FAA AC 23.1311-1 : 2011
Current
Current
The latest, up-to-date edition.
INSTALLATION OF ELECTRONIC DISPLAY IN PART 23 AIRPLANES
Available format(s)
Hardcopy , PDF
Language(s)
English
Published date
01-01-2011
Publisher
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1.0 Purpose
2.0 Cancellation
3.0 Related Regulations and Documents
4.0 Background
5.0 Scope
6.0 Acronyms/Definitions
7.0 Display Description
8.0 Flight Displays
9.0 Powerplant Displays
10.0 Electronic Displays for Navigation Information
11.0 Aircraft Flight Manual (AFM)
12.0 Electronic Checklist and Charts
13.0 General Human Factors Considerations for
Design of Electronic Displays
14.0 Location and Configuration of Displays
15.0 Pilot Field-of-View Considerations
16.0 Luminance
17.0 Symbology and Format
18.0 Annunciation
19.0 Lag Time and Data Update
20.0 Controls
21.0 Test Functions
22.0 Color Standardization
23.0 General Installation Requirements
24.0 Aircraft Electrical Power Source
25.0 Safety Assessments
26.0 Software and Hardware Development Assurance
27.0 Environmental Conditions
28.0 Electromagnetic Protection
29.0 Electromagnetic Interference
30.0 Implosion Protection
31.0 Configuration Management by Electronic
Identification Guidance
Specifies guidance for showing compliance with certain requirements of Title 14, Code of Federal Regulations (CFR), part 23, as well as general guidance for the design, installation, integration, and approval of electronic flight deck displays, components, and systems installed in part 23 category airplanes.
| DocumentType |
Standard
|
| Pages |
57
|
| PublisherName |
Federal Aviation Administration
|
| Status |
Current
|
| FAA AC 23-15 : 2003 | SMALL AIRPLANE CERTIFICATION COMPLIANCE PROGRAM |
| FAA AC 20-170 : 2013 | INTEGRATED MODULAR AVIONICS DEVELOPMENT, VERIFICATION, INTEGRATION, AND APPROVAL USING RTCA/DO-297 AND TECHNICAL STANDARD ORDER-C153 |
| FAA N 8110.98 : 2002 | ADDRESSING HUMAN FACTORS/PILOT INTERFACE ISSUES OF COMPLEX, INTEGRATED AVIONICS AS PART OF THE TECHNICAL STANDARD ORDER (TSO) PROCESS |
| FAA AC 23-24 : 2005 | AIRWORTHINESS COMPLIANCE CHECKLISTS FOR COMMON PART 23 SUPPLEMENTAL TYPE CERTIFICATE (STC) PROJECTS |
| SAE ARP5589 | Human Engineering Considerations for Design and Implementation of Perspective Flight Guidance Displays |
| SAE ARP4032B | Human Engineering Considerations in the Application of Color to Electronic Aircraft Displays |
| SAE AS5498A | Minimum Operational Performance Specification for Inflight Icing Detection Systems |
| SAE ARP5677 | 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 20-173 : 2011 | INSTALLATION OF ELECTRONIC FLIGHT BAG COMPONENTS |
| SAE AS8055A | Minimum Performance Standard for Airborne Head Up Display (HUD) |
