https://www.fuseaviation.com/troubleshooting-blog daily 0.75 2025-01-29 https://www.fuseaviation.com/troubleshooting-blog/ads-b-fail-in-flight monthly 0.5 2025-01-29 https://images.squarespace-cdn.com/content/v1/5e72e3693b16e04cc4bef593/a86c2694-3387-4b31-b004-8a6c505312a3/20220425_083740.jpg Troubleshooting - ADS-B Fail in Flight - Make it stand out Whatever it is, the way you tell your story online can make all the difference. https://images.squarespace-cdn.com/content/v1/5e72e3693b16e04cc4bef593/3a3aa60f-e179-4524-88fb-d51e830d76e7/20220616_082657.jpg Troubleshooting - ADS-B Fail in Flight - Make it stand out Whatever it is, the way you tell your story online can make all the difference. https://images.squarespace-cdn.com/content/v1/5e72e3693b16e04cc4bef593/dcb3d466-0570-4ec4-971b-e741534b01b8/20220616_082812.jpg Troubleshooting - ADS-B Fail in Flight - Make it stand out Whatever it is, the way you tell your story online can make all the difference. https://www.fuseaviation.com/troubleshooting-blog/blog-post-title-one-w8ss6 monthly 0.5 2022-06-27 https://images.squarespace-cdn.com/content/v1/5e72e3693b16e04cc4bef593/7c8098bf-d09e-4a78-8c32-1944f8101e1e/processed_20211117_111752.jpg Troubleshooting - ATC Reports Loss Of Altitude - Make it stand out Upon checking the resistance with a multimeter, the blind encoder ground was reading high at 39 ohms. Reminder: A good ground is usually less than 1 ohm. The ground wire was chased to the ground stud and the ground screw was found loose causing the high resistance. The screw in this situation was striped and could not be tightened. https://images.squarespace-cdn.com/content/v1/5e72e3693b16e04cc4bef593/f30ffe32-8088-49a0-bae5-da32d8a051ec/processed_20211117_114606.jpg Troubleshooting - ATC Reports Loss Of Altitude - Make it stand out Corrective action: The ground screw was replaced by a ground stud using a brass screw and nuts for better conductivity. After the replacement of the ground screw the ground wire was checked for resistance and was found to be within serviceable limits of 0.3 ohms. After putting the system back together a transponder test was accomplished in accordance with 14 CFR 91.411 and 91.413. This is because any time work is accomplished on the altitude reporting system 91.411 (a)(3) and 91.413 (b) state that testing must be accomplished “Following the installation or maintenance on the automatic pressure altitude reporting system of the ATC transponder where data correspondence error could be introduced, the integrated system has been tested, inspected and found to comply with paragraph (c), Appendix E, of part 43”. Aircraft has flown multiple flights with no altitude issues reported. If no discrepancies are found after performing the troubleshooting steps mentioned above, the next step would be to check wiring integrity from the blind encoder to transponder. 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