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14 CFR · Part 27

14 CFR § 27.999

Fuel system drains.

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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)

There must be at least one accessible drain at the lowest point in each fuel system to completely drain the system with the rotorcraft in any ground attitude to be expected in service.

(b)

Each drain required by paragraph (a) of this section must—

(1)

Discharge clear of all parts of the rotorcraft;

(2)

Have manual or automatic means to assure positive closure in the off position; and

(3)

Have a drain valve—

(i)

That is readily accessible and which can be easily opened and closed; and

(ii)

That is either located or protected to prevent fuel spillage in the event of a landing with landing gear retracted.

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)