| MIL-HDBK-516 Revision C:2014 | AIRWORTHINESS CERTIFICATION CRITERIA |
| FAA AC 23-16 : 0 | POWERPLANT GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES AND AIRSHIPS |
| SAE ARP6467 | Human Factors Minimum Requirements and Recommendations for the Flight Deck Display of Data Linked Notices to Airmen (NOTAMs) |
| FAA AC 120-86 : 2005 | AIRCRAFT SURVEILLANCE SYSTEMS AND APPLICATIONS |
| FAA AC 20-167 : 2016 | AIRWORTHINESS APPROVAL OF ENHANCED VISION SYSTEM, SYNTHETIC VISION SYSTEM, COMBINED VISION SYSTEM, AND ENHANCED FLIGHT VISION SYSTEM EQUIPMENT |
| FAA AC 20-161 : 2008 | AIRCRAFT ONBOARD WEIGHT AND BALANCE SYSTEMS |
| FAA AC 20-182 : 2016 | AIRWORTHINESS APPROVAL FOR AIRCRAFT WEATHER RADAR SYSTEMS |
| SAE ARP5119 | Location of and Display Symbology Requirements for Head-Down Electronic Flight Displays for Steep IMC Approaches |
| SAE ARP5740 | Cockpit Display of Data Linked Weather Information |
| FAA AC 120-76 : 2017 | AUTHORIZATION FOR USE OF ELECTRONIC FLIGHT BAGS |
| SAE ARP5430 | Human Interface Criteria for Vertical Situation Awareness Displays |
| SAE AIR5924A | Guidelines for the Integration of Electronic Engine Control Systems for Transport Category (Part 25) and General Aviation (Part 23) Aircraft |
| FAA AC 23-21 : 2004 | AIRWORTHINESS COMPLIANCE CHECKLISTS USED TO SUBSTANTIATE MAJOR ALTERATIONS FOR SMALL AIRPLANES |
| FAA AC 23.1523 : 2005 | MINIMUM FLIGHT CREW |
| FAA AC 20-185 : 2015 | AIRWORTHINESS APPROVAL OF SYNTHETIC VISION GUIDANCE SYSTEM |
| FAA AC 23.1309-1 : 2011 | SYSTEM SAFETY ANALYSIS AND ASSESSMENT FOR PART 23 AIRPLANES |
| FAA AC 20-138 : 2014 | AIRWORTHINESS APPROVAL OF POSITIONING AND NAVIGATION SYSTEMS |
| FAA AC 20-150 : 2014 | AIRWORTHINESS APPROVAL OF SATELLITE VOICE (SATVOICE) EQUIPMENT SUPPORTING AIR TRAFFIC SERVICE (ATS) COMMUNICATION |
| FAA AC 20-172 : 2015 | AIRWORTHINESS APPROVAL FOR ADS-B IN SYSTEMS AND APPLICATIONS |
| FAA AC 20-149 : 2015 | INSTALLATION GUIDANCE FOR DOMESTIC FLIGHT INFORMATION SERVICE - BROADCAST |
| FAA AC 20-145 : 2003 | GUIDANCE FOR INTEGRATED MODULAR AVIONICS (IMA) THAT IMPLEMENT TSO-C153 AUTHORIZED HARDWARE ELEMENTS |
| SAE ARP6023 | Human Engineering Considerations for Implementing Enhanced Synthetic Vision Systems in Vertical Flight Capable Platforms |
| SAE ARP1161A | Crew Station Lighting - Commercial Aircraft |
| SAE ARP 4260 : 2014 | PHOTOMETRIC AND COLORIMETRIC MEASUREMENT PROCEDURES FOR AIRBORNE ELECTRONIC FLAT PANEL DISPLAYS |
| RTCA DO 200B : 2015 | STANDARDS FOR PROCESSING AERONAUTICAL DATA |
| FAA AC 20-140 : 2016 | GUIDELINES FOR DESIGN APPROVAL OF AIRCRAFT DATA LINK COMMUNICATION SYSTEMS SUPPORTING AIR TRAFFIC SERVICES (ATS) |
| FAA AC 20-170 : 2010 | INTEGRATED MODULAR AVIONICS DEVELOPMENT, VERIFICATION, INTEGRATION, AND APPROVAL USING RTCA/DO-297 AND TECHNICAL STANDARD ORDER-C153 |
