a. This advisory circular (AC) will show you how to gain Federal Aviation Administration (FAA) approval of your compliance with Title 14, Code of Federal Regulations (14 CFR) §§ 23.954, 25.954, 27.954, and 29.954, Fuel system lightning protection.

This advisory circular (AC) will show you how to gain Federal Aviation Administration (FAA) approval of your 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.

Provides information and guidance concerning an acceptable means, but not the only means, of compliance with Parts 23, 25, 27, and 29 of the FAR as applicable for preventing hazardous effects, due to lightning, from occurring to electrical/electronic systems performing critical essential functions.

This advisory circular (AC) provides applicants with guidance for installing and using passive radio frequency identification (RFID) tags on aviation products and equipment.

RTCA/DO-160E, “Environmental Conditions and Test Procedures for Airborne Equipment,” dated December 9, 2004, as containing acceptable environmental qualifications for showing compliance with certain airworthiness requirements.

This advisory circular (AC) provides applicants with guidance for installing and using passive radio frequency identification (RFID) tags on aviation products and equipment.

Suggests acceptable methods by which product manufacturers may indicate FAA approval of recommended actions prescribed in manufacturers’ service documents.

This advisory circular (AC) provides guidance and acceptable methods, but not the only methods, for demonstrating compliance with the applicable engine induction system icing and engine ice ingestion requirements.

Provides guidelines for design approval of aircraft data communications systems and applications primarily used for air traffic services.

This advisory circular (AC) applies to manufacturers and installers of products or appliances incorporating complex custom micro-coded components with hardware design assurance levels of A, B, and C.

This advisory circular (AC) establishes an acceptable means, but not the only means, to obtain Federal Aviation Administration’s (FAA) airworthiness approval for the installation of an Integrated Modular Avionics (IMA) System that uses hardware elements authorized under Technical Standard Order (TSO)-C153, Integrated Modular Avionics Hardware Elements.

This advisory circular (AC) provides guidance for the migration of satellite voice systems for direct pilot/controller communictions as a supplement to high frequency/very high frequency (HF/vhf) voice communication systems.

Provides a means of getting Federal Aviation Administration (FAA) approval of aircraft lightning protection.

In this advisory circular (AC), the Federal Aviation Administration (FAA) provides applicants with guidance for obtaining airworthiness approval for equipment installation of a Synthetic Vision Guidance System (SVGS) in aircraft.

The AC offers one way to achieve an acceptable level of performance for an aircraft recording system when a controller-pilot data communication capability is installed.