C.F.R. » Title 14 » CHAPTER I—FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION › SUBCHAPTER C—AIRCRAFT › PART 33—AIRWORTHINESS STANDARDS: AIRCRAFT ENGINES › Subpart A—General

14 C.F.R. § 33.1

Applicability

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(a) This part prescribes airworthiness standards for the issue of type certificates and changes to those certificates, for aircraft engines.

(b) Each person who applies under part 21 for such a certificate or change must show compliance with the applicable requirements of this part and the applicable requirements of part 34 of this chapter.

[Amdt. 33-7, 41 FR 55474, Dec. 20, 1976, as amended by Amdt. 33-14, 55 FR 32861, Aug. 10, 1990]
Notes of Decisions
Cited in 2 cases, 1987–2016 · leading case: Sikkelee Ex Rel. Est. of Sikkelee v. Precision Airmotive Corp., 822 F.3d 680 (3rd Cir. 2016).
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Sikkelee Ex Rel. Est. of Sikkelee v. Precision Airmotive Corp., 822 F.3d 680 (3rd Cir. 2016). “§ 21 , and in the context of those procedures, to “pre-scriben airworthiness standards for the issue of type certificates,” 14 C.F.R. § 33.1 (a) (aircraft engines) (emphasis added); see also 14 C.”
Fagerquist v. W. Sun Aviation, Inc., 191 Cal. App. 3d 709 (Cal. Ct. App. 1987). · cites it 2× “Further, the record supports that if a checklist had been properly utilized and the mechanical history of the aircraft properly noticed, the crack in the left engine cylinder would have been discovered.”
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