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REV 2.3 

 

     © 2012 TCW Technologies, LLC. 

2

Installation Instructions: 
 
 

1.  IMPORTANT NOTE: 

Consult the attached wiring diagrams to identify wiring connections for your 
particular installation.   The IBBS system may be fed from a bus that remains active 
during engine starting, such as the master bus or it may be fed from an avionics 
bus that is switched off during engine starting.     If you want your avionics to be up 
and running during engine cranking, ensure input power is derived from the master 
bus.     
 
 

2.  The IBBS-12v-2ah was designed to drive one piece of equipment, such as an EFIS, 

Autopilot or an electronics ignition module.   The output current limit for this model is 
3 amps maximum continuous current.   If more load current is required use model 
IBBS-12v-4ah.   Consult the install manual for detailed specifications. 
 

3.  Mount the IBBS in a suitable location in the aircraft.  Ensure the mounting points and 

fasteners are suitable for the weight of the product, consult the specifications for 
details. The IBBS must be mounted inside the aircraft, do not mount the IBBS in the 
firewall forward area.  Avoid mounting the IBBS unit up under the instrument panel 
where significant heat may be trapped.  Select an area that is accessible to allow for 
future battery servicing.  The operating temperature range of the system is -10 C° to 
60 C° and the effective charging temperature range is 0 C° to 40 C°.  Select an 
installation location that will comply with these requirements. 

 
4.  Connect the aircraft wiring according to one of the wiring diagrams shown. 

The IBBS must be powered through a properly sized circuit breaker or fuse.  
ENSURE the proper size wire is utilized for the input feed, output supply and ground 
connection.  The IBBS has two power inputs, pin1 provides main recharge current 
and main bus sensing, pin 6 provides pass through power from the main bus to the 
connected load during normal operation.  Connect the two input wires together at the 
fuse or circuit breaker as shown in the diagrams.  The IBBS-12v-2ah has three 
output pins, pin 7,8,9, that provide power to the connected load.   These three wires 
may be paralleled together for added redundancy.   The output wires of the IBBS 
system are internally protected with a single 8 amp, 5 x 20 mm fuse.   No additional 
external fusing is required; however, use at least 20 awg wire for the output wires.   
 

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 utilizing ASF EFIS systems and 
following the specific wiring diagram for this application.  This 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.  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    

Summary of Contents for IBBS-12v-2ah

Page 1: ...output power during normal and emergency operations The IBBS system also provides an output signal to communicate the operating state of the back up bus as well as the state of the battery The IBBS sy...

Page 2: ...lect an installation location that will comply with these requirements 4 Connect the aircraft wiring according to one of the wiring diagrams shown The IBBS must be powered through a properly sized cir...

Page 3: ...tem connections directly to aircraft battery must be utilized as shown 8 When using the IBBS product to provide back up power to an electronic ignition system CDI pullable circuit breakers must be use...

Page 4: ...on the input of the IBBS the info line may be read to determine the internal battery voltage A nominal battery with a full charge will read between 12 and 15 volts When the IBBS is on line providing b...

Page 5: ...harged battery the following average performance can be expected in terms of operating duration The operating duration is for output voltage down to 9 5 volts Nominal Current Draw Duration total conne...

Page 6: ...procedures Start up Procedure 1 Prior to turning on the Aircraft Master Switch turn ON the Back up Power master switch 2 Turn on any equipment that derives back up power from the IBBS product 3 Ensure...

Page 7: ...he Back up Power Master Switch 3 Turn on all equipment connected to and supplied with back up power from the IBBS product 4 Measure and record at least the following information The time until the fir...

Page 8: ...operation based on the use of only the electronic 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...

Page 9: ...ullable breakers to the normal ON position and ensure aircraft engine is properly returned to the off position by following normal run and shut down procedures 10 After completing these tests recharge...

Page 10: ...l high performance fast charger Surge Protection 16 volt active clamp 1500w 10 1000uS waveform Wiring CPC connector with Mil spec machined contacts Field replaceable inline fuse AGC 7 5 Enclosure Cast...

Page 11: ...rness PIN Description Wire Color optional harness 1 Main Aircraft Bus charge power Red 2 Aux Battery trickle charge Always ON Purple yellow 3 Aircraft ground Black 4 Back up power master switch White...

Page 12: ...g 20 awg www tcwtech com Emmaus PA USA MODEL IBBS 12V 2AH Input 10 15 volts DC Output 12 volts 3 amps Capacity 2 amp hours INTEGRATED Back up Battery SYSTEM Pin 1 Main Aircraft Bus Pin 2 Aux Battery t...

Page 13: ...hout back up power inputs Equipment without Back up Power Input 2 amps 10 amp Main Aircraft Bus Aux Battery trickle charge Back up Power Master cpc connector INFO Low active signal High battery voltag...

Page 14: ...x Battery trickle charge Back up Power Master cpc connector INFO Low active signal High battery voltage Back up power input 20 awg 22 awg 22 awg 20 awg 20 awg 22 awg 20 awg www tcwtech com Emmaus PA U...

Page 15: ...REV 2 3 2012 TCW Technologies LLC 15 Main Aircraft Bus 20 awg Shielded...

Page 16: ...REV 2 3 2012 TCW Technologies LLC 16...

Page 17: ...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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