# 14 CFR § 27.613: Material strength properties and design values

> Federal · Regulations · In force

URL: https://www.frixlaw.com/law-library/statutes/ecfr-14-27.613

## Section

- **Citation:** 14 CFR § 27.613
- **Heading:** Material strength properties and design values
- **Jurisdiction:** Federal
- **Kind:** Regulations
- **Status:** In force
- **Text as of:** September 22, 2026
- **Source:** Publisher's official text
- **Location:** Title 14—Aeronautics and Space > CHAPTER I—FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION > SUBCHAPTER C—AIRCRAFT > PART 27—AIRWORTHINESS STANDARDS: NORMAL CATEGORY ROTORCRAFT > Subpart D—Design and Construction > General

## Text

(a) Material strength properties must be based on enough tests of material meeting specifications to establish design values on a statistical basis.
(b) Design values must be chosen to minimize the probability of structural failure due to material variability. Except as provided in paragraphs (d) and (e) of this section, compliance with this paragraph must be shown by selecting design values that assure material strength with the following probability—
(1) Where applied loads are eventually distributed through a single member within an assembly, the failure of which would result in loss of structural integrity of the component, 99 percent probability with 95 percent confidence; and
(2) For redundant structure, those in which the failure of individual elements would result in applied loads being safely distributed to other load-carrying members, 90 percent probability with 95 percent confidence.
(c) The strength, detail design, and fabrication of the structure must minimize the probability of disastrous fatigue failure, particularly at points of stress concentration.
(d) Design values may be those contained in the following publications (available from the Naval Publications and Forms Center, 5801 Tabor Avenue, Philadelphia, Pennsylvania 19120) or other values approved by the Administrator:
(1) MIL-HDBK-5, “Metallic Materials and Elements for Flight Vehicle Structure”.
(2) MIL-HDBK-17, “Plastics for Flight Vehicles”.
(3) ANC-18, “Design of Wood Aircraft Structures”.
(4) MIL-HDBK-23, “Composite Construction for Flight Vehicles”.
(e) Other design values may be used if a selection of the material is made in which a specimen of each individual item is tested before use and it is determined that the actual strength properties of that particular item will equal or exceed those used in design.
(Secs. 313(a), 601, 603, 604, Federal Aviation Act of 1958 (49 U.S.C. 1354(a), 1421, 1423, 1424), sec. 6(c), Dept. of Transportation Act (49 U.S.C. 1655(c)))
[Doc. No. 5074, 29 FR 15695, Nov. 24, 1964, as amended by Amdt. 27-16, 43 FR 50599, Oct. 30, 1978; Amdt. 27-26, 55 FR 8000, Mar. 6, 1990]

## Nearby sections

- [14 CFR § 27.601 § 27.601 Design.](https://www.frixlaw.com/law-library/statutes/ecfr-14-27.601.md)
- [14 CFR § 27.602 § 27.602 Critical parts.](https://www.frixlaw.com/law-library/statutes/ecfr-14-27.602.md)
- [14 CFR § 27.603 § 27.603 Materials.](https://www.frixlaw.com/law-library/statutes/ecfr-14-27.603.md)
- [14 CFR § 27.605 § 27.605 Fabrication methods.](https://www.frixlaw.com/law-library/statutes/ecfr-14-27.605.md)
- [14 CFR § 27.607 § 27.607 Fasteners.](https://www.frixlaw.com/law-library/statutes/ecfr-14-27.607.md)
- [14 CFR § 27.609 § 27.609 Protection of structure.](https://www.frixlaw.com/law-library/statutes/ecfr-14-27.609.md)
- [14 CFR § 27.610 § 27.610 Lightning and static electricity protection.](https://www.frixlaw.com/law-library/statutes/ecfr-14-27.610.md)
- [14 CFR § 27.611 § 27.611 Inspection provisions.](https://www.frixlaw.com/law-library/statutes/ecfr-14-27.611.md)
- [14 CFR § 27.613 § 27.613 Material strength properties and design values.](https://www.frixlaw.com/law-library/statutes/ecfr-14-27.613.md)
- [14 CFR § 27.619 § 27.619 Special factors.](https://www.frixlaw.com/law-library/statutes/ecfr-14-27.619.md)
- [14 CFR § 27.621 § 27.621 Casting factors.](https://www.frixlaw.com/law-library/statutes/ecfr-14-27.621.md)
- [14 CFR § 27.623 § 27.623 Bearing factors.](https://www.frixlaw.com/law-library/statutes/ecfr-14-27.623.md)
- [14 CFR § 27.625 § 27.625 Fitting factors.](https://www.frixlaw.com/law-library/statutes/ecfr-14-27.625.md)
- [14 CFR § 27.629 § 27.629 Flutter.](https://www.frixlaw.com/law-library/statutes/ecfr-14-27.629.md)

---

Source: Frix Law Library, https://www.frixlaw.com/law-library/statutes/ecfr-14-27.613. Check the current official text before relying on it. Not legal advice.