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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 nameactual current drawcircuit breaker valuemin wire size VP-X pinbackup?current fault detect?switchbank preference
Transponder/ADSB 1.3A 3.0A20g J8-8 none Yes Avionics Master Bank A or B
GMA 245
Audio Panel 0.3A 5.0A20g J8-3 none No Avionics Master Bank A or B
G5 w/Battery
G5 (BU EFIS) 0.8A 5.0A20g J10-2 none Yes Avionics Master Bank B
notes: Backup EFIS & ADAHRS
GMU 11
Magnetometer 0.5A 1.0A20g J10-7 none No always on Bank A or B
GTN 650
GTN 650 Nav 2.2A 10.0A18g J12-1 none Yes Avionics Master Bank A
GTN 650 Comm 0.5A 8.0A18g J12-3 none Yes Avionics Master Bank A
Autopilot
AFCS 4.1A 5.0A20g J8-1 none No Avionics Master Bank A or B
notes: AFCS Mode Controller GMC 507, Pitch & Roll Servos
GEA 24
EIS 0.4A 5.0A20g J8-4 Method C Yes always on Bank A or B
notes: Engine Indication System (EIS)
Accessory Block
AccBlock12 3.0A 5.0A18g 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 2.0A20g J12-10 none Yes Avionics Master Bank A or B
notes: ARINC 429 Interface
GSU 25
ADAHRS 0.2A 2.0A20g J1-1 Method C Yes always on Bank A
notes: Primary ADAHRS
GTR 20
Comm#2 0.6A 8.0A18g 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 5.0A20g J8-5 Method C No Avionics Master Bank A
G3X GDU 460
G3X (MFD) 2.0A 5.0A20g J12-9 Method C No always on Bank A
GAP 26 (-20)
Pitot/AOA 0.5A 15.0A14g J12-2 none Yes Pitot Heat Bank A or B
notes: Heated Pitot/AOA (4 - 12 amps)

Lights
Strobes
pin nameactual current drawcircuit breaker valuemin wire size VP-X pinbackup?current fault detect?switchbank preference
Strobes 6.0A 10.0A18g J10-6 none No Strobe Lt Bank A or B
notes: AeroLEDs Pulsar NS/Suntail
Nav Lights (LED)
Nav Lights 1.5A 2.0A20g J10-8 none Yes Nav Lt Bank A or B
notes: AeroLEDs Pulsar NS/Suntail
Landing Lt Left
Landing Lt Left 4.3A 10.0A18g J8-2 none Yes Land Lt Bank A
notes: AeroLEDs Aerosun VX
Taxi Light (LED)
Taxi Lights 3.4A 5.0A18g J8-6 none Yes Taxi Lt Bank B
notes: AeroLEDs Aerosun VX
Landing Lt Right
Landing Lt Right 4.3A 10.0A18g J12-7 none Yes Land Lt Bank A
notes: AeroLEDs Aerosun VX

Accessories/Ignition/Other
Boost Pump (inj)
pin nameactual current drawcircuit breaker valuemin wire size VP-X pinbackup?current fault detect?switchbank preference
BoostPump 4.5A 10.0A14g J10-5 none No Boost Pump Bank A or B
notes: Airflow Performance Pump
Garmin GSA 28
AP Yaw Servo 2.8A 3.0A20g J8-7 none No Avionics Master Bank A or B
TCW 6ah IBBS
Backup Battery 4.0A 10.0A18g 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 nameactual current drawcircuit breaker valuemin wire size VP-X pinbackup?current fault detect?switchbank preference
Alternator Field 2.5A 5.0A20g J12-11 none No Alternator Bank A
Alternator Vsense 0.1A 2.0A20g J1-2 none No always on Bank A
SD-20 BU Alt
Alt - BU - Field 2.5A 5.0A20g J10-4 none No BU Alternator Bank B
Alt - BU - Vsense 0.1A 2.0A20g 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 namecurrent draw wire sizecircuit breakerswitch 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 namecurrent draw wire sizecircuit breakerswitch 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 namecurrent draw wire sizecircuit breakerswitch 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 namecurrent draw wire sizecircuit breakerswitch 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 namecurrent draw wire sizecircuit breakerswitch 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 namebackup methodcircuit 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
<-- Edit here
  • 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.

VP-X System Settings

VP-X Pro. 32 circuits, 14v or 28v, aux battery monitoring, DualBuss™ technology.

System Voltage: 14

Both systems support primary and backup alternators, two-axis trim controller, and flap controller. More information is available in the VP-X Product Description

Options

Primary Alternator
Externally regulated (B&C or similar)
Backup Alternator
Externally regulated (B&C SD-20)
Note: For 28v systems using SD-20, user must install a B&C LS-1A

More information on alternators and the options below is available in the VP-X Installation Guide

Ignition (left side)
Magneto
Ignition (right side)
Magneto

Are you installing electric flaps?
Flap circuit breaker: 5 amps
Are you installing electric roll trim?
Are you installing electric pitch trim?
Do you want to measure voltage on a second or aux battery? (VP-X Pro only, see installation guide for details)
Do you want to use the starter annunciator feature?

 

Electrical Diagram

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 namebackup methodcircuit 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:



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