Document Information
- Number
- 23-13A
- Title
- Fatigue, Fail-Safe, and Damage Tolerance Evaluation of Metallic Structure for Normal, Utility, Acrobatic, and Commuter Category Airplanes
- Status
- Active
- Date issued
- 2005-09-29
- Office of Primary Responsibility
- ACE-100, Small Airplane Directorate
- Description
- Provides information and guidance concerning an acceptable means of demonstrating compliance with the requirements of Part 23 of the Federal Aviation Regulations (FAR) regarding fatigue and fail-safe evaluation of metallic airplane structure.
- Content
-
- AC 23-13A (PDF)
- Cancels
-
Cancels Number Title Date 23-13 Fatigue and Fail-Safe Evaluation of Flight Structure and Pressurized Cabin for Part 23 Airplanes Provides information and guidance concerning an acceptable means of demonstrating compliance with the requirements of Part 23 of the Federal Aviation Regulations (FAR) regarding fatigue and fail-safe evaluation of metallic airplane structure. 1993-04-15