Skip to Main Content
FlightPushFLIGHTPUSH
Part 27

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 27
  5. § 27.931
Loading
flightpush.co home

14 CFR · Part 27

14 CFR § 27.931

Shafting critical speed.

← Previous SectionNext Section →
Read in Subpart E
Part 27 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 27: Instructions for Continued Airworthiness
  • Appendix B to Part 27: Airworthiness Criteria for Helicopter Instrument Flight
  • Appendix C to Part 27: Criteria for Category A
  • Appendix D to Part 27: HIRF Environments and Equipment HIRF Test Levels
(a)

The critical speeds of any shafting must be determined by demonstration except that analytical methods may be used if reliable methods of analysis are available for the particular design.

(b)

If any critical speed lies within, or close to, the operating ranges for idling, power on, and autorotative conditions, the stresses occurring at that speed must be within safe limits. This must be shown by tests.

(c)

If analytical methods are used and show that no critical speed lies within the permissible operating ranges, the margins between the calculated critical speeds and the limits of the allowable operating ranges must be adequate to allow for possible variations between the computed and actual values.

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 27)