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FAA AC 23-19 : 2007

Current

Current

The latest, up-to-date edition.

AIRFRAME GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

01-01-2007

€53.84
Excluding VAT

- 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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