Code of Federal Regulations

Title 14 - Aeronautics and Space
Volume: 1Date: 2020-01-01Original Date: 2020-01-01Title: Section § 29.610 - Lightning and static electricity protection.Context: Title 14 - Aeronautics and Space. CHAPTER I - FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION. SUBCHAPTER C - AIRCRAFT. PART 29 - AIRWORTHINESS STANDARDS: TRANSPORT CATEGORY ROTORCRAFT. Subpart D - Design and Construction. - General.
§ 29.610 Lightning and static electricity protection. (a) The rotorcraft structure must be protected against catastrophic effects from lightning. (b) For metallic components, compliance with paragraph (a) of this section may be shown by— (1) Electrically bonding the components properly to the airframe; or (2) Designing the components so that a strike will not endanger the rotorcraft. (c) For nonmetallic components, compliance with paragraph (a) of this section may be shown by— (1) Designing the components to minimize the effect of a strike; or (2) Incorporating acceptable means of diverting the resulting electrical current to not endanger the rotorcraft. (d) The electric bonding and protection against lightning and static electricity must— (1) Minimize the accumulation of electrostatic charge; (2) Minimize the risk of electric shock to crew, passengers, and service and maintenance personnel using normal precautions;
Code of Federal Regulations / Title 14 - Aeronautics and Space / Vol. 1 / 2020-01-01603
(3) Provide and electrical return path, under both normal and fault conditions, on rotorcraft having grounded electrical systems; and (4) Reduce to an acceptable level the effects of static electricity on the functioning of essential electrical and electronic equipment. [Amdt. 29-24, 49 FR 44437, Nov. 6, 1984; Amdt. 29-40, 61 FR 21907, May 10, 1996; 61 FR 33963, July 1, 1996; Amdt. 29-53, 76 FR 33135, June 8, 2011]