MXS System Description and Installation Manual UM06945
© Sagetech Avionics 2022 Proprietary Confidential Page 11 of 56
2.5 Device Marking
The Part number 10-0000 includes the released hardware and software configuration.
2.6 Continued airworthiness
Every 24 Calendar months the MXS must be checked for Transponder and Altitude Encoder performance.
The Transponder must be tested, inspected and found to comply with 14 CFR Part 91.413 as described in
14 CFR 43 Appendix F. The altitude Encoder must be tested to ensure correspondence to the primary flight
altimeter, as described in AC 43-6D and 14 CFR 43 Appendix E in order to meet the maintenance
requirements of 14 CFR Part 91.411. If the difference between the automatic reporting output and the
altitude displayed at the altimeter shall not exceed 125 feet.
2.7 Installation Approvals and System Limitations
1. This article meets the minimum performance and quality control standards required by the
applicable technical standard orders (TSOs). Those installing this article, on or in a specific type or
class of aircraft, must determine that the aircraft installation conditions are within the applicable
TSOs standards. TSO articles must have separate approval for installation in an aircraft. The article
may be installed only according to 14 CFR parts 43 or the applicable airworthiness requirements.
2. All antennas used in the installation must meet the requirements specified in this manual.
3. The GPS receiver must use antenna meeting the requirements specified in this manual.
4. It is the installer’s responsibility to ensure the ADS-B Out system is compliant with AC 20-165A,
14 CFR 91.225 (b) and 91.227 when installed in accordance with Sagetech’s installation
instructions.
5. The MXS Transponder may be optionally configured to support single or diversity antenna
installations.
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