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  4. Part 21
  5. § 21.95
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14 CFR · Part 21

14 CFR § 21.95

Approval of minor changes in type design.

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Read in Subpart D
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

Minor changes in a type design may be approved under a method acceptable to the FAA before submitting to the FAA any substantiating or descriptive data.

Referenced By

Interpretations of This Section (2)

  • New (Tennessee Aircraft Services), 2015
  • Hill (CarsonHelicopters), 2011

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)