FAA AC 20-167 : 2016
Current
The latest, up-to-date edition.
AIRWORTHINESS APPROVAL OF ENHANCED VISION SYSTEM, SYNTHETIC VISION SYSTEM, COMBINED VISION SYSTEM, AND ENHANCED FLIGHT VISION SYSTEM EQUIPMENT
Hardcopy , PDF
English
01-01-2016
Chapter 1 - Introduction
Chapter 2 - Vision Systems Overview
Chapter 3 - Airworthiness Package Contents
Chapter 4 - System Criteria
Chapter 5 - Systems Installation Considerations
Chapter 6 - Performance Evaluation
Appendix A - FAA EFVS 14 CFR Compliance (Partial List)
Appendix B - EFVS Approach System and EFVS Landing
System Systems Safety Guidance
Appendix C - EFVS Approach System and II Safety Standards
Appendix D - Sample EFVS Approach System Flight Test Considerations
Appendix E - Sample Flight Test Considerations for EFVS Landing System
Appendix F - Sample Airplane Flight Manual (AFM) Supplement
Appendix G - Installation of Enhanced Vision System and or/Synthetic
Vision System on Rotorcraft
Appendix H - Additional Part 23 Considerations for Enhanced Vision
System/or Synthetic Vision System for Situation
Awareness Only
Appendix I - Definitions and Acronyms
Appendix J - Related Publications
Appendix K - Advisory Circular Feedback Information
Specifies guidance on airworthiness approval of enhanced vision system (EVS), synthetic vision system (SVS), combined vision system (CVS), and enhanced flight vision system (EFVS) equipment installation.
DevelopmentNote |
Supersedes FAA AC 23-26. (10/2010)
|
DocumentType |
Standard
|
Pages |
104
|
PublisherName |
Federal Aviation Administration
|
Status |
Current
|
FAA AC 23.1311-1 : 2011 | INSTALLATION OF ELECTRONIC DISPLAY IN PART 23 AIRPLANES |
SAE ARP 5677 : 2012 | HUMAN ENGINEERING CONSIDERATIONS FOR AIRBORNE IMPLEMENTATION OF ENHANCED SYNTHETIC VISION SYSTEMS |
FAA AC 20-181 : 2014 | AIRWORTHINESS APPROVAL OF ATTITUDE HEADING REFERENCE SYSTEM (AHRS) EQUIPMENT |
FAA AC 25-11 : 2014 | ELECTRONIC FLIGHT DISPLAYS |
FAA AC 90-106 : 2017 | ENHANCED FLIGHT VISION SYSTEMS |
SAE ARP 6467 : 2014 | HUMAN FACTORS MINIMUM REQUIREMENTS AND RECOMMENDATIONS FOR THE FLIGHT DECK DISPLAY OF DATA LINKED NOTICES TO AIRMEN (NOTAMS) |
FAA AC 20-185 : 2015 | AIRWORTHINESS APPROVAL OF SYNTHETIC VISION GUIDANCE SYSTEM |
FAA AC 20-138 : 2014 | AIRWORTHINESS APPROVAL OF POSITIONING AND NAVIGATION SYSTEMS |
FAA AC 27-1 : 2008 | CERTIFICATION OF NORMAL CATEGORY ROTORCRAFT |
RTCA DO 200B : 2015 | STANDARDS FOR PROCESSING AERONAUTICAL DATA |
FAA AC 23.1311-1 : 2011 | INSTALLATION OF ELECTRONIC DISPLAY IN PART 23 AIRPLANES |
FAA AC 25.629-1 : 2014 | AEROELASTIC STABILITY SUBSTANTIATION OF TRANSPORT CATEGORY AIRPLANES |
RTCA DO 178 : C2011 | SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION |
