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23.1311-1C ACE-100 Installation of Electronic Display in Part 23 Airplanes

This advisory circular (AC) provides 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. The guidance provided in this document is directed to airplane and avionics manufacturers, modifiers, and operators of part 23 category airplanes.  Applicants for a technical standard order (TSO) should consider following the guidance in this AC when the TSO requirements do not provide sufficient guidance. The main purpose of this revision of the AC is providing the guidance for the requirements in the turbojet rulemaking and some general updating due to lessons learned and advance and emerging technologies.

11-17-2011
23-8C ACE-100 Flight Test Guide for Certification of Part 23 Airplanes

a. This advisory circular (AC) sets forth an acceptable means, but not the only means, of  showing compliance with Title 14 of the Code of Federal Regulations (14 CFR) part 23 concerning flight tests and pilot judgements. Material in this AC is neither mandatory nor regulatory in nature and does not constitute a regulation.

b. This AC is one method being utilized to achieve national standardization in normal, utility, acrobatic, and commuter category airplanes. This AC applies to Subpart B and various sections under Subparts A, D, E, F and G from § 23.1 through § 23.1589. This AC consolidates existing policy documents, and certain ACs that cover specific paragraphs of the regulations, into a single document.

c. This material is intended as a ready reference for part 23 airplane manufacturers, modifiers, Federal Aviation Administration (FAA) design evaluation engineers, flight test engineers, and engineering flight test pilots, including Organization Delegation Option (DOA).

11-16-2011
150/5220-26 AAS-100 Airport Ground Vehicle Automatic Dependent Surveillance - Broadcast (ADS-B) Out Squitter Equipment

Provides guidance on the development, installation, testing, approval, and maintenance of Automatic Dependent Surveillance – Broadcast (ADS-B) Out squitter units for airport ground vehicles. Using this AC, airports will be able to acquire approved and authorized airport ground vehicle ADS-B squitter units that are compliant with Title 14 Code of Federal Regulations (CFR), Part 91, Automatic Dependent Surveillance-Broadcast (ADS–B) Out Performance Requirements to Support Air Traffic Control (ATC) Service, as well as the initial set of ADS-B applications. Please note that the technical specifications for manufacturing ADS-B squitter units for airport ground vehicles are published in the FAA’s document, Vehicle Automatic Dependent Surveillance - Broadcast (ADS-B) Specification, Version 2.4, published May 1, 2012.

Contact the appropriate FAA Airport District Office or Regional Airports Division to discuss Airport Improvement Program (AIP) eligibility.

Learn more about Automatic Dependent Surveillance-Broadcast (ADS-B).

CHANGE 1 (09-01-2012)

Provides guidance on the development, installation, testing, approval, and maintenance of Automatic Dependent Surveillance – Broadcast (ADS-B) Out squitter units for airport ground vehicles. Change 1 updates the ADS-B Specification version number, Table 1 to show airports with existing or planned FAA surveillance systems, and Appendix A to list qualified products.

CHANGE 2 (04-11-2016)

 Provides updated reference to the current version of the Vehicle Automatic Dependent Surveillance-Broadcast (ADS-B) Specification, FAA-E-3032, published January 7, 2015. The contact information of the existing product has been updated and a new qualified product (appendix A) is also included.

11-14-2011
35.23-1 ANE-111 Guidance Material for 14 CFR § 35.23, Propeller Control System

This advisory circular (AC) provides definitions and guidance for demonstrating compliance with the propeller control system requirements of Title 14 of the Code of Federal Regulations (14 CFR 35.23).

