FAA AC 23-19 : A
NA
Status of Standard is Unknown
AIRFRAME GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES
12-01-2013
- SUBPART C - STRUCTURE
- GENERAL
- SPANWISE WING-LOADING METHODOLOGIES
- FLIGHT LOADS
- FLIGHT LOADS
- LIMIT ENGINE TORQUE DEFINITION
- CONTROL SURFACE AND SYSTEM LOADS
- CONTROL SYSTEM LOADS
- HORIZONTAL STABILIZING AND BALANCING SURFACES
- VERTICAL SURFACES
- AILERONS AND SPECIAL DEVICES
- GROUND LOADS
- WATER LOADS
- EMERGENCY LANDING CONDITIONS
- RELATIONAL VIEW OF TURNOVER PROTECTION
- FATIGUE EVALUATION
- SUBPART D - DESIGN AND CONSTRUCTION
- WINGS
- CONTROL SURFACES
- APPENDIX A TO PART 23 - Simplified Design Load Criteria
Gives information and guidance on an acceptable means, but not the only means, to comply with Title 14 of the Code of Federal Regulations (14 CFR) part 23, Subpart C, and portions of Subpart D.
| DocumentType |
Standard
|
| PublisherName |
Federal Aviation Administration
|
| Status |
NA
|
| Supersedes |
| FAA AC 23-24 : 2005 | AIRWORTHINESS COMPLIANCE CHECKLISTS FOR COMMON PART 23 SUPPLEMENTAL TYPE CERTIFICATE (STC) PROJECTS |
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