C.F.R. » Title 14 » CHAPTER I—FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION › SUBCHAPTER C—AIRCRAFT › PART 27—AIRWORTHINESS STANDARDS: NORMAL CATEGORY ROTORCRAFT › Subpart A—General

14 C.F.R. § 27.1

Applicability

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(a) This part prescribes airworthiness standards for the issue of type certificates, and changes to those certificates, for normal category rotorcraft with maximum weights of 7,000 pounds or less and nine or less passenger seats.

(b) Each person who applies under Part 21 for such a certificate or change must show compliance with the applicable requirements of this part.

(c) Multiengine rotorcraft may be type certified as Category A provided the requirements referenced in appendix C of this part are met.

[Doc. No. 5074, 29 FR 15695, Nov. 24, 1964, as amended by Amdt. 27-33, 61 FR 21906, May 10, 1996; Amdt. 27-37, 64 FR 45094, Aug. 18, 1999]
Notes of Decisions
Cited in 1 case, 2019–2019 · leading case: Mary Riggs v. Airbus Helicopters, Inc., 939 F.3d 981 (9th Cir. 2019).
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Mary Riggs v. Airbus Helicopters, Inc., 939 F.3d 981 (9th Cir. 2019). “Standards for certification of helicopters, such as the Crashed Helicopter, are set forth in 14 C.F.R. § 27.1 . After demonstrating compliance with the FARs, an aircraft owner may obtain a certificate from the FAA approving the aircraft’s design.”
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