# 14 C.F.R. § 29.1317 (2026): High-intensity Radiated Fields (HIRF) Protection > Federal · Regulations · In force URL: https://www.frixlaw.com/law-library/statutes/CFR_T14_P29_S29_1317 ## Section - **Citation:** 14 C.F.R. § 29.1317 (2026) - **Heading:** High-intensity Radiated Fields (HIRF) Protection - **Jurisdiction:** Federal - **Kind:** Regulations - **Status:** In force - **Text as of:** August 14, 2026 - **Source:** Compiled text - **Location:** Title 14 CFR: Aeronautics and Space / Chapter I: FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION / Part 29: AIRWORTHINESS STANDARDS: TRANSPORT CATEGORY ROTORCRAFT / Subpart F: Equipment / § 29.1317: § 29.1317 High-intensity Radiated Fields (HIRF) Protection. ## Text (a) Except as provided in paragraph (d) of this section, each electrical and electronic system that performs a function whose failure would prevent the continued safe flight and landing of the rotorcraft must be designed and installed so that— (1) The function is not adversely affected during and after the time the rotorcraft is exposed to HIRF environment I, as described in appendix E to this part; (2) The system automatically recovers normal operation of that function, in a timely manner, after the rotorcraft is exposed to HIRF environment I, as described in appendix E to this part, unless this conflicts with other operational or functional requirements of that system; (3) The system is not adversely affected during and after the time the rotorcraft is exposed to HIRF environment II, as described in appendix E to this part; and (4) Each function required during operation under visual flight rules is not adversely affected during and after the time the rotorcraft is exposed to HIRF environment III, as described in appendix E to this part. (b) Each electrical and electronic system that performs a function whose failure would significantly reduce the capability of the rotorcraft or the ability of the flightcrew to respond to an adverse operating condition must be designed and installed so the system is not adversely affected when the equipment providing these functions is exposed to equipment HIRF test level 1 or 2, as described in appendix E to this part. (c) Each electrical and electronic system that performs such a function whose failure would reduce the capability of the rotorcraft or the ability of the flightcrew to respond to an adverse operating condition must be designed and installed so the system is not adversely affected when the equipment providing these functions is exposed to equipment HIRF test level 3, as described in appendix E to this part. electrical and electronic system that performs such a function whose failure would reduce the capability of the rotorcraft or the ability of the flightcrew to respond to an adverse operating condition must be designed and installed so the system is not adversely affected when the equipment providing these functions is exposed to equipment HIRF test level 3, as described in appendix E to this part. (d) Before December 1, 2012, an electrical or electronic system that performs a function whose failure would prevent the continued safe flight and landing of a rotorcraft may be designed and installed without meeting the provisions of paragraph (a) provided— (1) The system has previously been shown to comply with special conditions for HIRF, prescribed under § 21.16, issued before December 1, 2007; (2) The HIRF immunity characteristics of the system have not changed since compliance with the special conditions was demonstrated; and (3) The data used to demonstrate compliance with the special conditions is provided. [Doc. No. FAA-2006-23657, 72 FR 44027, Aug. 6, 2007] ## Nearby sections - [14 C.F.R. § 29.1301 (2026) § 29.1301 Function and installation.](https://www.frixlaw.com/law-library/statutes/CFR_T14_P29_S29_1301.md) - [14 C.F.R. § 29.1303 (2026) § 29.1303 Flight and navigation instruments.](https://www.frixlaw.com/law-library/statutes/CFR_T14_P29_S29_1303.md) - [14 C.F.R. § 29.1305 (2026) § 29.1305 Powerplant instruments.](https://www.frixlaw.com/law-library/statutes/CFR_T14_P29_S29_1305.md) - [14 C.F.R. § 29.1307 (2026) § 29.1307 Miscellaneous equipment.](https://www.frixlaw.com/law-library/statutes/CFR_T14_P29_S29_1307.md) - [14 C.F.R. § 29.1309 (2026) § 29.1309 Equipment, systems, and installations.](https://www.frixlaw.com/law-library/statutes/CFR_T14_P29_S29_1309.md) - [14 C.F.R. § 29.1316 (2026) § 29.1316 Electrical and electronic system lightning protection.](https://www.frixlaw.com/law-library/statutes/CFR_T14_P29_S29_1316.md) - [14 C.F.R. § 29.1317 (2026) § 29.1317 High-intensity Radiated Fields (HIRF) Protection.](https://www.frixlaw.com/law-library/statutes/CFR_T14_P29_S29_1317.md) - [14 C.F.R. § 29.1321 (2026) § 29.1321 Arrangement and visibility.](https://www.frixlaw.com/law-library/statutes/CFR_T14_P29_S29_1321.md) - [14 C.F.R. § 29.1322 (2026) § 29.1322 Warning, caution, and advisory lights.](https://www.frixlaw.com/law-library/statutes/CFR_T14_P29_S29_1322.md) - [14 C.F.R. § 29.1323 (2026) § 29.1323 Airspeed indicating system.](https://www.frixlaw.com/law-library/statutes/CFR_T14_P29_S29_1323.md) - [14 C.F.R. § 29.1325 (2026) § 29.1325 Static pressure and pressure altimeter systems.](https://www.frixlaw.com/law-library/statutes/CFR_T14_P29_S29_1325.md) - [14 C.F.R. § 29.1327 (2026) § 29.1327 Magnetic direction indicator.](https://www.frixlaw.com/law-library/statutes/CFR_T14_P29_S29_1327.md) - [14 C.F.R. § 29.1329 (2026) § 29.1329 Automatic pilot and flight guidance system.](https://www.frixlaw.com/law-library/statutes/CFR_T14_P29_S29_1329.md) - [14 C.F.R. § 29.1331 (2026) § 29.1331 Instruments using a power supply.](https://www.frixlaw.com/law-library/statutes/CFR_T14_P29_S29_1331.md) --- Source: Frix Law Library, https://www.frixlaw.com/law-library/statutes/CFR_T14_P29_S29_1317. Check the current official text before relying on it. Not legal advice.