TCW Technologies IBBS-12v-3ah-CRT-V Manual Download Page 8

                       p/n 725.0002  REV 3.0 

 

© 2023 TCW Technologies, LLC. 

is available a peak charging voltage of 14-15 volts will be observed as the battery reaches full 
capacity.    
 
Alternately, a ground based charger is available from TCW Technologies LLC., model # IBBS-12v-
CHARGER-LI-FE. This charger may be used for recharging the IBBS unit as well as keeping it fully 
charged during long term product storage.  (9 months or longer) 
 
 

Battery Capacity:

 

The IBBS provides an energy capacity of 3 amp-hours at 12.8 volts when the system is fully 
charged and operated at 25 C°.   Depending on various conditions including operating and storage 
temperature and age of the battery pack, the capacity of the system will vary. With a fully charged 
battery, the following average performance can be expected in terms of operating duration.  The 
operating duration is for an output voltage down to 9.0 volts. (end point voltage).  The battery is 
also rated for at least 500 shallow discharge cycles,  this is defined as a 10 minute discharge 
operation at 3 amps followed by 30 minutes of recharge time.  

 
Nominal Current Draw                 

Duration  

 

Effective Nominal Capacity 

Total connected load all outputs 
 
1.5  amps  

 

 

 

120 minutes   

 

3 amp-hrs 

 

3.0 amps   

 

 

 

60 minutes   

 

3 amp hrs. 

5.0 amps   

 

 

 

30 minutes   

 

2.5 amp-hrs 

 
Capacity at Low Temperatures:    
 
-18 C°      75% of effective nominal capacity 
-30 C°   70% of effective nominal capacity  
-45 C° 

45% of effective nominal capacity 

 

 

Servicing: 

The internal battery in the IBBS system is replaceable; however, the IBBS product must be 
returned to TCW Technologies, LLC. for this service.  The unit must be replaced with the same 
Part Number unit or later FAA approved revision.  Battery life depends strongly on many factors 
including operating and storage temperature, number of discharge cycles and depth of discharge.  
The battery capacity should be checked at least annually for suitable back-up power operation 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. regarding battery replacement. 

 

Storage beyond 9 months: 

If the IBBS unit is to be stored without connection to the aircraft for a period greater than 9 months, 
it must be connected to a source of DC power to maintain the batt

ery’s charge.   Only conne

ctions 

to the ground terminal and the main power terminal are required.   Connect Pin 5 (main power) and 
Pin 9 (ground) of the IBBS to any source of regulated DC power at 14-15 volts with a current 
capability of at least 1.8 amps to accomplish full recharging.  Ensure the IBBS unit is in an ambient 
temp of 0-40 C° for ground-based charging.   Charger model IBBS-12v-CHARGER-Li-Fe is 
available from TCW Technologies, LLC. to simplify this activity. 

 
 
 
 
 

Summary of Contents for IBBS-12v-3ah-CRT-V

Page 1: ...by integrating all of the key elements in a single enclosure The IBBS system provides back up power to critical electronic loads such as EFIS GPS Autopilots Radios Electronic Ignition systems and engi...

Page 2: ...lots JPI and EI engine monitors SureFly electronic ignitions Lycoming EIS electronic ignitions and ElectroAir electronic ignitions IBBS must be installed using the current aircraft standards and pract...

Page 3: ...mance Specifications and potential limitations and ratings under various conditions including environmental and application installations See Item 3 below for installation location limitations Install...

Page 4: ...rt The vent port must be routed to the bottom or side exterior of the aircraft via the vent hose Locate a suitable flat location measuring at least 3 3 x 12 in area or in an existing avionics rack for...

Page 5: ...atically transfers the load current on the output pins to the internal back up battery source Pin 5 nominal current draw is 3 3 amps during charging Pin 4 provides power to an internal battery heater...

Page 6: ...ve an input impedance 100k ohms otherwise it will load down pin 2 and provide an artificially low voltage reading When used with the following EFIS systems wire pin 2 to the Volts2 input of the EFIS o...

Page 7: ...Power Master Switch The IBBS has one input switch connection as identified in the wiring diagrams Back up Power Master This switch enables back up power from the IBBS system to be available on the ou...

Page 8: ...Low Temperatures 18 C 75 of effective nominal capacity 30 C 70 of effective nominal capacity 45 C 45 of effective nominal capacity Servicing The internal battery in the IBBS system is replaceable howe...

Page 9: ...test ensures the transfer circuit and back up battery are properly working 4 Verify the low voltage warning light is indicating a low voltage condition 5 Turn on the Aircraft Master Switch ensure the...

Page 10: ...p n 725 0002 REV 3 0 2023 TCW Technologies LLC 10 3 Land aircraft as soon as practical to resolve the loss of main electrical power...

Page 11: ...nstallation approval The internal battery is not field replaceable The IBBS unit must be returned to TCW Technologies LLC for all repair and servicing requirements Endurance testing 1 Turn off the Air...

Page 12: ...FAA approved revision The use of alternate models will require a new FAA installation approval The internal battery is not field replaceable The IBBS unit must be returned to TCW Technologies LLC for...

Page 13: ...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 the IBBS product by operating the system n...

Page 14: ...d transient load 30 second duration max Battery Internal sealed Li Fe PO4 nominal 12 8 volts Charger Integral high performance fast charger with cell balancing and thermal monitoring Surge Protection...

Page 15: ...erational Performance Standards for Rechargeable Lithium Battery Systems Environmental Qualification RTCA DO 160 g B2BBBSC1EYXXFSZB IX XXXXAZ ZC TT MA3H3L3XXAX Power input 14 volts nominal 1 8 amps ch...

Page 16: ...0 temp variation 5 Category B Humidity 6 Category B operational shock 7 Category B vibration 8 Category S curve C explosion 9 Category E waterproofness 10 Category Y fluid susceptibility 11 Category x...

Page 17: ...ss View from back of aircraft wiring harness connector 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 sw...

Page 18: ...p n 725 0002 REV 3 0 2023 TCW Technologies LLC 18 IBBS unit mounting footprint 11 16in 2 00in Mounting holes 0 188 4 plcs All dimensions in inches IBBS unit height 3 2 C G at center of all axis...

Page 19: ...aus PA USA IBBS 12V 3AH CRT V Input 13 16 volts DC Output 12 volts 5amps INTEGRATED Back up Battery SYSTEM Back up power output 20 awg Main Aircraft Bus charge sense pass thru Pin Function 15 pin Male...

Page 20: ...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 NOTE Use redundant gro...

Page 21: ...nfo 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 NOTES 7 11 8 13 14 15 output output output ww...

Page 22: ...designed and manufactured RETURN OR REPLACED COMPONENTS any item to be replaced under this Warranty must be returned to TCW Technologies in Emmaus PA or such place as TCW may designate freight prepaid...

Reviews: