Skip to Main Content
FlightPushFLIGHTPUSH
Part 29

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 29
  5. § 29.305
Loading
flightpush.co home

14 CFR · Part 29

14 CFR § 29.305

Strength and deformation.

← Previous SectionNext Section →
Read in Subpart C
Part 29 Contents
  • Subpart A: General
  • Subpart B: Flight
  • Subpart C: Strength Requirements
  • Subpart D: Design and Construction
  • Subpart E: Powerplant
  • Subpart F: Equipment
  • Subpart G: Operating Limitations and Information
  • Appendix A to Part 29: Instructions for Continued Airworthiness
  • Appendix B to Part 29: Airworthiness Criteria for Helicopter Instrument Flight
  • Appendix C to Part 29: Icing Certification
  • Appendix D to Part 29: Criteria for Demonstration of Emergency Evacuation Procedures Under § 29.803
  • Appendix E to Part 29: HIRF Environments and Equipment HIRF Test Levels
(a)

The structure must be able to support limit loads without detrimental or permanent deformation. At any load up to limit loads, the deformation may not interfere with safe operation.

(b)

The structure must be able to support ultimate loads without failure. This must be shown by—

(1)

Applying ultimate loads to the structure in a static test for at least three seconds; or

(2)

Dynamic tests simulating actual load application.

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 29)