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. § 29.908
Loading
flightpush.co home

14 CFR · Part 29

14 CFR § 29.908

Cooling fans.

← Previous SectionNext Section →
Read in Subpart E
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

For cooling fans that are a part of a powerplant installation the following apply:

(a)

Category A. For cooling fans installed in Category A rotorcraft, it must be shown that a fan blade failure will not prevent continued safe flight either because of damage caused by the failed blade or loss of cooling air.

(b)

Category B. For cooling fans installed in category B rotorcraft, there must be means to protect the rotorcraft and allow a safe landing if a fan blade fails. It must be shown that—

(1)

The fan blade would be contained in the case of a failure;

(2)

Each fan is located so that a fan blade failure will not jeopardize safety; or

(3)

Each fan blade can withstand an ultimate load of 1.5 times the centrifugal force expected in service, limited by either—

(i)

The highest rotational speeds achievable under uncontrolled conditions; or

(ii)

An overspeed limiting device.

(c)

Fatigue evaluation. Unless a fatigue evaluation under § 29.571 is conducted, it must be shown that cooling fan blades are not operating at resonant conditions within the operating limits of the rotorcraft.

Regulations Referenced

14 CFR 29.571

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)