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. § 27.1091
Loading
flightpush.co home

14 CFR · Part 27

14 CFR § 27.1091

Air induction.

← 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 air induction system for each engine must supply the air required by that engine under the operating conditions and maneuvers for which certification is requested.

(b)

Each cold air induction system opening must be outside the cowling if backfire flames can emerge.

(c)

If fuel can accumulate in any air induction system, that system must have drains that discharge fuel—

(1)

Clear of the rotorcraft; and

(2)

Out of the path of exhaust flames.

(d)

For turbine engine powered rotorcraft—

(1)

There must be means to prevent hazardous quantities of fuel leakage or overflow from drains, vents, or other components of flammable fluid systems from entering the engine intake system; and

(2)

The air inlet ducts must be located or protected so as to minimize the ingestion of foreign matter during takeoff, landing, and taxiing.

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)