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  5. § 27.625
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14 CFR · Part 27

14 CFR § 27.625

Fitting factors.

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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

For each fitting (part or terminal used to join one structural member to another) the following apply:

(a)

For each fitting whose strength is not proven by limit and ultimate load tests in which actual stress conditions are simulated in the fitting and surrounding structures, a fitting factor of at least 1.15 must be applied to each part of—

(1)

The fitting;

(2)

The means of attachment; and

(3)

The bearing on the joined members.

(b)

No fitting factor need be used—

(1)

For joints made under approved practices and based on comprehensive test data (such as continuous joints in metal plating, welded joints, and scarf joints in wood); and

(2)

With respect to any bearing surface for which a larger special factor is used.

(c)

For each integral fitting, the part must be treated as a fitting up to the point at which the section properties become typical of the member.

(d)

Each seat, berth, litter, safety belt, and harness attachment to the structure must be shown by analysis, tests, or both, to be able to withstand the inertia forces prescribed in § 27.561(b)(3) multiplied by a fitting factor of 1.33.

Regulations Referenced

14 CFR 27.561

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)