10-21-2011
25-19A ANM-117 Certification Maintenance Requirements

This advisory circular (AC) provides guidance on the selection, documentation, and control of Certification Maintenance Requirements (CMR). This AC also provides a rational basis for coordinating the Maintenance Review Board (MRB), if the MRB process is used, and CMR selection processes to ensure premises made in the system safety analyses supporting the compliance with the requirements of Title 14, Code of Federal Regulations (14 CFR) 25.1309, and other system safety rules (such as §§ 25.671, 25.783, 25.901, and 25.933) are protected in service. This AC describes an acceptable means, but not the only means, for selecting, documenting, and managing CMRs. Terms such as "shall" and "must" are used only in the sense of ensuring applicability of this particular means of compliance when the acceptable means of compliance described herein is used.

10-03-2011
150/5300-17C AAS-100 Standards for Using Remote Sensing Technologies in Airport Surveys

Provides guidance on the use of remote sensing technologies in the collection of data describing the physical infrastructure of an airport. This version is a substantial rewrite and includes new sections on remote sensing technologies other than aerial imagery (primarily LIDAR) for collecting airport data. See also the Airports GIS website.

09-30-2011
150/5370-11B AAS-100 Use of Nondestructive Testing in the Evaluation of Airport Pavements

Focuses on nondestructive testing (NDT) equipment that measures pavement surface deflections after applying a static or dynamic load to the pavement. It also briefly introduces other types of nondestructive measuring equipment to illustrate how supplementing NDT data with other test data may improve the quality and reliability of the pavement evaluation. This version updates Chapter 8, NDT-Based Evaluation and Design Updates, to reflect the requirements of the pavement design program FAARFIELD rather than the previous design program LEDFAA.

See also Airport Design Software.

09-30-2011
150/5370-15B AAS-100 Airside Applications for Artificial Turf

Provides guidance for the planning, design, installation, and maintenance of aviation grade artificial turf in areas adjacent to the operational areas of an airport.

09-30-2011
20-174 AIR-120 Development of Civil Aircraft and Systems

This advisory circular (AC) recognizes the Society of Automotive Engineers (SAE) Aerospace Recommended Practice (ARP) 4754A, Guidelines for Development of Civil Aircraft and Systems, dated December 21, 2010, as an acceptable method for establishing a development assurance process. SAE ARP 4754A discusses the development of aircraft and systems taking into account the overall aircraft operating environment and functions. This includes validation of requirements and verification of the design implementation for certification and process assurance.

09-30-2011
150/5345-28G AAS-100 Precision Approach Path Indicator (PAPI) Systems

Contains the FAA standards for the Precision Approach Path Indicator (PAPI) systems, which provides pilots with visual glideslope guidance during approach for landing.

See also--

09-29-2011
150/5345-56B AAS-100 Specification for L-890 Airport Lighting Control and Monitoring System (ALCMS)

Specifies the minimum requirements for an Airport Lighting Control and Monitoring System (ALCMS). The ALCMS simplifies the control and monitoring of lighted visual aids and enhances airport safety. The basic function of the system remains the same whether for a general aviation airport that supports only a few operations in a day or a large commercial airport which caters to hundreds of operations on any given day.

09-29-2011
150/5370-2F AAS-100 Operational Safety on Airports During Construction

Provides guidelines for operational safety on airports during construction. Principal changes include prohibiting construction in safety areas when associated runway or taxiway is open, providing guidance for incorporating safety risk management, and including checklists for writing Construction Safety and Phasing Plans (CSPP) and for daily inspections.

09-29-2011
20-173 AIR-130 Installation of Electronic Flight Bag Components

This advisory circular (AC) provides guidance material on the installation of electronic flight bag (EFB) components including aircraft connectivity provisions.  In it, the Federal Aviation Administration (FAA) describes certification considerations for individual EFB components and for installing EFB aircraft connectivity provisions by addressing the principal elements, or “components,” which comprise a typical EFB device or system. 

This AC describes an acceptable means, but not the only means, to comply with Title 14 of the Code of Federal Regulations (14 CFR) part 23, 25, 27, or 29.  This AC is not mandatory and does not constitute a regulation.  However, if you use the means described in this AC, you must follow it entirely.  The term “must” is used to indicate mandatory requirements when following the guidance in this AC.  The terms “should” and “recommend” are used when following the guidance is recommended but not required to comply with this AC. 