| FAA AC 21-16 : 2011 | RTCA DOCUMENT DO-160 VERSIONS D, E, F, AND G, "ENVIRONMENTAL CONDITIONS AND TEST PROCEDURES FOR AIRBORNE EQUIPMENT" |
| SAE ARP926B | FAULT/FAILURE ANALYSIS PROCEDURE |
| RTCA DO 178 : C2011 | SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION |
| FAA AC 20-88 : A | GUIDELINES ON THE MARKING OF AIRCRAFT POWERPLANT INSTRUMENTS (DISPLAYS) |
| RTCA DO-201A : 2000 | STANDARDS FOR AERONAUTICAL INFORMATION |
| FAA AC 20-149 : 2015 | INSTALLATION GUIDANCE FOR DOMESTIC FLIGHT INFORMATION SERVICE - BROADCAST |
| SAE ARP 268 : 1994 | LOCATION AND ACTUATION OF FLIGHT DECK CONTROLS FOR TRANSPORT |
| SAE ARP 5365 : 1999 | HUMAN INTERFACE CRITERIA FOR COCKPIT DISPLAY OF TRAFFIC INFORMATION |
| FAA AC 23-15 : 2003 | SMALL AIRPLANE CERTIFICATION COMPLIANCE PROGRAM |
| FAA AC 91-78 : 2007 | USE OF CLASS 1 OR CLASS 2 ELECTRONIC FLIGHT BAG (EFB) |
| FAA AC 25-11 : 2014 | ELECTRONIC FLIGHT DISPLAYS |
| FAA AC 20-136 : 2011 | AIRCRAFT ELECTRICAL AND ELECTRONIC SYSTEM LIGHTNING PROTECTION |
| SAE ARP 4067 : 1989 | DESIGN OBJECTIVES FOR CRT DISPLAYS FOR PART 23 AIRCRAFT |
| FAA 8110.105 : 2017 | SIMPLE AND COMPLEX ELECTRONIC HARDWARE APPROVAL GUIDANCE |
| FAA AC 90-106 : 2017 | ENHANCED FLIGHT VISION SYSTEMS |
| SAE ARP4754A | Guidelines for Development of Civil Aircraft and Systems |
| FAA AC 20-167 : 2016 | AIRWORTHINESS APPROVAL OF ENHANCED VISION SYSTEM, SYNTHETIC VISION SYSTEM, COMBINED VISION SYSTEM, AND ENHANCED FLIGHT VISION SYSTEM EQUIPMENT |
| FAA AC 20-158 : 2014 | THE CERTIFICATION OF AIRCRAFT ELECTRICAL AND ELECTRONIC SYSTEMS FOR OPERATION IN THE HIGH-INTENSITY RADIATED FIELDS (HIRF) ENVIRONMENT |
| SAE ARP4032B | Human Engineering Considerations in the Application of Color to Electronic Aircraft Displays |
| FAA 8110.49 : 2011 | SOFTWARE APPROVAL GUIDELINES |
| RTCA DO 254 : 2000 | DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE |
| FAA AC 20-152 : 2005 | RTCA, INC., DOCUMENT RTCA/DO-254, DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE |
| SAE ARP 450 : 1994 | FLIGHT DECK VISUAL, AUDIBLE, AND TACTILE SIGNALS |
| FAA AC 23-8 : 2011 | FLIGHT TEST GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES |
| FAA AC 20-153 : 2016 | ACCEPTANCE OF AERONAUTICAL DATA PROCESSES AND ASSOCIATED DATABASES |
| SAE ARP4761 | GUIDELINES AND METHODS FOR CONDUCTING THE SAFETY ASSESSMENT PROCESS ON CIVIL AIRBORNE SYSTEMS AND EQUIPMENT |
| RTCA DO 267 : A2004 | MINIMUM AVIATION SYSTEM PERFORMANCE STANDARDS (MASPS) FOR FLIGHT INFORMATION SERVICES-BROADCAST (FIS-B) DATA LINK |
| FAA AC 91-75 : 2003 | ATTITUDE INDICATOR |
| 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 |
