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  5. § 27.681
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14 CFR · Part 27

14 CFR § 27.681

Limit load static tests.

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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)

Compliance with the limit load requirements of this part must be shown by tests in which—

(1)

The direction of the test loads produces the most severe loading in the control system; and

(2)

Each fitting, pulley, and bracket used in attaching the system to the main structure is included.

(b)

Compliance must be shown (by analyses or individual load tests) with the special factor requirements for control system joints subject to angular motion.

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)