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MOD Upgrading the ignition backup battery in a Carbon Cub E/FX-3 to a TCW IBBS 3AH battery

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Neal

Forums Chief Pilot
Staff member
Joined
Oct 31, 1996
Posts
1,360
Type aircraft owned
Carbon Cub FX-3
Base airport
KFCI
Ratings
COMM, IFR, MEL, SEL
While I'm still testing the EarthX backup battery as outlined in this thread, I'll start a thread for those considering use of the TCW IBBS 3AH LiFePO4 battery. I welcome discussion on wiring required for a EX-3/FX-3 which the factory uses a 12V AGM battery, typically the PowerSonic P1221S which is a 2AH battery.

Items required:



The FX-3 has a two position emergency ignition switch OFF/ON.

From my high level overview and not looking at the current schematic of the ignition backup circuit, hopefully someone can post that, it seems the current incoming positive would go to PIN 5 and the ground PIN 9. However, the difference here is the OUTPUT of the IBBS battery goes out 6,7,8 so this would require some wiring change so that output goes to the Light Speed Ignition. I'm interested in how that's currently wired and what would need to be changed to effect this battery upgrade.

Open to discussion and share knowledge to help others that may be considering this option.

Light Speed diagram below, others and manual attached.

LSE Plasma Ignition.jpg
 

Attachments

  • General Wiring Diagram.jpg
    General Wiring Diagram.jpg
    59.9 KB · Views: 0
  • IBBS-12v-3ah.pdf
    IBBS-12v-3ah.pdf
    505.2 KB · Views: 2
Would tying pins 5 and 6 together work as a drop in replacement for the current setup? PIN 5 would the incoming charge and sense, pin 6 would be the output from the battery to the ignition.
 
A consideration that needs thought is how we engage the backup battery and power the LSE ignition module by turning emergency ignition ON. We need to make sure doing so removes the charge current, triggers IBBS sense to provide power and powers the R ign module for ground testing.
 
My assumption is the OFF/ON toggle in the FX-3 for emergency ignition is a "charger" control? In the OFF position, charger is enabled. In the ON position, charger is removed?

Nope. Doesn't make sense. We need to enable the R ign circuit to be powered by the battery. Cancel above.

Click images if needed. Sourced from AMM REV B

Ignition-backup-system.jpg
Ignition-System-2.jpg
Ignition-system.jpg
 

Attachments

Last edited:
If you are going as far as to replace the PowerSonic AGM with a TCW IBBS, I think that it makes much more sense remove the PowerSonic completely and connect the right ignition directly to the existing TCW IBBS 3Ah. This would then have a 3.93 A load out of a max continuous current of 5 Amps. The 3Ah capacity of the IBBS will then give you >30 min IFR-required minimums. If you want more time, swap out the IBBS 3 Ah for a TCW IBBS 6Ah or an EarthX EBBS (7.8 Ah).

I am just completing a design to be able to power the majority of the avionics, including a radio and transponder, and the right ignition off a single EarthX EBBS. Hopefully, this week, I will be able to measure real-life current draws to compare them to the datasheets.
 
Re-reading the IBBS manual this morning and attaching the pin connector diagram. Slight correction to my initial wiring assumption but let me know your thoughts on this.

Error: Pins 6, 7, 8 are pass through power
Correction: Pins 12, 13, 14, 15 are the wires that provide power to the loads such as the Ignition module when the sensing falls below 11V.

So it seems to me the following wires can all be connected to the positive terminal of the battery:

Pin 5: charge/sense
Pin 2: Battery state of charge
Pin 12 (and could also include 13, 14, 15): which would provide the output power to the ignition module when the emergency ignition switch is engaged (ON) to open the circuit for the R ignition to receive battery power.

Pin 9: Ground

Thoughts/Feedback?

ibbs-wiring-connector.jpg
 

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