FAA AC 25-11 : 2014 | ELECTRONIC FLIGHT DISPLAYS |
FAA AC 25.1329-1 : 2016 | APPROVAL OF FLIGHT GUIDANCE SYSTEMS |
FAA AC 90-106 : 2017 | ENHANCED FLIGHT VISION SYSTEMS |
FAA 8110.4 : 2011 | TYPE CERTIFICATION |
SAE ARP 4754 : 2010 | GUIDELINES FOR DEVELOPMENT OF CIVIL AIRCRAFT AND SYSTEMS |
FAA AC 25-23 : 0 | AIRWORTHINESS CRITERIA FOR THE INSTALLATION APPROVAL OF A TERRAIN AWARENESS AND WARNING SYSTEM (TAWS) FOR PART 25 AIRPLANES |
RTCA DO 254 : 2000 | DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE |
SAE ARP 5589 : 2005 | HUMAN ENGINEERING CONSIDERATIONS FOR DESIGN AND IMPLEMENTATION OF PERSPECTIVE FLIGHT GUIDANCE DISPLAYS |
SAE ARP 4761 : 1996 | GUIDELINES AND METHODS FOR CONDUCTION THE SAFETY ASSESSMENT PROCESS ON CIVIL AIRBORNE SYSTEMS AND EQUIPMENT |
FAA AC 120-57 : 0 | SURFACE MOVEMENT GUIDANCE AND CONTROL SYSTEM |
SAE ARP 4101 : 1988 | FLIGHT DECK LAYOUT AND FACILITIES |
FAA AC 23-18 : 0 | INSTALLATION OF TERRAIN AWARENESS AND WARNING SYSTEM (TAWS) APPROVED FOR PART 23 AIRPLANES |
FAA AC 25.1523-1 : 0 | MINIMUM FLIGHTCREW |
FAA AC 25.571-1 : 2011 | DAMAGE TOLERANCE AND FATIGUE EVALUATION OF STRUCTURE |
SAE ARP 4105 : 2012 | ABBREVIATIONS, ACRONYMS, AND TERMS FOR USE ON THE FLIGHT DECK |
RTCA DO 309 : 2008 | MINIMUM OPERATIONAL PERFORMANCE STANDARDS (MOPS) FOR HELICOPTER TERRAIN AWARENESS AND WARNING SYSTEM (HTAWS) AIRBORNE EQUIPMENT |
FAA AC 23.1309-1 : 2011 | SYSTEM SAFETY ANALYSIS AND ASSESSMENT FOR PART 23 AIRPLANES |
FAA AC 120-76 : 2017 | AUTHORIZATION FOR USE OF ELECTRONIC FLIGHT BAGS |
SAE AS 8055A : 2015 | MINIMUM PERFORMANCE STANDARD FOR AIRBORNE HEAD UP DISPLAY (HUD) |
FAA AC 120-29 : 0 | CRITERIA FOR APPROVAL OF CATEGORY 1 AND CATEGORY 2 WEATHER MINIMA FOR APPROACH |
RTCA DO 276 : C2015 | USER REQUIREMENTS FOR TERRAIN AND OBSTACLE DATA |
FAA AC 29-2 : 2008 | CERTIFICATION OF TRANSPORT CATEGORY ROTORCRAFT |
FAA AC 25.1309-1 : 0 | SYSTEM DESIGN AND ANALYSIS |
SAE ARP 5288 : 2001 | TRANSPORT CATEGORY AIRPLANE HEAD UP DISPLAY (HUD) SYSTEMS |
RTCA DO 315 : B2011 | MINIMUM AVIATION SYSTEM PERFORMANCE STANDARDS (MASPS) FOR ENHANCED VISION SYSTEMS, SYNTHETIC VISION SYSTEMS, COMBINED VISION SYSTEMS AND ENHANCED FLIGHT VISION SYSTEMS |
FAA 8110.54 : 2010 | INSTRUCTIONS FOR CONTINUED AIRWORTHINESS RESPONSIBILITIES, REQUIREMENTS, AND CONTENTS |
SAE AS 8034 : 2011 | MINIMUM PERFORMANCE STANDARD FOR AIRBORNE MULTIPURPOSE ELECTRONIC DISPLAYS |
SAE ARP 4102 : 1988 | FLIGHT DECK PANELS, CONTROLS, AND DISPLAYS |
SAE ARP 5677 : 2012 | HUMAN ENGINEERING CONSIDERATIONS FOR AIRBORNE IMPLEMENTATION OF ENHANCED SYNTHETIC VISION SYSTEMS |
SAE ARP 4103 : 2014 | FLIGHT DECK LIGHTING FOR COMMERCIAL TRANSPORT AIRCRAFT |
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