FAA AC 23-19 : 2007
Current
The latest, up-to-date edition.
AIRFRAME GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES
Hardcopy , PDF
English
01-01-2007
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- 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.
| DevelopmentNote |
Supersedes FAA AC 23-3, FAA AC 23-4, FAA AC 23-5, FAA AC 23-6, FAA AC 23-7 and FAA AC 23-12 (03/2004)
|
| DocumentType |
Standard
|
| Pages |
91
|
| PublisherName |
Federal Aviation Administration
|
| Status |
Current
|
| FAA AC 23-13 : 2005 | FATIGUE, FAIL-SAFE, AND DAMAGE TOLERANCE EVALUATION OF METALLIC STRUCTURE FOR NORMAL, UTILITY, ACROBATIC, AND COMMUTER CATEGORY AIRPLANES |
| FAA AC 23-9 : 0 | EVALUATION OF FLIGHT LOADS ON SMALL AIRPLANES WITH T, V, +, OR Y EMPENNAGE CONFIGURATIONS |
| FAA AC 23-15 : 2003 | SMALL AIRPLANE CERTIFICATION COMPLIANCE PROGRAM |
| FAA 8110.4 : 2011 | TYPE CERTIFICATION |
| FAA AC 20-33 : 0 | TECHNICAL INFORMATION REGARDING CIVIL AERONAUTICS MANUALS 1, 3, 4A, 4B, 5, 6, 7, 8, 9, 13 AND 14 |
| FAA AC 20-44 : 0 | GLASS FIBER FABRIC FOR AIRCRAFT COVERING |
| FAA AC 21.25-1 : 0 | ISSUANCE OF TYPE CERTIFICATE: RESTRICTED CATEGORY AGRICULTURAL AIRPLANES |
| FAA AC 20-107 : 2009 | COMPOSITE AIRCRAFT STRUCTURE |
| FAA AC 25.571-1 : 2011 | DAMAGE TOLERANCE AND FATIGUE EVALUATION OF STRUCTURE |
| FAA 8100.5 : 2017 | AIRCRAFT CERTIFICATION SERVICE - ORGANIZATIONAL STRUCTURE AND FUNCTIONS |
| FAA AC 20-146 : 2003 | METHODOLOGY FOR DYNAMIC SEAT CERTIFICATION BY ANALYSIS FOR USE IN PARTS 23, 25, 27, AND 29 AIRPLANES AND ROTORCRAFT |
| FAA AC 23-20 : 2003 | ACCEPTANCE GUIDANCE ON MATERIAL PROCUREMENT AND PROCESS SPECIFICATIONS FOR POLYMER MATRIX COMPOSITE SYSTEMS |
| FAA AC 23.629-1 : 2004 | MEANS OF COMPLIANCE WITH TITLE 14 CFR, PART 23, SECTION 23.629, FLUTTER |
| FAA AC 23.562-1 : 0 | DYNAMIC TESTING OF PART 23 AIRPLANE SEAT/RESTRAINT SYSTEMS AND OCCUPANT PROTECTION |
| FAA AC 183.29-1 : 0 | DESIGNATED ENGINEERING REPRESENTATIVES CONSULTANT DIRECTORY |
| FAA AC 20-71 : 1970 | DUAL LOCKING DEVICES ON FASTENERS |
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