1.1 This practice provides an acceptable means of meeting the airworthiness requirements for the flight design loads and conditions of small normal category level 1 and 2 aeroplanes. The material was developed through open consensus of international experts in general aviation. This information was created by focusing on Normal Category aeroplanes. The content may be more broadly applicable; it is the responsibility of the applicant to substantiate broader applicability as a specific means of compliance. The topics covered within this practice are: Simplified Design Load Criteria, Acceptable Methods for Control Surface Loads Calculations, Acceptable Methods for Primary Control System Loads Calculations, and Control Surface Loading (Level 1 Aeroplanes).
Product Details
- Published:
- 03/15/2023
- Number of Pages:
- 12
- File Size:
- 1 file , 510 KB
- Redline File Size:
- 2 files , 810 KB
- Note:
- This product is unavailable in Russia, Ukraine, Belarus