| SAE ARP 4105 : 2012 | ABBREVIATIONS, ACRONYMS, AND TERMS FOR USE ON THE FLIGHT DECK |
| SAE ARP1834A | FAULT/FAILURE ANALYSISFor Digital Systems and Equipment |
| SAE ARP 4155 : 1997 | HUMAN INTERFACE DESIGN METHODOLOGY FOR INTEGRATED DISPLAY SYMBOLOGY |
| SAE ARP 5287 : 1999 | OPTICAL MEASUREMENT PROCEDURES FOR AIRBORNE HEAD UP DISPLAY (HUD) |
| 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 AS8055A | Minimum Performance Standard for Airborne Head Up Display (HUD) |
| SAE AIR1093A | Numeral, Letter and Symbol Dimensions for Aircraft Instrument Displays |
| SAE ARP 4033 : 1995 | PILOT-SYSTEM INTEGRATION |
| FAA AC 23-22 : 2005 | GUIDANCE FOR APPROVED MODEL LIST (AML) SUPPLEMENTAL TYPE CERTIFICATE (STC) APPROVAL OF PART 23 AIRPLANE AVIONICS INSTALLATIONS |
| SAE ARP5364 | Human Factor Considerations in the Design of Multifunction Display Systems for Civil Aircraft |
| SAE ARP5430 | Human Interface Criteria for Vertical Situation Awareness Displays |
| FAA AC 120-64 : 0 | OPERATIONAL USE AND MODIFICATION OF ELECTRONIC CHECKLISTS |
| FAA AC 23-17 : 2011 | SYSTEMS AND EQUIPMENT GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES AND AIRSHIPS |
| RTCA DO 187 : 1984 | MINIMUM OPERATIONAL PERFORMANCE STANDARDS FOR AIRBORNE AREA NAVIGATION EQUIPMENT USING MULTI-SENSOR INPUTS |
| FAA AC 20-155 : 2013 | INDUSTRY DOCUMENTS TO SUPPORT AIRCRAFT LIGHTNING PROTECTION CERTIFICATION |
| SAE ARP 1874 : 1988 | DESIGN OBJECTIVES FOR CRT DISPLAYS FOR PART 25 (TRANSPORT) AIRCRAFT |
| SAE ARP 5288 : 2001 | TRANSPORT CATEGORY AIRPLANE HEAD UP DISPLAY (HUD) SYSTEMS |
| SAE ARP5289A | Electronic Aeronautical Symbols |
| FAA AC 20-138 : 2014 | AIRWORTHINESS APPROVAL OF POSITIONING AND NAVIGATION SYSTEMS |
| FAA AC 20-115 : 2017 | AIRBORNE SOFTWARE DEVELOPMENT ASSURANCE USING EUROCAE ED-12( ) AND RTCA DO-178( ) |
| SAE ARP 4102/7 : 1988 | ELECTRONIC DISPLAYS |
| 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 |
| RTCA DO 313 : 2008 | CERTIFICATION GUIDANCE FOR INSTALLATION OF NON-ESSENTIAL, NON-REQUIRED AIRCRAFT CABIN SYSTEMS AND EQUIPMENT |
| SAE AS8034B | Minimum Performance Standard for Airborne Multipurpose Electronic Displays |
| FAA AC 23-23 : 2004 | STANDARDIZATION GUIDE FOR INTEGRATED COCKPITS IN PART 23 AIRPLANES |
| SAE ARP 4256 : 2001 | DESIGN OBJECTIVES FOR LIQUID CRYSTAL DISPLAYS FOR PART 25 (TRANSPORT) AIRCRAFT |
| SAE ARP 4102 : 1988 | FLIGHT DECK PANELS, CONTROLS, AND DISPLAYS |
| SAE ARP1782B | Photometric and Colorimetric Measurement Procedures for Airborne Direct View CRT Displays |
| RTCA DO 297 : 2005 | Integrated Modular Avionics (IMA) Development Guidance and Certification Considerations<br> |
| SAE ARP5677 | 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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