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  5. § 27.675
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14 CFR · Part 27

14 CFR § 27.675

Stops.

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Read in Subpart D
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)

Each control system must have stops that positively limit the range of motion of the pilot's controls.

(b)

Each stop must be located in the system so that the range of travel of its control is not appreciably affected by—

(1)

Wear;

(2)

Slackness; or

(3)

Takeup adjustments.

(c)

Each stop must be able to withstand the loads corresponding to the design conditions for the system.

(d)

For each main rotor blade—

(1)

Stops that are appropriate to the blade design must be provided to limit travel of the blade about its hinge points; and

(2)

There must be means to keep the blade from hitting the droop stops during any operation other than starting and stopping the rotor.

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)