Name: FAA AC 23-19 : A
Brand: FAA

AIRFRAME GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES

Published date

12-01-2013

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.

DocumentType	Standard
PublisherName	Federal Aviation Administration
Status	NA
Supersedes	FAA AC 23-12 : 1993 FAA AC 23-6 : 1986 FAA AC 23-5 : 1986 FAA AC 23-3 : 1985 FAA AC 23-7 : 1987 FAA AC 23-4 : 1986

FAA AC 23-24 : 2005

AIRWORTHINESS COMPLIANCE CHECKLISTS FOR COMMON PART 23 SUPPLEMENTAL TYPE CERTIFICATE (STC) PROJECTS

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FAA AC 23-19 : A

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Abstract

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Standards Referenced By This Book

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