Astronics Vertical Power Installation And Operating Manual Download Page 3

PPS Installation and Operating Manual

Rev. C.2 (January 19, 2018)

Important Notice

This manual contains important information that may affect the safety of your aircraft. Do 

not fly the aircraft until you fully understand the installation and operating instructions, 

and all of the pre-flight checks have been successfully completed. 

Read the Limited Warranty (document number AD263 Limited Warranty Vertical Power Product 

Line) available at www.verticalpower.com. There is information in the Limited Warranty that 

may alter your decision to install this product. 

If you do not accept the terms of the Limited 

Warranty, do not install this product.

 The product may be returned for a refund if you do not 

accept the terms of the Limited Warranty.

Ballard Technology, Inc. is not liable or responsible for a pilot’s action or any situation that 

results in personal injury, property damage, missed commitments, lack of use of an aircraft 

or any expenses incurred due to: product failure, inaccuracy in displayed data or text files, 

display or display format issues, software bugs or problems, upgrade or customization 

issues, misinterpretation of the display, warning and/or limit settings, calibration problems, 

installation issues (leaks, mis-wiring, obstructions, damage to aircraft or components, incorrect 

installation of any parts, wrong parts, parts that don’t fit, etc.) or any other issues related to the 

installation or operation of this product. All of the above are solely the pilot’s and/or installer’s 

responsibility.

The pilot must understand the operation of this product before flying the aircraft.

 The pilot 

will not allow anyone to operate the aircraft that does not know the operation of this product. 

The pilot will keep the PPS Operating Instructions in the aircraft at all times. The ability for this 

product to correctly control electronic components and detect a problem is directly related to the 

pilot’s ability to properly install the system, and the pilot’s interpretation and observation skills.

By installing this product, the aircraft owner/pilot and installer agree to hold Ballard 

Technology, Inc. harmless and in no way responsible for monetary compensation, including 

punitive damages for any incident, harm and/or damage associated with this product (including 

but not limited to the ones listed above). If you do not agree to the above,

 DO NOT INSTALL 

THIS PRODUCT.

 The pilot, aircraft owner and/or installer may want to obtain an appropriate 

insurance policy before installing this product. If you do not have the skills, knowledge, tools, 

equipment or facility, to perform and determine the installation of this 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 take 

the responsibility for the installation and operation of this product, 

DO NOT INSTALL THIS 

PRODUCT

. This product may be returned for a refund by contacting Ballard Technology, Inc.

It is possible for any system to fail thereby disabling electronic components or displaying 

inaccurate high, low or jumpy readings. Therefore, you must be able to recognize a system 

failure and you must be proficient in operating your aircraft safely in spite of a system failure. 

IT IS THE BUILDER AND/OR PILOT’S RESPONSIBILITY TO DETERMINE THE 

APPROPRIATE LEVEL OF BACKUP AND REDUNDANT SYSTEMS NEEDED FOR 

SAFE OPERATION OF THE AIRCRAFT.

 If you do not have this knowledge or skill, contact 

the FAA, a certified aircraft mechanic, or a local flight instructor for training prior to building or 

flying the aircraft with this system.

Before flying the aircraft verify the instrument markings displayed on the system are accurate 

with your POH for every function displayed. Verify that each electrical device is configured 

correctly and behaves appropriately. All data must be verified by the pilot before it is used.

Before starting the installation, make sure that your planned installation will not interfere 

with the proper operation of any controls. The installer should use current aircraft standards 

and practices to install this product. Refer to AC 43.13-2A, Acceptable Methods, Techniques, 

and Practices - Aircraft Alterations and AC 43.13-1B, Acceptable Methods, Techniques, and 

Practices—Aircraft Inspection and Repair.

The PPS is an experimental system limited to use in experimental aircraft or Light Sport 

Aircraft. PPS products are not approved for use in aircraft with FAA or foreign type certificates.

Limited Warranty

For Warranty information, please refer to document number AD263 Limited Warranty Vertical 

Power Product Line available at www.verticalpower.com/documents

.

Copyright Notice

Copyright ©2018 by Ballard Technology, Inc. Ballard Technology’s permission to copy and 

distribute this manual is for the purchaser’s private use only and is conditioned upon purchaser’s 

use and application with the hardware that was shipped with this manual. No commercial resale 

or outside distribution rights are allowed by this notice. This material remains the property of 

Ballard Technology. All other rights reserved by Ballard Technology, Inc.

Trademarks

Vertical Power is a registered trademark of Ballard Technology, Inc. All other product names or 

trademarks are property of their respective owners.

Astronics Ballard Technology

11400 Airport Road

Everett, WA 98204

Phone: 425.328.1658

Fax: 425.339.0915

Email: [email protected]

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...

Reviews: