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  5. § 29.75
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14 CFR · Part 29

14 CFR § 29.75

Landing: General.

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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)

For each rotorcraft—

(1)

The corrected landing data must be determined for a smooth, dry, hard, and level surface;

(2)

The approach and landing must not require exceptional piloting skill or exceptionally favorable conditions; and

(3)

The landing must be made without excessive vertical acceleration or tendency to bounce, nose over, ground loop, porpoise, or water loop.

(b)

The landing data required by §§ 29.77, 29.79, 29.81, 29.83, and 29.85 must be determined—

(1)

At each weight, altitude, and temperature for which landing data are approved;

(2)

With each operating engine within approved operating limitations; and

(3)

With the most unfavorable center of gravity.

Regulations Referenced

14 CFR 29.7714 CFR 29.7914 CFR 29.8114 CFR 29.83

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)