09-27-2011
21-51 AIR-110 Applicant’s Showing of Compliance and Certifying Statement of Compliance

We, the Federal Aviation Administration (FAA), wrote this advisory circular (AC) to describe how to comply with the requirements of Title 14 of the Code of Federal Regulations (14 CFR) 21.20, 21.97 and 21.303(a)(5). 
 This AC is not mandatory and is not a regulation.  This AC describes an acceptable means, but not the only means, to comply with the requirements 14 CFR 21.20, 21.97 and 21.303(a)(5).  However, if you use the means described in this AC, you must follow it entirely

09-27-2011
150/5345-39D AAS-100 Specification for L-853, Runway and Taxiway Retroreflective Markers

Contains the Federal Aviation Administration (FAA) standards for retroreflective markers for airport runways and taxiways. Version D changes Paragraph 3.4.2.2, Cylindrical Markers, to increase the marker diameter and surface area, and Paragraph 3.4.3.1, Mounting System, to clarify Type II marker mounting and tethering requirements.

Effective six months after the issue date of this AC, only equipment qualified per these specifications will be listed in AC 150/5345-53, Airport Lighting Equipment Certification Program.

09-26-2011
20-136B AIR-130 Aircraft Electrical and Electronic System Lightning Protection

This advisory circular (AC) provides you with information and guidance on how you can protect aircraft electrical and electronic systems from the effects of lightning. This AC describes a means, but not the only means, for you to show compliance with Title 14 of the Code of Federal Regulations (14 CFR) 23.1306, 25.1316, 27.1316, and 29.1316, Electrical and electronic system lightning protection, as they pertain to the type or supplemental type certification of your aircraft.

This AC is not mandatory and does not constitute a regulation. However, if you use the means described in this AC to comply with 14 CFR 23.1306, 25 .1316, 27.1316, and 29.131 6, you must follow it in its entirety.

The term "must" is used to indicate mandatory requirements when following the guidance in this AC in its entirety. The terms "should" and "recommend" are used when following the guidance is recommended but not required to comply with this AC.

09-07-2011
150/5100-13B AAS-100 Development of State Standards for Nonprimary Airports

Provides guidelines for the development of State standards for and the use of State highway specifications for pavement construction at nonprimary public-use airports as provided for in title 49 United States Code (USC), Sections 47105(c) and 47114(d)(5), respectively.

08-31-2011
91-82A ACE-100 Fatigue Management Programs for In-Service Issues

a.This advisory circular (AC) provides guidance on developing and implementing a Fatigue Management Program (FMP) to address in-service issues for metallic fatigue critical structure.  An applicant may develop an FMP as one method to address an unsafe condition when the Federal Aviation Administration (FAA) determines an airplane type design has a demonstrated risk of catastrophic failure due to fatigue.  In such cases, the FMP should incorporate damage-tolerance based inspections or a part replacement/modification program to mitigate the demonstrated risk.  The FMP should also incorporate other fatigue critical structure inspections to address the broader risk posed by potential cracking of these structures in the airplane.  The FAA will mandate the FMP by Airworthiness Directive (AD).  The FAA may also approve the FMP as an alternative method of compliance (AMOC) to an AD.

b.This AC includes guidance relevant to developing FMPs for other purposes such as life extensions, type certification requirements, or non-mandatory maintenance programs.  This guidance supplements other ACs that contain guidance for developing damage-tolerance based inspection programs to look proactively for potential cracks.  Such guidance includes AC 91?56B, Continuing Structural Integrity Program for Airplanes, AC 25.571?1D, Damage Tolerance and Fatigue Evaluation of Structure, and AC 23?13A, Fatigue, Fail-Safe, and Damage-Tolerance Evaluation of Metallic Structure for Normal, Utility, Acrobatic, and Commuter Category Airplanes.  Applicants should use product specific guidance in conjunction with this AC.

c.   This AC is not mandatory and does not constitute a regulation.  It describes an acceptable means, but not the only means, for maintaining the continued operational safety for airplane type designs that have a demonstrated risk.  In this AC, the FAA uses terms such as “must” or “require” only in the sense of ensuring applicability of a particular method of compliance when using a specific acceptable method of compliance described herein.

