C.F.R. » Title 14 » CHAPTER I—FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION › SUBCHAPTER C—AIRCRAFT › PART 25—AIRWORTHINESS STANDARDS: TRANSPORT CATEGORY AIRPLANES › Subpart D—Design and Construction

14 C.F.R. § 25.605

Fabrication methods

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(a) The methods of fabrication used must produce a consistently sound structure. If a fabrication process (such as gluing, spot welding, or heat treating) requires close control to reach this objective, the process must be performed under an approved process specification.

(b) Each new aircraft fabrication method must be substantiated by a test program.

[Doc. No. 5066, 29 FR 18291, Dec. 24, 1964, as amended by Amdt. 25-46, 43 FR 50595, Oct. 30, 1978]
Notes of Decisions
Cited in 1 case, 2007–2007 · leading case: United States Ex Rel. Smith v. Boeing Co., 505 F. Supp. 2d 974 (D. Kan. 2007).
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United States Ex Rel. Smith v. Boeing Co., 505 F. Supp. 2d 974 (D. Kan. 2007). “601 ); and failed to comply with regulatory requirements on fabrication methods ( 14 CFR § 25.605 ). Paragraph 95 of the SAC alleges that guidelines in the Defense Department Handbook on Airworthiness Certification Criteria were incorporated into the contracts and the defendants…”
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