Astronics Vertical Power Installation And Operating Manual Download Page 21

Page 17 

PPS Installation and Operating Manual

Rev. C.2 (January 19, 2018)

4.3c Ground Test with engine running

This section verifies the proper operation of the PPS with the engine 

running. If this is coincident with first engine start, be sure to integrate 

the kit manufacturer’s first engine start safety procedures with the test 

plan below. You may consider first verifying proper operation of the 

engine and once that is complete, begin the electrical system test.
Prolonged low-power operation of a new engine may adversely affect the 

engine. Be sure you understand the engine break-in requirements, and 

balance those against the time needed to test the electrical system.
The following tests should be used as a guideline. Follow the engine 

manufacturer’s starting and safety procedures.

• 

Ensure that the battery is fully charged. If the voltage drops 

rapidly during engine start, then the battery is bad or not fully 

charged.

• 

Start the engine.

• 

Note the bus voltage. Then turn on the primary alternator. If 

installed turn on the alternator enable to the PPS.

• 

The voltage should increase to 14.2 volts +/- 0.3 volts (check 

with your alternator manufacturer for specifics)

• 

If installed, verify the alternator current output.

• 

If installed, verify the main bus current output. Current should 

show charging or zero current flow once alternator is operating.

• 

Verify the each alternator can be turned off and on.

• 

If installed, turn on the alternator enable to the PPS on and off. 

Verify correct operation.

• 

If installed, turn the main battery enable to the PPS on and off. 

Verify correct operation.

• 

Turn off all switches.

4.4 Flight Test

Prior to flight, make sure you understand how to operate the PPS and 

clear faults. This section provides a series of recommended steps which 

should be incorporated into the overall flight test plan as you deem 

appropriate. Review the ground test steps, as complete and thorough 

ground testing will mitigate the risk of trouble while airborne.

Do not fly the aircraft until you are comfortable everything 

operates correctly on the ground and you are knowledge-

able about the systems and their proper operation.

It is the pilot’s responsibility to develop a test plan that ensures a safe and 

productive first flight. Typically, the first flight is focused on verifying 

basic flight characteristics and proper engine operation. With that in 

mind, we recommend deferring complete electrical system tests until 

after you are comfortable that the engine and airframe are performing as 

expected, and you are comfortable flying the aircraft.
If you are installing the system as a retrofit, it is still important to 

complete as much of the testing on the ground as possible.
Once airborne, keep an eye out for traffic and obstacles during the test 

procedure. Carry a handheld radio as a backup in case of electrical 

system failure. If you encounter any difficulties in flight due to improper 

setup or unknown electrical system behavior, land as soon as practical or 

simply turn off the master switch. 

Verify backup power is ON for ignition and required 

devices prior to turning off the master switch.

If you have completed a thorough check out on the ground, the chances 

of problems while airborne are greatly reduced.
Verify each of the following in flight:

• 

Verify the each alternator can be turned off and on.

• 

If installed, turn on the alternator enable to the PPS on and off. 

Verify correct operation.

• 

If installed, turn the main battery enable to the PPS on and off. 

Verify correct operation.

Summary of Contents for Vertical Power

Page 1: ...20180119 Rev C 2 Copyright 2018 by Ballard Technology Inc Primary Power System PPS Primary power control for experimental and light sport aircraft Installation and Operating Manual January 19 2018 Re...

Page 2: ...ts 6 3 3 Alternator Options 6 3 4 Wire Sizes and Circuit Protection 7 3 5 Grounding IMPORTANT 7 3 6 Switch Nomenclature 8 3 7 Current Sensing Shunt 8 4 Installation and Test 4 1 Planning 9 4 1a Tools...

Page 3: ...product is safe reliable and accurate and to determine this product is operating properly after installation DO NOT INSTALL THIS PRODUCT If the aircraft owner pilot and or installer are unwilling to t...

Page 4: ...29 2017 Updates based on product changes incl new pinouts Aug 24 2017 Updated grounding instructions Sep 25 2017 Updated grounding diagram and Table 4 2b Jan 19 2018 Updated current values added Start...

Page 5: ...ndependent batteries alternators battery contactors and a cross tie contactor Multiple PPS units can be used to implement a dual bus architecture Please contact support for more information on dual bu...

Page 6: ...maintain it but contributions come from builders Top 10 Wiring Mistakes A free 12 page paper describing the most common wiring mistakes and how to get started wiring your aircraft Additional document...

Page 7: ...or will latch open if the slow trip current the fast trip current of 1200 amps or the instantaneous maximum current of 1500 amps is exceeded The slow trip current emulates the trip curve for a standar...

Page 8: ...nt fault indication BUS GND ALT DIST FAULT Latched Over current fault indication BUS GND STARTER ACTIVE Starter Active indication BUS GND BATT CURRENT Main Battery current sense 1 mV A relative to 7 5...

Page 9: ...imilar and not because you blindly copied him We believe the most important free advice we can offer is the following CLARIFY YOUR MISSION In this age of gadgets it is all too tempting to add just one...

Page 10: ...lit and sent to individual devices through circuit protection devices fuses and circuit breakers and switches The VP X assumes the role of busses circuit protection and a host of single function modul...

Page 11: ...g IMPORTANT Many people think that the power or positive wire is the most important wire to provide electricity to a device The electrical ground is just as important as electricity must flow the enti...

Page 12: ...drawing more current than the alternator can provide note engine must be running If you set your low voltage alarm on the EFIS at 13 volts then you will get a low voltage alarm if the alternator fail...

Page 13: ...with planning Some items may vary depending on the requirements of your specific installation Crimper insulated terminals 20 AWG Crimper TE Connectivity Hand Crimper 601966 1 or equivalent and TE Conn...

Page 14: ...ay not be needed depending on alternator PPS Wiring Overview with the Vertical Power VP X Aircraft with a remote mounted battery may require the addition of a battery contactor near the battery as sho...

Page 15: ...e connected Maximum wire length 24 in Twist together sense lines on pins 9 and 20 to reduce common mode noise Twist together sense lines on pins 19 and 18 to reduce common mode noise PPS basic install...

Page 16: ...basic installation with the Vertical Power VP X Comprehensive Installation with the Vertical Power VP X The image below details comprehensive PPS connector wiring for an aircraft wired with the Verti...

Page 17: ...airframe 4 2a Mount the PPS The PPS should be mounted to the firewall or other desired location using 4 10 bolts not included A drill punch template is provided on the next page You can print this as...

Page 18: ...Page 14 PPS Installation and Operating Manual Rev C 2 January 19 2018 PPS Mounting Template...

Page 19: ...tor battery starter and grounds 4 2c Control Status Wiring Per your installation plan route wires for the switches and indicators Crimp and install these wires into the circular connector The PPS uses...

Page 20: ...d must connect both pins 26 and 27 to GND maximum wire length 24 inches 26 27 RSVD Reserved do not connect 28 4 3 Ground Test The ground test steps are performed in two parts the first part without th...

Page 21: ...nderstand how to operate the PPS and clear faults This section provides a series of recommended steps which should be incorporated into the overall flight test plan as you deem appropriate Review the...

Page 22: ...put terminal Use multi meter to verify that Master switch input primary or alternate voltage is ground must be below minimum input voltage Use multi meter to verify that Main contactor switch input vo...

Page 23: ...aximum intermittent Alternator Input 80 A maximum continuous Analog Current Monitor Outputs Common mode reference of 7 5 VDC Scale 1 mV Amp Short circuit protected 7 3 Environmental Physical Component...

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