§ 25.1316. Electrical and electronic system lightning protection.
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/us/cfr/t14/s§ 25.1316·A research copy — for the controlling text, always check the official state or federal source. Not legal advice.
(a)Each electrical and electronic system that performs a function, for which failure would prevent the continued safe flight and landing of the airplane, must be designed and installed so that—
(1)The function is not adversely affected during and after the time the airplane is exposed to lightning; and
(2)The system automatically recovers normal operation of that function in a timely manner after the airplane is exposed to lightning.
(b)Each electrical and electronic system that performs a function, for which failure would reduce the capability of the airplane or the ability of the flightcrew to respond to an adverse operating condition, must be designed and installed so that the function recovers normal operation in a timely manner after the airplane is exposed to lightning. [Doc. No. FAA-2010-0224, Amdt. 25-134, 76 FR 33135, June 8, 2011]
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- Rules and RegulationsFinal special conditions; request for comments
- Rules and RegulationsFinal special conditions; request for comments
- Rules and RegulationsFinal special conditions; request for comments
- Rules and RegulationsFinal special conditions
- Rules and RegulationsNotice of petition for exemption received
- Rules and RegulationsFinal special conditions; request for comments
- NoticesNotice of proposed special conditions
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§ 25.1316
Electrical and electronic system lightning protection.
Fed. Reg.×7
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