08-23-2011
121.321-1 ANM-100 Compliance with Requirements of § 121.321, Operations in Icing

This advisory circular (AC) describes an acceptable means for showing compliance with the requirements of Title 14, Code of Federal Regulations (14 CFR) 121.321, Operations in Icing.  Part 121 contains the aircraft operating requirements applicable to domestic, flag, and supplemental operations.  This AC provides guidance for:

a.   Using visible moisture and temperature as a means for the flightcrew to know when the airframe ice protection system (IPS) must be activated.

b.   Developing acceptable procedures for activating and deactivating the airframe IPS.

c.    Installing a primary or advisory ice detection system.

08-04-2011
65-33 AFS-300 Development of Training/Qualification Programs for Composite Maintenance Technicians

This document is intended as a guideline for organizations to develop a formal training program for qualification of composite technicians. This advisory circular (AC) contains recommendations for the experience, training, qualification, and examination of persons performing maintenance and repair of aircraft composite structures or other aviation composite components. It recommends criteria for the qualification of personnel to be able to understand the technical principles involved in the maintenance and repair of aircraft composites. This document applies to those individuals directly responsible for providing training, supervision, or oversight of composite maintenance personnel. Organizations may use the information contained in this AC to develop a written program describing the guidelines used to train and qualify personnel.This AC provides a means, but not the only means, of developing a composite maintenance training program.

08-03-2011
150/5345-47C AAS-100 Specification for Series to Series Isolation Transformers for Airport Lighting Systems

Contains the Federal Aviation Administration (FAA) specifications for series to series isolation transformers for use in airport lighting systems.

07-22-2011
33.27-1A ANE-111 Engine and Turbosupercharger Rotor Overspeed Requirements of 14 CFR § 33.27.

This advisory circular (AC) provides guidance and acceptable methods, but not the only methods, for demonstrating compliance with the rotor strength (overspeed) requirements of Title 14 of the Code of Federal Regulations (14 CFR) 33.27.

07-18-2011
150/5100-19D ACO-100 Guide for Airport Financial Reports Filed by Airport Sponsors

Provides airport sponsors with guidance on filing FAA Form 5100-126, Financial Governmental Payment Report, and FAA Form 5100-127, Operating and Financial Summary. Announces changes to the FAA's financial reporting program and to Form 5100-127.

See also Airport Financial Reporting Program.

06-23-2011
21-16G AIR-100 RTCA Document DO-160 versions D, E and F, “Environmental Conditions and Test Procedures for Airborne Equipment”

a. This advisory circular (AC) identifies RTCA Document No. (RTCA/DO)-160 versions D, E, F, and G, Environmental Conditions and Test Procedures for Airborne Equipment, dated July 27, 1997, December 20, 2005, December 6, 2007, and December 8, 2010, respectively, as containing acceptable environmental qualifications to show compliance with certain airworthiness requirements. The FAA strongly encourages the use of RTCA/DO-160G for new articles.

b. Appendix 1 of this AC provides a summary of the changes from RTCA/DO-160C to RTCA/DO-160D, version D to E, version E to F, and F to G. The information in the table will assist you in determining if a particular version of RTCA/DO-160 is acceptable.

06-22-2011
150/5220-10E AAS-100 Guide Specification for Aircraft Rescue and Fire Fighting (ARFF) Vehicles

Provides an interactive specification that airports can use in procuring Aircraft Rescue and Fire Fighting (ARFF) vehicles. It describes the selection process, vehicle requirements, and how to produce formal specifications.

06-01-2011

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