Skip to Main Content
FlightPushFLIGHTPUSH
Part 21

Learn

Dashboard My Courses Mastery Map Practice Flight Bag

Resources

CFR & AIM FAA Orders Handbooks & Guides Certification Standards Pilot/Controller Glossary Advisory Circulars Legal Interpretations
Safety Center
Articles Trust Center
Help Center FAQ Status
  1. Reference Library
  2. CFR & AIM
  3. CFR
  4. Part 21
  5. § 21.213
Loading
flightpush.co home

14 CFR · Part 21

14 CFR § 21.213

Eligibility.

← Previous SectionNext Section →
Read in Subpart I
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)

A manufacturer who is a United States citizen may apply for a Class I or Class II provisional airworthiness certificate for aircraft manufactured by him within the U.S.

(b)

Any holder of an air carrier operating certificate under Part 121 of this chapter who is a United States citizen may apply for a Class II provisional airworthiness certificate for transport category aircraft that meet either of the following:

(1)

The aircraft has a current Class II provisional type certificate or an amendment thereto.

(2)

The aircraft has a current provisional amendment to a type certificate that was preceded by a corresponding Class II provisional type certificate.

(c)

An aircraft engine manufacturer who is a United States citizen and who has altered a type certificated aircraft by installing different type certificated engines, manufactured by him within the United States, may apply for a Class I provisional airworthiness certificate for that aircraft, if the basic aircraft, before alteration, was type certificated in the normal, utility, acrobatic, commuter, or transport category.

Regulations Referenced

14 CFR Part 121

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)