FAA AC 23-9 : 0
Current
The latest, up-to-date edition.
EVALUATION OF FLIGHT LOADS ON SMALL AIRPLANES WITH T, V, +, OR Y EMPENNAGE CONFIGURATIONS
Hardcopy , PDF
English
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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 |
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