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p/n 725.0001  REV 3.0 

 

     © 2023 TCW Technologies, LLC. 

3. 

Mount the IBBS system to structure in a suitable area of the aircraft utilizing the 
practices identified in AC 43.13-2A/1B.  Ensure the mounting points and fasteners 
are suitable for the weight of the IBBS unit, consult the specifications for details.  Do 
not mount the IBBS in the firewall forward area.   Select an area that is accessible 
to allow for future battery servicing.  The preferred operating temperature range of 
the system is -40 C° to 60 C°, the effective charging temperature range is -40 C° to 
40 C° with extended charging times below 0 C°.  Select an installation location that 
takes these temperatures into consideration. 

 

Note:  Rechargeable lithium cells are capable of generating hazardous emissions when 
defective or subject to physical or operational abuse.  Although the IBBS system is 
protected from abusive failure conditions and includes a variety of fail-safe mechanisms, 
conditions may occur that could cause a Thermal Runaway (TR) event resulting in the 
venting of smoke or fumes and/or liquid from the designated vent port.   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 mounting the IBBS enclosure.   
 
The mounting area must meet one of the following requirements:    

i. 

A piece of 2024-T3 or T42 (alternate 6061-T6 or T62) sheet aluminum at least 

0.050” thick material minimum.

 

Supported by at least 4 fasteners on at least two opposite edges with a 
ma

ximum unsupported panel dimension of 12” in one direction and a 15” in the 

other direction. 

ii. 

Existing support brackets or rails that are 

at least 0.032” thick that are part of an 

avionics rack and form a flat surface for mounting.  
 
Important mounting notes: 

a.  The IBBS unit must be installed in the horizontal axis with respect to the 

mounting base plate of the unit. 

b.  Ensure there is sufficient clearance around the IBBS unit for the wiring harness 

and vent hose, and ensure sufficient clearance to fuel tanks, fuel lines, oxygen 
lines or any other critical systems. 

c.  Visually inspect the IBBS unit to ensure no damage has occurred to the unit 

prior to installation.  Do not deform the unit enclosure by means such as drilling, 
bending or cutting of the enclosure.  Do not open or modify the IBBS unit in any 
manner. 

 
 
 
 
 

 

Содержание IBBS-12v-6ah-CRT-V

Страница 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...

Страница 2: ...ilots 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 prac...

Страница 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...

Страница 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...

Страница 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...

Страница 6: ...re pin 2 must have 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 inp...

Страница 7: ...onnection 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 output wires when power on the normal aircraft bus fal...

Страница 8: ...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...

Страница 9: ...ck 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 connected equipment remains energized Th...

Страница 10: ...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...

Страница 11: ...replaced with the same Part Number unit or later FAA approved revision The use of alternate models will require a new FAA installation approval The internal battery is not field replaceable The IBBS u...

Страница 12: ...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 procedures 10 After completing these tests rec...

Страница 13: ...s and 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 Protect...

Страница 14: ...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 3 3 amps ch...

Страница 15: ...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...

Страница 16: ...wiring harness View from back of 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 switch 9 Groun...

Страница 17: ...p n 725 0001 REV 3 0 2023 TCW Technologies LLC 17 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...

Страница 18: ...aus PA USA IBBS 24V 3AH CRT V Input 22 32 volts DC Output 24 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...

Страница 19: ...p 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 gr...

Страница 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...

Страница 21: ...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...

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