14 C.F.R. § 21.7
Continued airworthiness and safety improvements for transport category airplanes
(a) On or after December 10, 2007, the holder of a design approval and an applicant for a design approval must comply with the applicable continued airworthiness and safety improvement requirements of part 26 of this subchapter.
(b) For new transport category airplanes manufactured under the authority of the FAA, the holder or licensee of a type certificate must meet the applicable continued airworthiness and safety improvement requirements specified in part 26 of this subchapter for new production airplanes. Those requirements only apply if the FAA has jurisdiction over the organization responsible for final assembly of the airplane.
Notes of Decisions
Cited in 2
cases, 2011–2011 · leading case: Burton v. Twin Commander Aircraft LLC, 254 P.3d 778 (Wash. 2011).
Burton v. Twin Commander Aircraft LLC, 254 P.3d 778 (Wash. 2011). “3 ; see 14 C.F.R. § 21.7 . Also, as a type certificate holder Twin Commander has the obligation to submit design changes if the FAA issues an airworthiness directive that makes such changes necessary, 14 C.”
Burton v. Twin Commander Aircraft, LLC, 171 Wash. 2d 204 (Wash. 2011). “3 ; see 14 C.F.R. § 21.7 . Also, as a type certificate holder Twin Commander has the obligation to submit design changes if the FAA issues an airworthiness directive that makes such changes necessary, 14 C.”
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