FAA AC 20-146 : 2003
Current
The latest, up-to-date edition.
METHODOLOGY FOR DYNAMIC SEAT CERTIFICATION BY ANALYSIS FOR USE IN PARTS 23, 25, 27, AND 29 AIRPLANES AND ROTORCRAFT
12-01-2013
1 PURPOSE
2 CANCELLATION
3 BACKGROUND
4 APPLICABILITY
5 RELATED PUBLICATIONS
6 DEFINITIONS
7 COMPUTER MODEL VALIDATION
8 APPLICATION OF COMPUTER MODELING IN SUPPORT OF DYNAMIC
TESTING
9 APPLICATION OF COMPUTER MODELING IN LIEU OF DYNAMIC
TESTING
10 SEAT CERTIFICATION AND COORDINATION PROCESS
11 DOCUMENTATION REQUIREMENTS FOR COMPLIANCE
APPENDIX 1 OCCUPANT TRAJECTORY AND HIC
APPENDIX 2 LOAD TIME HISTORIES
Gives guidance on how to validate the computer model and under what conditions the model may be used in support of certification or TSO approval/authorization.
| DocumentType |
Standard
|
| PublisherName |
Federal Aviation Administration
|
| Status |
Current
|
| FAA AC 23-24 : 2005 | AIRWORTHINESS COMPLIANCE CHECKLISTS FOR COMMON PART 23 SUPPLEMENTAL TYPE CERTIFICATE (STC) PROJECTS |
| FAA AC 23-19 : 2007 | AIRFRAME GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES |
| SAE ARP5765A | Analytical Methods for Aircraft Seat Design and Evaluation |
| FAA AC 27-1 : 2008 | CERTIFICATION OF NORMAL CATEGORY ROTORCRAFT |
| FAA 8110.4 : 2011 | TYPE CERTIFICATION |
| SAE AS8049C | Performance Standard for Seats in Civil Rotorcraft, Transport Aircraft, and General Aviation Aircraft |
| SAE J211/1_201403 | Instrumentation for Impact Test - Part 1 - Electronic Instrumentation |
| FAA AC 29-2 : 2008 | CERTIFICATION OF TRANSPORT CATEGORY ROTORCRAFT |
| FAA AC 23.562-1 : 0 | DYNAMIC TESTING OF PART 23 AIRPLANE SEAT/RESTRAINT SYSTEMS AND OCCUPANT PROTECTION |
| SAE J211/2_201406 | Instrumentation for Impact Test—Part 2: Photographic Instrumentation |
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