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14 CFR · Part 29

14 CFR § 29.29

Empty weight and corresponding center of gravity.

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Read in Subpart B
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
(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 rotorcraft 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 29)