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REV 2.3 

 

     © 2012 TCW Technologies, LLC. 

6

Technologies, LLC. to simplify this requirement, it has the mating connector  installed 
and performs trickle charging as well as fast charging functions. 
 

Upon completion of installation: 
 

1)  The builder/operator is responsible for determining the minimum operating duration 

of the back-up enabled equipment. 

 
2)  The required back-up operating time for the connected equipment should be 

recorded in the aircraft log-book with follow-up entries confirming the annual testing 
results that indicate that the required operating time is satisfied. 

 
 
 
Normal Product Operation: 
 

For normal operation the following is the recommend operating procedure, it is strongly 
recommended that this operating procedure be added to the aircraft operating check-list 
for standard 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 the connected equipment successfully boots-up and is operating properly. 

(During this period of time the equipment is running off of the back-up battery in the 
IBBS product.  This test ensures the transfer circuit and back-up battery are properly 
working) 

4)  Turn on the Aircraft Master Switch, ensure the connected equipment remains 

energized. 

5)  Start and operate the aircraft according to normal operating procedures. 

 
 
 
 

Shut-down Procedure: 
 

1)  Shut down aircraft engine using normal procedures. 
2)  Shut down the Aircraft Master Switch 
3)  Verify that equipment that derives back-up power from the IBBS product remains ON 
4)  Turn-off Back-up Power Master switch, ensure that connected equipment powers 

down. 
(This procedure further ensures the operation of the transfer circuit in the IBBS 
product.) 
 

 

 

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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