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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  
 

 

Installation Requirements 

“This  article  meets  the  minimum  requirements  of  technical  standard  order  (TSO)  C179b.  

Installation of this article requires separate approval.”  The article may be installed only according 
to  14  CFR  part  43  or  the  applicable  airworthiness  requirements.      Below  are  the  installation 

specific, in-service requirements as identified in EarthX’s AML STC process document 18114-03 

and is not part of the TSO Part (LRU) specific certification under TSO-C179b: 

 

The maximum charge rating is 80 amps, so the aircraft alternator rated output must be 80 
amps or less. 

 

The  maximum  voltage  output  from  aircraft charging system  shall  not  exceed  16  volts.  

Thus,  an  automatic  over-voltage  protection  device  (OVPD)  is  required  on  the  aircraft 
charging system. 

 

The battery fault monitoring indicator must be installed and tested. 

 

The battery vent system must be installed (see installation section of this manual). 

 

The  cranking  current  demand  should  not  exceed;  a Peak  Power  (Ipp)  800/390  Amps 

(+23C/-18C), Rated Power (Ipr) 600/365 Amps (+23C/-18C).  Note: Old CCA spec is 

Ipr at -18C. 

 

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 required. 

 

The  battery  must  be  installed  in  such  a  manner  and  or  location  to  limit  radiant  and 

convection heating.  The maximum short term (30 minute) environmental temperature of 

battery  location  should  be  less  than  65°C.      The  maximum  short  term  (30  minute) 
environmental temperature of battery location while the aircraft is on the ground shall not 
exceed 85°C.   The battery’s normal operating temperature is -30

°

C to 60

°

C. 

 

The battery should be secured in the existing battery box or battery holder as detailed in 

this manual and aircraft model specific STC IWD instruction.   

The  maintenance  must  comply  with  the  requirements  of  the  Instructions  for  Continued 
Airworthiness (ICA), a separate document. 

Specifications 

Model: ETX900-TSO-REVx 
Voltage 

13.2 V  

Capacity (1C, 1hour rate at 23 

°

C) 

15.6Ah @ 1C rate (See below) 

Capacity vs Temperature 

25 °C = 15.6Ah 

0°C = 15.3Ah 
-30°C = 15.0Ah 

Содержание ETX900-TSO

Страница 1: ...the property of EarthX Inc EarthX reserves the right to make changes to its documents or products without notice It is the responsibility of each user to ensure that all applications of EarthX s prod...

Страница 2: ...E R I E S Revision Log Rev Description Date New Created New 4 07 2018 A Update to limitations DO 311A 8 30 2018 B Updated elect mech Installation sections Incorporate FAA AEG comments 11 24 2020 I C...

Страница 3: ...Location 9 Battery Installation 9 Battery Vent Installation 10 Fault Monitoring Installation 10 Return to Service Checks Tests 13 Aircraft Voltage Monitoring Equipment if applicable 13 Accessory Parts...

Страница 4: ...t today Lithium batteries are fundamentally different than lead acid batteries A lithium battery voltage remains relatively constant while discharging while voltage for a lead acid battery decreases A...

Страница 5: ...al run away containment system The design aligns with the requirements for a FAA approved lithium battery as per RTCA performance specification DO 311A and DO 160 In the event of a charging system fai...

Страница 6: ...d should not exceed a Peak Power Ipp 800 390 Amps 23C 18C Rated Power Ipr 600 365 Amps 23C 18C Note Old CCA spec is Ipr at 18C The capacity demand storage requirement should not exceed 31 Amps for 30...

Страница 7: ...C 20 depth of discharge 2000 cycles 10C discharge rate 25 C 80 depth of discharge Life Years 6 Years Weight 5 4lb Dimensions 6 5in L x 3 1in W x 6 6in H 166mm L x79mm W x168mm H Environmental Rating r...

Страница 8: ...E T X T S O L I T H I U M B A T T E R I E S 5...

Страница 9: ...e current counting to track the charge level As seen from the graph the voltage only varies 4V for nearly 80 of the discharge cycle at 25 Deg C 13 4V is a good indication of full charge while 12 8V is...

Страница 10: ...0 F an equivalent lead acid battery will outperform a lithium battery see the graph below Like lead acid batteries lithium batteries discharge performance is lower as the temperature decreases meaning...

Страница 11: ...on temperature At high temperatures 25 C the cell internal resistance decreases so the self discharge rate increases See the graph below for self discharge rates in per month versus temperature 30 20...

Страница 12: ...Iron Phosphate batteries are very robust but if mishandled or misused they can rupture and they can burn Never disassemble the battery or disable the built in Battery Management System BMS It is reco...

Страница 13: ...ied tubing should be used The tubing is chemical resistant and rated for 500 F 1 4 ID 5 16 OD Teflon tubing The supplied stainless steel elbows allow the vent tubes to be routed to the left or right s...

Страница 14: ...st other manufacturers male quick connect terminals The following two examples detail how to connect the fault monitoring output to an EFIS general purpose discrete input The EFIS DC source negative m...

Страница 15: ...Monitoring Connection to 12V LED Part 11MM12 Connect the LED s red wire to a spare or existing fuse or breaker off the electrical bus Use any 25 Amp to 2 Amp fuse or breaker Connect the LED s white wi...

Страница 16: ...not exist or are not adjustable The low charge level is very different from a lead acid battery for a lithium battery is completely drained at approximately 11 5V and the normal resting voltage is 13...

Страница 17: ...ry 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...

Страница 18: ...ltage reading then use a voltmeter to check the voltage while charging If the battery gets hot while charging discontinue charging and use Do not charge battery in temperatures above 140 degrees F 60C...

Страница 19: ...out the online warranty submission form located on the EarthX website EarthX s acceptance of any items shipped to EarthX for warranty replacement shall not be deemed an admission that the item s are...

Страница 20: ...aircraft s LED or EFIS If the fault LED on the battery is not extinguished the battery should be replaced Solid Light that turns off after 3 minutes Any voltage Short Circuit protection was activated...

Страница 21: ...Federal Regulations or CFR s Title 49 CFR Sections 100 185 of the U S Hazardous Materials Regulations HMR Terminology The following table describes the terminology used in this document Ah Amp Hour i...

Страница 22: ...Temperature 2 4 4 11 Passed functional performance per DO 311A Section 2 2 1 11 Short Circuit with Protection Enabled 2 4 4 12 Passed functional performance per DO 311A Section 2 2 1 12 Overdischarge...

Страница 23: ...6 Equipment tested to Categories B Operational Shock and Crash Safety 7 Equipment tested to Categories B Vibration 8 Equipment tested to Category R S and U aircraft zone 1 and 2 for fixed wing turboje...

Страница 24: ...Lightning Direct Effects 23 Equipment identified as Category X no test performed Icing 24 Equipment identified as Category X no test performed Electrostatic Discharge 25 Equipment tested to Categorie...

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