AIRFRAME GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

01-01-2007

Publisher

Federal Aviation Administration

- 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