E T X T S O L I T H I U M B A T T E R I E S
180426
4
Airworthiness Limitations
The conditions and tests for TSO approval of this article are minimum performance standards.
Those installing this article, on or in a specific type and class of aircraft, must determine that the
aircraft installation conditions are within the TSO standards. The article may be 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 the Title
14 of the Code of Federal Regulations.
There are no new (or additional) airworthiness limitations associated with this equipment
and/or installation.
FAA APPROVAL:
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Printed Name/ Title
Signature
Dated
MARK J DALRYMPLE
Digitally signed by MARK J DALRYMPLE
Date: 2021.03.26 11:43:28 -06'00'
