HIRF Protection

FAR 23.2520 HIRF Protection

FAR 23.2520 requires Part 23 airplane electrical and electronic systems to be protected from High-Intensity Radiated Fields (HIRF) for safe flight and IFR ops.

In Plain English

FAR 23.2520 is a Part 23 airworthiness design standard that protects airplanes from High-Intensity Radiated Fields (HIRF) — the strong electromagnetic energy radiated by sources like high-power radar, broadcast transmitters, and military emitters. The concern is that this energy can disrupt avionics and electronic flight controls.

The rule applies to electrical and electronic systems based on how critical they are:

  • Safety-critical systems (those whose failure would prevent continued safe flight and landing) must be designed and installed so that:
    • The function is not adversely affected during or after HIRF exposure, and
    • The system recovers normal operation in a timely manner after exposure, unless recovery would conflict with other operational requirements.
  • IFR-approved airplanes have an additional requirement: any system whose failure would significantly reduce airplane capability or the crew's ability to handle an adverse condition must also recover normal operation in a timely manner after HIRF exposure.

Operationally, this is why your certified avionics keep working when you fly past a radar site or broadcast tower — the certification standard required the manufacturer to prove HIRF tolerance.

Regulation Text
14 CFR § 23.2520
§ 23.2520 High-intensity Radiated Fields (HIRF) protection. (a) Each electrical and electronic system that performs a function, the failure of which would prevent the continued safe flight and landing of the airplane, must be designed and installed such that— (1) The function at the airplane level is not adversely affected during and after the time the airplane is exposed to the HIRF environment; and (2) The system recovers normal operation of that function in a timely manner after the airplane is exposed to the HIRF environment, unless the system's recovery conflicts with other operational or functional requirements of the system. (b) For airplanes approved for IFR operations, each electrical and electronic system that performs a function, the failure of which would significantly reduce the capability of the airplane or the ability of the flightcrew 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 airplane is exposed to the HIRF environment. [Doc. No. FAA-2015-1621, Amdt. 23-64, 81 FR 96689, Dec. 30, 2016, as amended by Doc. No. FAA-2022-1355, Amdt. 23-65, 87 FR 75710, Dec. 9, 2022]
Oral Exam Questions a DPE Might Ask
Q1What does HIRF stand for, and why does Part 23 require protection against it?
HIRF means High-Intensity Radiated Fields — strong external electromagnetic energy. Per FAR 23.2520, electrical/electronic systems whose failure would prevent continued safe flight and landing must be designed so HIRF exposure doesn't adversely affect them and they recover normally afterward.
Q2How does FAR 23.2520 treat safety-critical systems differently from systems on IFR-approved airplanes?
FAR 23.2520(a) requires that safety-critical systems are not adversely affected during or after HIRF exposure and recover in a timely manner. FAR 23.2520(b) adds that on IFR-approved airplanes, systems whose failure would significantly reduce capability must also recover normal operation in a timely manner.
Q3Under FAR 23.2520, is there any exception to the requirement that a system recover normal function after HIRF exposure?
Yes. FAR 23.2520(a)(2) allows an exception when the system's recovery would conflict with other operational or functional requirements of the system.
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FAR 23.2520 — HIRF Protection for Airplane Systems