EVALUATION OF FLIGHT LOADS ON SMALL AIRPLANES WITH T, V, +, OR Y EMPENNAGE CONFIGURATIONS

Available format(s)

Hardcopy , PDF

Language(s)

English

Publisher

Federal Aviation Administration

1 PURPOSE
2 RELATED REGULATIONS
3 BACKGROUND
4 DEFINITIONS
5 ACCEPTABLE MEANS OF COMPLIANCE
APPENDIX 1

Gives information and guidance for an acceptable means, but not the only means, of demonstrating compliance with the requirements of Part 23 of the Federal Aviation Regulations (FAR) regarding evaluation of design flight loads for small airplanes with T, V, + or Y empennage configurations.

DocumentType	Standard
Pages	9
PublisherName	Federal Aviation Administration
Status	Current

FAA AC 23-24 : 2005	AIRWORTHINESS COMPLIANCE CHECKLISTS FOR COMMON PART 23 SUPPLEMENTAL TYPE CERTIFICATE (STC) PROJECTS
FAA AC 23-19 : 2007	AIRFRAME GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES