Document Information
- Number
- 25.362-1
- Title
- Engine Failure Loads
- Status
- Active
- Date issued
- 2014-12-12
- Office of Primary Responsibility
- ANM-115, Transport Airplane Directorate
- Description
-
This advisory circular (AC) describes an acceptable means for showing compliance with the requirements of Title 14, Code of Federal Regulations (14 CFR) 25.362, Engine failure loads. Section 25.362 specifies the engine failure dynamic load conditions that apply to the engine mounts, pylons, and adjacent supporting airframe structure.
- Content
-
- AC 25.362-1 (PDF)