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

14 C.F.R. § 27.607

Fasteners

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(a) Each removable bolt, screw, nut, pin, or other fastener whose loss could jeopardize the safe operation of the rotorcraft must incorporate two separate locking devices. The fastener and its locking devices may not be adversely affected by the environmental conditions associated with the particular installation.

(b) No self-locking nut may be used on any bolt subject to rotation in operation unless a nonfriction locking device is used in addition to the self-locking device.

[Amdt. 27-4, 33 FR 14533, Sept. 27, 1968]
Notes of Decisions
Cited in 1 case, 2012–2012 · leading case: Bouret Echevarria v. Caribbean Aviation Maint. Corp., 845 F. Supp. 2d 467 (D.P.R. 2012).
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Bouret Echevarria v. Caribbean Aviation Maint. Corp., 845 F. Supp. 2d 467 (D.P.R. 2012). “14 C.F.R. § 27.607 . Robinson argues that only Colin Sommer (“Sommer”), expert witness for Plaintiffs, could have provided testimony Robinson’s design was defective by the risk/utility test.”
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