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E T X   T S O   L I T H I U M   B A T T E R I E S  
 

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7

6)

 

Verify battery terminals are clean and terminal screws are properly secured (torque to 
45in-lbs). 

7)

 

Visually inspect the vent tubes to ensure they are not blocked (plugged, pinched or 
kinked). 

8)

 

Verify the battery box and or battery restraint system is in good working order. The 
foam insert (190531)

 

is used to loosely hold the battery in a corner on the opposite 

end of the box from drain hole (up to +-1/8” of movement sided to side or front to 
back is ok; as measured at the bottom of the box).

  

 

9)

 

Test complete, record in Aircraft Logbook with inspection info or storage log. 

Aircraft Charging System Maintenance Requirements  

An annual inspection (check and/or test) is required for the voltage regulator and Over-
Voltage Protection Device (OVPD) or System (OVS) of the aircraft charging system for safe 

operation of the battery and aircraft electrical system.  The regulator and OVPD or OVS 
may physically be separate devices or in a single housing.  Follow the regulator and OVP 

manufacturer’s ICA or maintenance instructions for annual checks and or tests.  

 
Battery Charging 

If at any time the aircraft will not start, or the battery seems low, or the voltage is less than 

13.2 volt, charge it for the recommended time and charge rates shown below and disconnect 
the charger when charging is complete.  The recommended and maximum charge rate is 

specified on the top label of the battery.  Never exceed the maximum charging amps for 
your battery.   

 
This table shows typical charging times for the battery: 

 

Model 

Charging Amps 

Charging Time 

ETX900-TSO 

5 amp (TM291 Charger) 

3 hour 

10 amp (TM275) 

1.5 hour 

 

 

      

Lithium batteries have a very low self-discharge rate which means the battery, if 
disconnected from the aircraft, could “hold its charge” for over a year. However, some 

aircraft may have systems that use a small amount of power with the “Master switch” off.  In 
those cases, we recommend disconnecting a battery cable from the battery during long term 

storage (greater than 6 months).   
 

Only an approved battery charger shall be used: 
 

Optimate TM291 (5 amp) or TM275 (9.5amp)  

 

If the battery has been over-discharged and “disconnected”, the voltage at the battery 
terminal should be near zero volts if the battery still has a load on it.  If the battery is 

disconnected from the load it will automatically reconnect and the terminal voltage return to 
> 9volts (remove the load by removing the positive or negative cables from the battery).  In 

Содержание ETX900-TSO

Страница 1: ...mments 7 31 2020 R Nicoson Copyright 2020 EarthX Inc All rights reserved The information contained in this document is the property of EarthX Inc EarthX reserves the right to make changes to its docum...

Страница 2: ...ttery Charging 7 Battery End of Life 8 Battery Storage and Handling 9 Battery Operation 9 Normal Operation 10 Abnormal Operation 10 Emergency Operation 10 Emergencies with Aircraft Charging System as...

Страница 3: ...attery is part of the electrical system as a Secondary function with the Alternator system being Primary in the aircraft electrical system The battery within this system has two subfunctions Starting...

Страница 4: ...The capacity demand storage requirement should not exceed 31 Amps for 30 Minutes Timely pilot identification and load shedding assumed per normal procedures An Electrical Load Analysis ELA is require...

Страница 5: ...installed according to 14 CFR part 43 or the applicable airworthiness requirements The Airworthiness Limitations section is FAA approved and specifies maintenance required under 43 16 and 91 403 of t...

Страница 6: ...ers will be notified of a change to the ICA via the customer s email of record Battery Maintenance Requirements The ETX900 TSO battery is a maintenance free battery with no internal replaceable compon...

Страница 7: ...capacity is capable of supporting the aircraft s emergency load for the required amount of time it is consider fit for continued service It is recommended that the article be replaced after 6 years o...

Страница 8: ...time the aircraft will not start or the battery seems low or the voltage is less than 13 2 volt charge it for the recommended time and charge rates shown below and disconnect the charger when chargin...

Страница 9: ...GPU plug stating the max current allowed Never jump start from a car size battery or larger Never charge a faulty battery a battery that will not accept a charge or hold a charge Never use the de sul...

Страница 10: ...nd inspected annually Our batteries can be stored at temperatures between 40 C to 70 C Our batteries have no liquid inside and will not freeze Special care must be taken in the handling shipping and s...

Страница 11: ...ing or storage limits of the battery As long as the bus voltage current remains normal this is not an emergency Emergency Operation Emergencies with Aircraft Charging System as Root Cause i If the bat...

Страница 12: ...rs and or smoke through vent system and to outside the aircraft Terminology The following table describes the terminology used in this document Ah Amp Hour is a unit of measure of charge that can be s...

Страница 13: ...rthX Battery 2 1 190531 35 Ah Battery Box Insert 3 1 11MM12 Amber 12 Volt LED 4 1 200208 Fault Indicator Placard 5 AR Wire Retention Ties Hardware Insulation per AC 43 13 1B Chapter 11 Below is pictur...

Страница 14: ...nt Possible Cause Recommended Action Slow Flashing 5s on 5s off 12 8 14 6V Normal Cell to cell charge level imbalance No pilot action is required in flight The pilot should report battery problem to m...

Страница 15: ...ischarged Pilot to make preparations to land prior to the battery s reserve capacity being depleted Slow Flashing 5s on 5s off Greater than 15V high charge amps high voltage warning light on Over char...

Страница 16: ...E T X T S O L I T H I U M B A T T E R I E S 180426 15...

Страница 17: ...E T X T S O L I T H I U M B A T T E R I E S 180426 16...

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