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REV 1.6 

 

     © 2019 TCW Technologies, LLC. 

 
 

Output Power connections

  
The IBBS-12v-6ah has four output pins, Pins 12,13,14,15.  These pins provide power to the 
connected load.   These four wires may be paralleled together for redundancy and load 
current sharing.  Use 20 awg wire for each pin.   Maximum output current of 3.5 amps per 
pin, and 8 amps maximum continuous combined for all four pins.    The output wires of the 
IBBS system are protected with a single 10 amp, mini ATC fuse.   This fuse is accessible on 
the side of the enclosure.   
 

IMPORTANT NOTE ON CHANGING FUSE: 

Disconnect the main product connector before changing the fuse! 

Replace fuse with 10 amp, mini ATC fuse only 

 
 
5. 

The Back-up Power Master switch must be utilized to turn the back-up battery system 

off when not in use, except for installations where the off state current requirement is less 
than 50 micro-amps, such as with the AFS EFIS systems.   Follow the specific wiring 
diagram for this application.  This back-up power master switch gives the pilot the ability to 
turn the back-up battery system off.  In some installations this may be the only means to 
shut down the connected equipment.  
 
6. 

The IBBS unit has a low voltage warning output, pin 3.   This pin may be used to drive 

an LED indicator or to provide a digital signal to indicate the main input bus is in a low 
voltage condition.   When the main input bus (connected to pin 5) falls below about 11 volts 
this output will drive to a low state.   Maximum current sourced on this pin is 25 milliamps. 
 
7. 

 The IBBS unit has in internal battery monitor connection, pin 2.  This pin allows the 

voltage state of the internal battery to be monitored with a separate voltage meter or analog 
input.  This pin will only report internal battery voltage when the unit is enabled by turning 
the Back-up Master switch ON.  A fully charged battery back will indicate about 13-14.7 volts 
on this pin.  

Important note:  the meter utilized to measure pin 2 must have an input 

impedance >100k ohms otherwise it will load down pin 2 and provide an artificially 
low voltage. 

 
8. 

Complete the installation of the wiring harness and connector prior to attaching the 

connector to the IBBS product.  This is essential to ensure the wires do not inadvertently 
short together during installation.  Remember, the IBBS pack is a back-up source of power 
and is ready to deliver output power even when the aircraft electrical system is in the off 
state. 
 
9. 

When using the IBBS product to provide back-up power to an electronic ignition 

system it MUST be used to back-up one and only one electronic ignition module.  Do not 
use one IBBS to back up both electronic ignition modules in a dual electronic ignition 
system.   Follow the wiring diagram for installation with electronic ignition module.  Note, the 
Light Speed Electronic ignition system connects directly to aircraft battery as shown.    Other 
brands of electronic ignition systems connect to the switch side of the aircraft master bus.   
Follow the instructions per the electronic ignition manufacture for your installation. 
 

Summary of Contents for IBBS-12V-AH

Page 1: ...h as EFIS GPS Autopilots and engine monitor systems Integral to the IBBS is a lithium iron phosphate battery pack and a matched charging system to ensure the battery is properly charged and maintained...

Page 2: ...own in AC 43 13 2A 1B The installer builder is solely responsible for determining the suitability of the installation and use of this product IBBS products are protected by US Patent 8 189 305 Table o...

Page 3: ...vicing The operating temperature range of the system is 10 C to 60 C the effective charging temperature range is 0 C to 40 C Select an installation location that will comply with these requirements 4...

Page 4: ...tput will drive to a low state Maximum current sourced on this pin is 25 milliamps 7 The IBBS unit has in internal battery monitor connection pin 2 This pin allows the voltage state of the internal ba...

Page 5: ...ilable on the output wires when power on the normal aircraft bus falls into the range of 10 11 volts If the back up power master switch is enabled and normal aircraft power falls into the range of 10...

Page 6: ...tion of the connected equipment When the battery capacity no longer meets the operating criteria of the aircraft it must be replaced Contact TCW Technologies LLC for battery replacement Storage beyond...

Page 7: ...nsure the connected equipment remains energized If you are utilizing a separate avionics bus this may need to be turned ON to continue the operation equipment connected to the IBBS output 5 Start and...

Page 8: ...the IBBS product 4 Measure and record at least the following information The time until the first piece of connected equipment no longer functions or the time until the output of back up power supply...

Page 9: ...c ignition module provided with back up battery power 3 PULL the 5 amp breaker feeding the Back up Master Switch confirm engine continues to run 4 PULL the 7 5 amp breaker feeding pins 6 7 8 of the IB...

Page 10: ...k up battery may need replacement 9 Return all pullable breakers to the normal ON position and ensure aircraft engine is properly returned to the off position by following normal run and shut down pro...

Page 11: ...and transient load 30 second duration max Battery Internal sealed Li Fe PO4 Charger Integral high performance fast charger Surge Protection 34 volt active clamp 1500w 10 1000uS waveform Wiring 15 pin...

Page 12: ...g harness View from back of connector on harness Pin Function 5 PWR in charge sensing 2 Batt info 3 Low Volt Warn 12 Output 13 Output 14 Output 15 Output 6 Pwr pass thru input 1 Enable backup switch 9...

Page 13: ...REV 1 6 2019 TCW Technologies LLC 13 Product mounting footprint 4 mounting holes 0 190 1 50 7 25 2 290 7 70 Top View 0 225 Product height 2 75...

Page 14: ...wer output 20 awg 10 amp Main Aircraft Bus charge sense pass thru Pin Function 15 pin Male Dsub on unit 12 Output 13 Output 14 Output 15 Output 9 Ground 10 Ground 11 Ground 5 PWR in charge sensing 2 B...

Page 15: ...Aircraft Bus Back up Power Master Battery Info Back up power output 20 awg 22 awg 22 awg 20 awg 20 awg 20 awg 1 6 9 10 2 5 12 main power input 15 pin female Dsub connector 3 Low Voltage Warning LED N...

Page 16: ...20 awg 20 awg 1 6 9 10 2 5 12 Main power input 15 pin female Dsub connector 3 Low Voltage Warning LED NOTES 7 11 10 amp 8 13 14 15 output output output www tcwtech com Emmaus PA USA MODEL IBBS 12V 6A...

Page 17: ...C Output 12 volts 8 amps INTEGRATED Back up Battery SYSTEM 1 Use redundant ground pins 9 10 11 2 See Garmin install manual for all wiring details and fusing requirements Garmin G3x Avionics GDU 46x or...

Page 18: ...g 1 6 9 10 2 5 12 15 pin female Dsub connector NOTES 7 11 10 amp 8 13 14 15 output Output to additional AFS efis www tcwtech com Emmaus PA USA MODEL IBBS 12V 6AH Input 10 15 volts DC Output 12 volts 8...

Page 19: ...onic ignition Back up power master switch Wiring diagram for use with electronic ignition such as LSE Plasma II and III Consult ignition module wiring documents for specific wiring requirements Do Not...

Page 20: ...Emmaus PA or such place as TCW may designate freight prepaid PRODUCT IMPROVEMENTS TCW reserves the right to change or improve its products or any portions thereof without being obligated to provide su...

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