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  4. Part 21
  5. § 21.33
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14 CFR · Part 21

14 CFR § 21.33

Inspection and tests.

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Read in Subpart B
Part 21 Contents
  • Special Federal Aviation Regulation No. 88: Fuel Tank System Fault Tolerance Evaluation Requirements
  • Subpart A: General
  • Subpart B: Type Certificates
  • Subpart C: Provisional Type Certificates
  • Subpart D: Changes to Type Certificates
  • Subpart E: Supplemental Type Certificates
  • Subpart F: Production Under Type Certificate
  • Subpart G: Production Certificates
  • Subpart H: Airworthiness Certificates
  • Subpart I: Provisional Airworthiness Certificates
  • Subpart K: Parts Manufacturer Approvals
  • Subpart L: Export Airworthiness Approvals
  • Subpart N: Acceptance of Aircraft Engines, Propellers, and Articles for Import
  • Subpart O: Technical Standard Order Approvals
  • Subpart P: Special Federal Aviation Regulations
(a)

Each applicant must allow the FAA to make any inspection and any flight and ground test necessary to determine compliance with the applicable requirements of this subchapter. However, unless otherwise authorized by the FAA—

(1)

No aircraft, aircraft engine, propeller, or part thereof may be presented to the FAA for test unless compliance with paragraphs (b)(2) through (b)(4) of this section has been shown for that aircraft, aircraft engine, propeller, or part thereof; and

(2)

No change may be made to an aircraft, aircraft engine, propeller, or part thereof between the time that compliance with paragraphs (b)(2) through (b)(4) of this section is shown for that aircraft, aircraft engine, propeller, or part thereof and the time that it is presented to the FAA for test.

(b)

Each applicant must make all inspections and tests necessary to determine—

(1)

Compliance with the applicable airworthiness, aircraft noise, fuel venting, and exhaust emission requirements;

(2)

That materials and products conform to the specifications in the type design;

(3)

That parts of the products conform to the drawings in the type design; and

(4)

That the manufacturing processes, construction and assembly conform to those specified in the type design.

Referenced By

Interpretations of This Section (2)

  • Jones (JJASPP Engineering Services), 2015
  • Fournier (AviationDesigneeAssoc), 2012

Documents that cite this section, found in their catalog metadata or text. Listed by date, not by significance.

Reflects the eCFR edition current as of September 29, 2026. Retrieved from ecfr.gov on October 16, 2026.

Primary Source

  • Official Source (14 CFR · Part 21)