(a) Maintain the quality control system in conformity with the data and procedures approved for the production certificate; and
(b) Determine that each part and each completed product, including primary category aircraft assembled under a production certificate by another person from a kit provided by the holder of the production certificate, submitted for airworthiness certification or approval conforms to the approved design and is in a condition for safe operation.
[Doc. No. 5085, 29 FR 14569, Oct. 24, 1964, as amended by Amdt. 21–64, 53 FR 48521, Dec. 1, 1988; Amdt. 21–70, 57 FR 41368, Sept. 9, 1992]