AC 20-167B Appendix G APPENDIX G. R ELATED MATERIAL G.1 Title 14, Code of Federal Regulations.
The following 14 CFR regulations are related to this AC. You can download the full text of these regulations from the Federal Register website at www.ecfr.gov.
• Part 1, Definitions and Abbreviations.
• Part 23, Airworthiness Standards: Normal Category Airplanes.
• Part 25, Airworthiness Standards: Transport Category Airplanes.
• Part 27, Airworthiness Standards: Normal Category Rotorcraft.
• Part 29, Airworthiness Standards: Transport Category Rotorcraft.
• Part 91, General Operating and Flight Rules.
G.2 FAA Advisory Circular(s).
The following publications are related to the guidance in this AC. You should refer to the latest version for guidance, which is available on the Dynamic Regulatory System (DRS) website at drs.faa.gov/browse.
• AC 20-185A, Airworthiness Approval of Synthetic Vision Systems, Synthetic Vision Guidance Systems, and Aircraft State Awareness Synthetic Vision Systems.
• AC 21-16G, RTCA Document DO-160 versions D, E, F,G “Environmental Conditions and Test Procedures for Airborne Equipment.”
• AC 23-18, Installation of Terrain Awareness and Warning System (TAWS) Approved for Part 23 Airplanes.
• AC 23.1309-1E, System Safety Analysis and Assessment for Part 23 Airplanes.
• AC 23.1311-1C, Installation of Electronic Display in Part 23 Airplanes.
• AC 25-11B, Electronic Flight Displays.
• AC 25-23, Airworthiness Criteria for the Installation Approval of a Terrain Awareness and Warning System (TAWS) for Part 25 Airplanes.
• AC 25.571-1D, Damage Tolerance and Fatigue Evaluation of Structure.
• AC 25.1309-1B, System Design and Analysis.
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AC 20-167B Appendix G
• AC 25.1329-1C, Approval of Flight Guidance Systems.
• AC 25.1322-1, Flightcrew Alerting.
• AC 25.1523-1, Minimum Flightcrew.
• AC 27-1B CHG 1-9, Certification of Normal Category Rotorcraft.
• AC 29-2C CHG 9, Certification of Transport Category Rotorcraft.
• AC 90-106B, Enhanced Flight Vision Systems.
• AC 120-29A, Criteria for Approval of Category I and Category II Weather Minima for Approach.
• AC 120-57C, Surface Movement Guidance and Control System.
• AC 120-62, Takeoff Safety Training Aid.
• AC 120-76E, Authorization for Use of Electronic Flight Bags.
• Order 8110.4C CHG 7, Type Certification.
• Order 8110.54A, Instructions for Continued Airworthiness Responsibilities, Requirements, and Contents.
• Order 8900.1A, Flight Standards Information Management.
G.3 Society of Automotive Engineers (SAE) International.
The following SAE Aerospace Recommended Practice (ARP) and Aerospace Standard (AS) documents are related to the guidance in this AC. Unless otherwise specified, use the latest FAA-accepted revision for guidance. If the document is revised after publication of this AC, you should verify that the FAA accepts the subsequent revision or update as an acceptable form of guidance. The documents are available online at:
www.sae.org.
• ARP4101, Flight Deck Layout and Facilities.
• ARP4102, Flight Deck Panels, Controls and Displays.
• ARP4103A, Flight Deck Lighting for Commercial Transport Aircraft.
• ARP4105C, Abbreviations, Acronyms, and Terms for Use on the Flight Deck.
• ARP4754B, Guidelines for Development of Civil Aircraft and Systems.
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AC 20-167B Appendix G
• ARP4761A, Guidelines and Methods for Conducting the Safety Assessment Process on Civil Airborne Systems and Equipment.
• ARP5287, Optical Measurement Procedures for Airborne Head Up Display (HUD).
• ARP5288, Transport Category Airplane Head Up Display (HUD) Systems.
• ARP5589, Human Engineering Considerations for Design and Implementation of Perspective Flight Guidance Displays.
• ARP5677, Human Engineering Considerations for Airborne Implementation of Enhanced Synthetic Vision Systems.
• AS8034C, Minimum Performance Standard for Airborne Multipurpose Electronic Displays.
• AS8055A, Minimum Performance Standard for Airborne Head Up Display (HUD).
G.4 ASTM Consensus Standard(s).
ASTM F3117M-24a, Standard Specification for Crew Interface in Aircraft is related to the guidance in this AC. FAA-accepted consensus standards, including any required changes for acceptance, are available online at faa.gov.
G.5 RTCA.
The following RTCA (formerly Radio Technical Commission for Aeronautics) document is related to the guidance in this AC. Unless otherwise specified, use the latest FAA-accepted revision for guidance. If the document is revised after publication of this AC, you should verify that the FAA accepts the subsequent revision or update as an acceptable form of guidance. This document can be ordered online at rtca.org.
• DO-160G, Environmental Conditions and Test Procedures for Airborne Equipment.
• DO-178C, Software Considerations in Airborne Systems and Equipment Certification.
• DO-200, Standards for Processing Aeronautical Data.
• DO-254, Design Assurance Guidance for Airborne Electronic Hardware.
• DO-276B, User Requirements for Terrain and Obstacle Data.
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AC 20-167B Appendix G
• DO-309, Minimum Operational Performance Standards (MOPS) for Helicopter Terrain Awareness and Warning System (HTAWS) Airborne Equipment.
• DO-315A, Minimum Aviation System Performance Standards (MASPS) for Enhanced Vision Systems, Synthetic Vision Systems, Combined Vision Systems, and Enhanced Flight Vision Systems.
• DO-390/EUROCAE 291, Test Procedures for Quantitative Visual Advantage.
G.6 Other Documents.
MIL-STD-1787D, Aircraft Display Symbology is related to the guidance in this AC.
This document can be purchased online at quicksearch.dla.mil/.
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If you find an error in this Advisory Ci rcular, have recommendations for improving it, or have suggestions for new items/subjects to be added, you may let us know by emailing this form to 9-AWA- AVS.AIR.DMO@faa.gov or faxing it to the attention of the N/A at N/A.
Subject: AC 20-167B, Airworthiness Approval of Enhanced Vision System, Enhanced Flight Vision Date:
System, and Combined Vision System Equipment Mark all appropriate line items:
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