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  5. § 27.1013
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14 CFR · Part 27

14 CFR § 27.1013

Oil tanks.

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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

Each oil tank must be designed and installed so that—

(a)

It can withstand, without failure, each vibration, inertia, fluid, and structural load expected in operation;

(b)

[Reserved]

(c)

Where used with a reciprocating engine, it has an expansion space of not less than the greater of 10 percent of the tank capacity or 0.5 gallon, and where used with a turbine engine, it has an expansion space of not less than 10 percent of the tank capacity.

(d)

It is impossible to fill the tank expansion space inadvertently with the rotorcraft in the normal ground attitude;

(e)

Adequate venting is provided; and

(f)

There are means in the filler opening to prevent oil overflow from entering the oil tank compartment.

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)