E T X 1 2 0 0 - 2 4 - T S O L I T H I U M B A T T E R Y Table of Contents Revision Log ..................i Table of Contents ................1 Airworthiness Limitations ..............
E T X 1 2 0 0 - 2 4 - T S O L I T H I U M B A T T E R Y Airworthiness Limitations The Airworthiness Limitations section is FAA approved and specifies maintenance required under Secs. 43.16 and 91.403 of Title 14 of the Code of Federal Regulations unless an alternative program has been FAA approved.
Introduction This manual covers the inspection, maintenance (charging) and replacement aspects for the ETX1200-24-TSO battery installed on 14 CFR Part 23 aircraft. Installation of the rechargeable lithium battery defined herein meets the guidance of AC 20-184. In accordance with Federal Aviation Administration (FAA) Advisory Circular (AC) 23.1309-1E and FAA Technical Standard...
B A T T E R Y Description EarthX Lithium batteries are a maintenance free replacement for lead-acid or lithium batteries. The battery operation is automatic (no operator control). The battery is part of the main aircraft electrical system with the alternator (charging system) being the primary power source and the battery being the secondary power source;...
E T X 1 2 0 0 - 2 4 - T S O L I T H I U M B A T T E R Y 4. Remove the battery negative (black) cable. 5. Disconnect the battery fault/status monitoring plug. 6.
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E T X 1 2 0 0 - 2 4 - T S O L I T H I U M B A T T E R Y Firewall Forward Battery Vent Installation Example 4. If replacing the tube that exits the belly of the aircraft, leave at least 1” exposed on the outside of the aircraft and secure in place with RTV silicon.
To replace the fuse, push the ends of the fuse holder together and ¼ turn counterclockwise to open the fuse housing, then replace with a new fuse (¼ x 1 ¼”, 1-amp, fast blow fuse). Fault/Status Indicator Replacement The installation or replacement of the EarthX Fault/Status LED Indicator (part# 11MM24) is detailed below. Fault / Status Indicator 1.
E T X 1 2 0 0 - 2 4 - T S O L I T H I U M B A T T E R Y 10. Behind the instrument panel, route the red wire (with inline fuse) to an instrument circuit breaker;...
E T X 1 2 0 0 - 2 4 - T S O L I T H I U M B A T T E R Y Battery Inspection Intervals Battery: Upon installation, record the next battery inspection due date based on the battery age as follows: •...
• Will not hold a charge (<26.4 volts a week after charging the battery to full charge) At battery end-of-life contact EarthX. The only approved replacement lithium battery is an EarthX battery of the same model number. The model number is displayed on the top label of the battery.
(greater than 6 months). Only use a Lithium Iron Phosphate (LiFePO4) charger or other compatible chargers listed on EarthX website https://earthxbatteries.com/ If the battery has been over-discharged and “disconnected” (meaning automatic electronic disconnect commanded by the Battery Management System), the voltage at the battery terminal should be near zero volts if the battery still has a load on it.
B A T T E R Y next (step 2) plug the charger power cord into AC outlet (or press the reset button on the charger). The charger should startup and go into the “Save” charging mode. If not contact EarthX technical support.
E T X 1 2 0 0 - 2 4 - T S O L I T H I U M B A T T E R Y Verify aircraft charging system is Over-charging (due to Slow Flashing Greater than functioning properly;...
( https://www.call2recycle.org/ Do not incinerate or expose to open flames! The Safety Data Sheet (SDS) is available on EarthX’s website. Always follow the manufacturers’ recommended safety precautions and procedures. Weight and Balance The installation of the battery is considered a permanent installation. The basic aircraft weight and balance should be updated inclusive of the added equipment when the installation is completed and documented on the aircraft Weight and Balance Record (WBR).
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E T X 1 2 0 0 - 2 4 - T S O L I T H I U M B A T T E R Y • UN 38.3, – United Nations ST/SG/AC.10/11/Rev.6, Recommendations on the Transport of Dangerous Goods, Manual of Tests and Criteria, Section 38.3, Lithium Metal and Lithium-Ion Batteries.
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