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  5. § 27.29
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14 CFR · Part 27

14 CFR § 27.29

Empty weight and corresponding center of gravity.

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Read in Subpart B
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 empty weight and corresponding center of gravity must be determined by weighing the rotorcraft without the crew and payload, but with—

(1)

Fixed ballast;

(2)

Unusable fuel; and

(3)

Full operating fluids, including—

(i)

Oil;

(ii)

Hydraulic fluid; and

(iii)

Other fluids required for normal operation of roto-craft systems, except water intended for injection in the engines.

(b)

The condition of the rotorcraft at the time of determining empty weight must be one that is well defined and can be easily repeated, particularly with respect to the weights of fuel, oil, coolant, and installed equipment.

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)