
15A-3 output |
Backup Battery
|
4.0
|
18
|
10.0
|
always on
|
No
|
|
power pin notes: Pass-through power to two Dual USB chargers. |
J1 |
| pin |
bank |
VP-X pin name |
power pin name | current draw |
wire size | circuit breaker | switch |
current fault detect |
|
|
1 |
A |
2A-1 output |
ADAHRS
|
0.2
|
20
|
2.0
|
always on
|
Yes
|
|
power pin notes: Primary ADAHRS |
|
2 |
A |
2A-2 output |
Alternator Vsense
|
0.1
|
20
|
2.0
|
always on
|
No
|
|
|
3 |
|
Roll Trim: +2.5v |
enabled
|
|
|
|
|
|
|
|
4 |
|
Roll Trim: gnd |
enabled
|
|
|
|
|
|
|
|
5 |
|
Roll Trim: pos input |
enabled
|
|
|
|
|
|
|
|
6 |
A |
Roll Trim: motor power |
enabled
|
|
|
|
|
|
|
|
7 |
A |
Roll Trim: motor power |
enabled
|
|
|
|
|
|
|
|
8 |
|
Pitch Trim: +2.5v |
enabled
|
|
|
|
|
|
|
|
9 |
|
Pitch Trim: gnd |
enabled
|
|
|
|
|
|
|
|
10 |
|
Pitch Trim: pos input |
enabled
|
|
|
|
|
|
|
|
11 |
A/B |
Pitch Trim: motor pwr |
enabled
|
|
|
|
|
|
|
|
12 |
A/B |
Pitch Trim: motor pwr |
enabled
|
|
|
|
|
|
|
|
17 |
|
Flap pos input |
enabled
|
|
|
|
|
|
|
|
18 |
|
Flap pos gnd |
enabled
|
|
|
|
|
|
|
|
19 |
|
Flap pos +2.5v |
enabled
|
|
|
|
|
|
|
|
20 |
|
Serial TX |
|
|
|
|
|
|
|
|
21 |
|
Serial GND |
|
|
|
|
|
|
|
|
22 |
|
Serial RX |
|
|
|
|
|
|
|
J2 |
| pin |
bank |
VP-X pin name |
power pin name | current draw |
wire size | circuit breaker | switch |
current fault detect |
|
|
1 |
|
External Switch Input 1 |
Alternator
|
|
|
|
|
|
|
|
2 |
|
External Switch Input 2 |
BU Alternator
|
|
|
|
|
|
|
|
3 |
|
External Switch Input 3 |
Avionics Master
|
|
|
|
|
|
|
|
4 |
|
External Switch Input 4 |
Boost Pump
|
|
|
|
|
|
|
|
5 |
|
External Switch Input 5 |
Land Lt
|
|
|
|
|
|
|
|
6 |
|
External Switch Input 6 |
Taxi Lt
|
|
|
|
|
|
|
|
7 |
|
External Switch Input 7 |
Nav Lt
|
|
|
|
|
|
|
|
8 |
|
External Switch Input 8 |
Strobe Lt
|
|
|
|
|
|
|
|
9 |
|
External Switch Input 9 |
Pitot Heat
|
|
|
|
|
|
|
|
10 |
|
External Switch Input 10 |
|
|
|
|
|
|
|
|
11 |
|
Starter annunciator input |
enabled
|
|
|
|
|
|
|
|
12 |
|
Aux battery voltage input |
enabled
|
|
|
|
|
|
|
|
14 |
|
Flap Up switch input |
enabled
|
|
|
|
|
|
|
|
15 |
|
Flap Down switch input |
enabled
|
|
|
|
|
|
|
|
16 |
|
Roll Left switch input |
enabled
|
|
|
|
|
|
|
|
17 |
|
Roll Right switch input |
enabled
|
|
|
|
|
|
|
|
18 |
|
Pitch Up switch Input |
enabled
|
|
|
|
|
|
|
|
19 |
|
Pitch Dn switch Input |
enabled
|
|
|
|
|
|
|
The following device pins also have backup circuits (not show in above diagram):
pin name | backup method | circuit breaker |
ADAHRS |
Method C |
2.0A |
G3X (PFD) |
Method C |
5.0A |
G3X (MFD) |
Method C |
5.0A |
EIS |
Method C |
5.0A |
Each column is explained below:
- Pin: the actual pin number on the connector.
- Bank: The VP-X Pro has two independent systems in one box. Each system is referred to as a "bank" of circuits. This column shows which bank that specific power pin is on. See Installation manual for details on determining which device goes on which bank.
- VP-X Pin Name: Describes the function of that pin. 5A-1 for example is a 5 amp circuit and it is the first five amp circuit. 10A-3 is a 10 amp circuit and is the third 10 amp circuit.
- Power pin name: You can give each pin a name that shows on the EFIS display.
- Current draw: The actual current drawn by a device. It is recommended you measure the ACTUAL current draw of each device prior to installation in the aircraft using an ammeter (commonly available from a friend at no cost or from Radio Shack, Sears, and electronic supply stores for a reasonable one).
- Wire size: the wire size you have specified to go between the VP-X and the device being powered.
- Circuit Breaker: The maximum current allowed for that pin. You can enter any value between 1 and the limit of that pin in increments of 1A. This value is equivalent to a circuit breaker or fuse. If a load draws more than the Circuit Breaker value, that circuit will fault. If too large of a breaker value is used, then the wire may overheat or fail. If too small a value is used, then the device may fault the circuit because it draws too much current.
