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AMC1 23.2515 Electrical and electronic system lightning protection
Available versions for ERULES-1963177438-6866
ED Decision 2023/002/R
found in: CS-23 Amdt 6 AMC-GM Issue 4 - Normal-Category Aeroplanes (Mar 2023)
ED Decision 2019/020/R
found in: CS-23 Amdt 5 AMC-GM Issue 3 - Normal-Category Aeroplanes (Jul 2020)
ED Decision 2026/003/R
found in: CS-23 Amdt 6 AMC-GM Issue 5 - Normal-Category Aeroplanes (May 2026)
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AMC1 23.2515 Electrical and electronic system lightning protection ED Decision 2023/002/R ASTM F44 F3264-21 Standard Specification for Normal Category Aeroplanes Certification 9.4 Electrical and Electronic System Lightning Protection [F3061/F3061M-20](https://www.astm.org/Standards/F3061.htm) Standard Specification for Systems and Equipment in Small Aircraft Remarks [F3367-21a](https://www.astm.org/catalogsearch/result/?q=F3367) Standard Practice for Simplified Methods for Addressing High Intensity Radiated Fields (HIRF) and Indirect Effects of Lightning on Aircraft, as referenced in [F3061/F3061M-20](https://www.astm.org/f3061_f3061m-22b.html), paragraph 17.3.4, is not an EASA accepted practice. At variance with [F3061-20](https://www.astm.org/f3061_f3061m-22b.html): (a) paragraph 17.3.1 should be replaced with the following: each electrical or electronic system that performs a function, the failure of which would prevent the continued safe flight and landing of the aeroplane, must be designed and installed such that: (1) the function at the aeroplane level is not adversely affected during and after the time the aeroplane is exposed to lightning; and (2) the system recovers normal operation of that function in a timely manner after the aeroplane is exposed to lightning unless the system’s recovery conflicts with other operational or functional requirements of the system; (b) paragraph 17.3.2 should be replaced with the following: each electrical and electronic system that performs a function, the failure of which would reduce the capability of the aeroplane or the ability of the flight crew to respond to an adverse operating condition, must be designed and installed such that the system recovers normal operation of that function in a timely manner after the aeroplane is exposed to lightning; and (c) paragraphs 17.3.3 and 17.3.4 should be removed.
AMC1 23.2515 Electrical and electronic system lightning protection ED Decision 2019/020/R ASTM F44 F3264-18b Standard Specification for Normal Category Aeroplanes Certification 9.4 Electrical and Electronic System Lightning Protection: [F3061/F3061M-17](https://www.astm.org/Standards/F3061.htm) Standard Specification for Systems and Equipment in Small Aircraft
##### AMC1 23.2515 Electrical and electronic system lightning protection *ED Decision 2026/003/R* **ASTM F44 F3264 Standard Specification for Normal Category Aeroplanes Certification** *9.4* *Electrical and Electronic System Lightning Protection* [F3061/F3061M-24a](https://www.astm.org/Standards/F3061.htm) Standard Specification for Systems and Equipment in Small Aircraft [F3367-23](https://store.astm.org/f3367-23.html?_gl=1*fmb3sr*_gcl_au*MTcyMzgwODA2Mi4xNzcyMDM1ODg5) Standard Practice for Simplified Methods for Addressing High Intensity Radiated Fields (HIRF) and Indirect Effects of Lightning on Aircraft [AMC & GM to CS-23: Issue 4] [AMC & GM to CS-23: Issue 5]