Establishes an acceptable means, but not the only means, of obtaining airworthiness approval of a multi-sensor navigation or flight management systems integrating data from multiple navigation sensors for use as a navigation system for oceanic and remote, domestic enroute, terminal, and non-precision instrument approach (except localizer, localizer directional aid (LDA) and simplified directional facility operations.

This advisory circular (AC) establishes an acceptable means, but not the only means, of obtaining airworthiness approval of Global Positioning System (GPS) equipment for use as a supplemental navigation system for oceanic and remote, domestic en route, terminal, and non-precision instrument approach [except localizer, localizer directional aid (LDA) and simplified directional facility (SDF)] operations.

This advisory circular (AC) supports the introduction and the use of flight information Service Broadcast (FIS-B) weather and other aeronautical data link products for enhanced situational awareness.

This advisory circular (AC) provides applicants guidance for obtaining an airworthiness approval for traffic alert collision avoidance systems (TCAS II).

This advisory circular (AC) identifies RTCA, Inc., document DO-307, Aircraft Design and Certification for Portable Electronic Device (PED) Tolerance, dated October 11, 2007, and RTCA/DO-307, Change 1, dated December 16, 2008, as an acceptable means for designing and demonstrating aircraft tolerance to potential electromagnetic interference from portable electronic devices (PEDs).

This advisory circular (AC) provides guidance material for the airworthiness approval of installed positioning and navigation equipment.

This advisory circular (AC) provides guidance on airworthiness approval for designers, manufacturers, and installers of satellite voice equipment supportingair traffic service (ATS).

This AC will help you to:

(1) Obtain a Letter of Acceptance (LOA) from the Federal Aviation Administration (FAA) that acknowledges compliance with this AC regarding aeronautical data processing.

This Advisory Circular (AC) provides guidance for the installation and airworthiness approval of Automatic Dependent Surveillance – Broadcast (ADS-B) Out systems in aircraft.

This AC provides airworthiness requirements for aircraft with an installed data link system intended to support air traffic services.

a. This advisory circular (AC) will provide you with information and guidance on how to show compliance with Title 14, Code of Federal Regulations (14 CFR) 23.1308, 25.1317, 27.1317, and 29.1317, High-intensity Radiated Fields (HIRF) Protection.

a. This advisory circular (AC) provides guidance for the initial and follow-on airworthiness approval of aircraft weather radar systems meeting the latest revision of the Technical Standard Order (TSO)-C63, Airborne Weather Radar Equipment.

This advisory circular (AC) provides guidance for gaining airworthiness approval for enhanced and synthetic vision systems in aircraft.

Calls attention to RTCA, Inc., (formerly the Radio Technical Commission for Aeronautics) Document RTCA/DO- 178B, “Software Considerations in Airborne Systems and Equipment Certification,” issued December 1992.

Establishes an acceptable means, but not the only means, of obtaining airworthiness approval of Global Positioning System (GPS) equipment for use as a supplemental navigation system for oceanic and remote domestic en route, terminal, and non-precision instrument approach (except localizer directional aid (LDA) and simplified directional facility (SDF) operations.

Provides guidance material on how to evaluate whether data processes comply with the requirements of RTCA/DO-200A, Standards for Processing Aeronautical Data.

This advisory circular (AC) guides airworthiness approval of Traffic Alert and Collision Avoidance Systems (TCAS II) Version 7.0 certified to technical standard order (TSO)-C119b, and associated Mode S transponders.

This AC will guide you in obtaining a design and production approval inder Technical Standard Order (TSO) C-165, Electronic Map Display Equipment for Graphical Depiction of Aircraft Position, for the software used to provide an airport moving map display(AMMD) intended for use on a Class 2 electronic flight bag (EFB).

a. This AC provides guidance for the installation and airworthiness approval of Automatic Dependent Surveillance - Broadcast (ADS?

a. The guidance in this advisory circular (AC) provides one acceptable means of compliance, but not the only means, for type design approval of aircraft that have a data link system installed.

This advisory circular (AC) provides guidance material for the airworthiness approval of installed positioning and navigation equipment.

a. In this advisory circular (AC), the Federal Aviation Administration (FAA) provides 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.

This advisory circular (AC) provides guidance for the initial and follow-on installations of Automatic Dependent Surveillance - Broadcast (ADS-B) In systems supporting ground and airborne traffic display applications.

a. This advisory circular (AC) supports the use of Flight Information Services - Broadcast (FIS-B) weather and other aeronautical data link products for enhanced situation awareness of flight conditions.

This advisory circular (AC) provides applicants with guidance for obtaining an airworthiness approval for traffic alert collision avoidance systems II (TCAS II).