- Switch: The number of the switch input (switch input 1 through 10) you have specified to control this pin. Or it can be set to 'always on' or 'always off'. Each switch input is labeled 1 through 10. You can assign multiple devices to a single switch, and conversely, a switch can control multiple devices. If you set the circuit to 'always on', it will be on anytime the VP-X is powered (i.e. the master switch is on). Multiple pins can be assignedto a single switch. You don't have to use all of the switch inputs.
- Current Fault detect: The pin can be configured to detect a "current fault" or open circuit. When a circuit with this feature enabled is turned on and does not draw any current for 3 seconds, the circuit is faulted. You can use this to detect burned out lights, faulty boost pump, failed avionics fan, or inop heated pitot tube for example. The minimum detectable current is about 100ma, so this should be used on devices like lights, strobes and loads that draw at least 100ma of current.
VP-X Switches
The VP-X allows up to 10 switches, configured to operate any number of connected devices. The following names are suggestions, you can
edit this list as required.
The trim and flap switches are wired to their own dedicated pins. The master switch is wired separately from the VP-X and directly to the master contactor. The Starter switch is wired in between the VP-X and the starter contactor.
Do not include trim, flap, master, or starter switches in the items below. Please see the
VP-X Installation Guide for details.
- Your Switches
-
-
1:
Alternator
-
2:
BU Alternator
-
3:
Avionics Master
-
4:
Boost Pump
-
5:
Land Lt
-
6:
Taxi Lt
-
7:
Nav Lt
-
8:
Strobe Lt
-
9:
Pitot Heat
-
10:
Device pins can also be assigned to "always on" or "always off" as required.
AFCS (5.0A CB, 20awg)
Landing Lt Left (10.0A CB, 18awg)
Audio Panel (5.0A CB, 20awg)
EIS (5.0A CB, 20awg)
G3X (PFD) (5.0A CB, 20awg)
Taxi Lights (5.0A CB, 18awg)
AP Yaw Servo (3.0A CB, 20awg)
Transponder/ADSB (3.0A CB, 20awg)
Starter Switch
G5 (BU EFIS) (5.0A CB, 20awg)
Comm#2 (8.0A CB, 18awg)
Alt - BU - Field (5.0A CB, 20awg)
BoostPump (10.0A CB, 14awg)
Strobes (10.0A CB, 18awg)
Magnetometer (1.0A CB, 20awg)
Nav Lights (2.0A CB, 20awg)
To GND block
Alt - BU - Vsense (2.0A CB, 20awg)
GTN 650 Nav (10.0A CB, 18awg)
Pitot/AOA (15.0A CB, 14awg)
GTN 650 Comm (8.0A CB, 18awg)
To GND block
Flap motor
Flap motor
Landing Lt Right (10.0A CB, 18awg)
AccBlock12 (5.0A CB, 18awg)
G3X (MFD) (5.0A CB, 20awg)
ARINC 429 (2.0A CB, 20awg)
Alternator Field (5.0A CB, 20awg)
Backup Battery (10.0A CB, 18awg)
ADAHRS (2.0A CB, 20awg)
Alternator Vsense (2.0A CB, 20awg)
Roll Trim: +2.5v
Roll Trim: gnd
Roll Trim: pos input
Roll Trim: motor power
Roll Trim: motor power
Pitch Trim: +2.5v
Pitch Trim: gnd
Pitch Trim: pos input
Pitch Trim: motor pwr
Pitch Trim: motor pwr
Flap pos input
Flap pos gnd
Flap pos +2.5v
Serial TX
Serial GND
Serial RX
Starter annunciator input
Aux battery voltage input
Flap Up switch input
Flap Down switch input
Roll Left switch input
Roll Right switch input
Pitch Up switch Input
Pitch Dn switch Input
Alternator (switch)
BU Alternator (switch)
Avionics Master (switch)
Boost Pump (switch)
Land Lt (switch)
Taxi Lt (switch)
Nav Lt (switch)
Strobe Lt (switch)
Pitot Heat (switch)
(switch)
The following device pins also have backup circuits (not show in above diagram):
pin name | backup method | circuit breaker |
ADAHRS |
Method C |
2.0A |
G3X (PFD) |
Method C |
5.0A |
G3X (MFD) |
Method C |
5.0A |
EIS |
Method C |
5.0A |
Buying Guide
Some suggestion to help you source your electrical system.
Vertical Power
VP-X Pro
VP-X Pro Wiring Harness
EFIS Manufacturers
Avionics Dealers and Panel Builders
Electrical Supplies
Alternators
Builder Education Resources
Wiring Checklist
Review the following list to be sure you've included everything in your electrical
system planning:
- Alternator field
- Backup alternator field
- Starter
- Pitch trim
- Roll trim
- Yaw trim
- Flaps
- EFIS
- Backup EFIS
- Backup battery for EFIS
- Radios/Nav/GPS
- Audio panel/intercom
- Transponder
- Autopilot
- Avionics fan
- Defrost fan
- CO Detector
- XM Weather receiver
- AOA or stall warning
- Manifold pressure sensor
- Engine monitor
- Cabin lights
- Panel lights
- Seat heaters
- Landing light(s)
- Taxi light(s)
- Strobe lights
- Nav lights
- Fuel boost pump
- Electronic ignition
- Hobbs meter
- Music player, DVD, etc.
- Smoke system
- Power outlets
- Headset power
- Microswitches for doors, canopy, etc.