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Number Office Title Date
21-2L AIR-40 Complying with the Requirements of Importing Countries or Jurisdictions When Exporting U.S. Products, Articles, or Parts

This advisory circular (AC) provides information about Title 14, Code of Federal Regulations (14 CFR) part 21, subpart L. It describes how to comply with the requirements of importing countries or jurisdictions when exporting U.S. products, articles, or parts. This AC does not include the requirements submitted to the Federal Aviation Administration (FAA) by other countries or jurisdictions, but it incorporates the requirements by reference to the FAA’s internet website. This AC is not mandatory and does not constitute a regulation. This AC describes an acceptable means, but not the only means, to comply with these requirements. However, if you use the means described in this AC, you must follow it in all important respects.

01-29-2010
21-19B AIR-200 Installation of Used Aircraft Engines in New Production Aircraft 01-29-2010
33.201-1 ANE-111 Extended Operations (ETOPS) Eligibility for Turbine Engines 01-21-2010
25.1419-2 ANM-110 Compliance with the Ice Protection Requirements of §§ 25.1419(e), (f), (g), and (h)

This advisory circular (AC) describes an acceptable means for showing compliance with the requirements of Title 14, Code of Federal Regulations (14 CFR), 25.1419(e), (f), (g), and (h), Ice protection. Part 25 contains the airworthiness standards applicable to transport category airplanes a. Installing a primary ice detection system; b. Developing visual cues and installing an advisory ice detection system to alert the flightcrew that the airframe ice protection system (IPS) must be activated; c. Identifying conditions conducive to airframe icing through the use of temperature and visible moisture cues; and d. Including in the airplane flight manual (AFM) procedures for activating and deactivating the airframe IPS.

10-27-2009
21-43 AIR-200 Issuance of Production Approvals Under Subparts G, K, & O

This advisory circular (AC) provides information for production approval holders (PAH) under Title 14, Code of Federal Regulations (14 CFR) part 21, Certification Procedures for Products, Articles, and Parts. This AC guides PAHs in developing and maintaining quality systems for the products and articles they produce. This guidance aids the applicant for a production approval or current PAH in developing a quality system that both meets the needs of the PAH and is compliant with the regulations. You can find this AC at http://www.faa.gov/regulations_policies/advisory_circulars/.

10-16-2009
21-44 AIR-200 Issuance of Export Airworthiness Approvals Under 14 CFR Part 21 Subpart L

This advisory circular (AC) provides information about Title 14, Code of Federal Regulations (14 CFR) part 21, Certification Procedures for Products, Articles, and Parts. The AC covers subpart L, Export Airworthiness Approvals. This AC is not mandatory and does not constitute a regulation. This AC describes an acceptable means, but not the only means, to comply with these requirements. However, if you use the means described in the AC, you must follow it in all important respects.

10-16-2009
45-2D AIR-200 Identification and Registration Marking

a. This advisory circular (AC) provides information about Title 14, Code of Federal Regulations (14 CFR), part 45, Identification and Registration Marking. This AC is not mandatory and does not constitute a regulation. This AC describes an acceptable means, but not the only means, to comply with the requirements for identifying aircraft, aircraft engines, or propellers with identification plates, and marking aircraft with nationality and registration marks. However, if you use the means described in the AC, you must follow it in all important respects.

b. A list of other related sections of 14 CFR and related publications, and definitions pertinent to this AC are located in the appendixes to this AC.

 

10-16-2009
23-11B ACE-100 14 CFR Part 23 Type Certification of an Airplane Originally Certificated to European Aviation Safety Agency (EASA) (CS-VLA) Standards or Joint Aviation Requirements – Very Light Airplane (JAR-VLA)

This advisory circular (AC) sets forth an acceptable means of showing compliance with Title 14 Code of Federal Regulations (14 CFR), part 23, for the certification of airplanes originally certificated to either European Aviation Safety Agency (EASA) CS-VLA or Joint Aviation Requirements (JAR) JAR-VLA.

10-07-2009
129-4A AFS-50 Maintenance Programs for U.S. Registered Aircraft Operated Under 14 CFR Part 129

 

This advisory circular (AC) provides information on maintenance programs to foreign air carriers and foreign persons operating U.S.-registered aircraft under Title 14 of the Code of Federal Regulations (14 CFR) part 129. Part 129, § 129.14(a) requires that each foreign air carrier and each foreign person operating a U.S.-registered aircraft within or outside the United States in common carriage shall ensure that each aircraft is maintained in accordance witha program approved by the FAA. Title 14 CFR part 43 prescribes the rules governing the performance of maintenance, reventive maintenance, and alterations of aircraft having a U.S. airworthiness certificate. You may submit an alternate maintenance program to the Federal Aviation Administration (FAA) if you ascertain the maintenance program meets therequirements of the pertinent FAA regulations. However, if you use the means described in this AC, you should conform to it in all important respects to assure acceptability.

09-30-2009
150/5220-24 AAS-100 Foreign Object Debris Detection Equipment

Provides information that airports can use to procure foreign object debris (FOD) detection equipment. Contains minimum performance specifications for systems and equipment that detect foreign objects on airports, including stationary radar, stationary electro-optical, stationary hybrid radar and electro-optical, and mobile radar.

See also Buy American Preferences to view:

  • Notice of Decision to Issue Buy American Waivers for Foreign Object Debris (FOD) Detection Equipment (11/28/2010)
  • Notice to Manufacturers of Foreign Object Debris (FOD) Detection Equipment (8/5/2010)
  • Waiver request process
09-30-2009
150/5300-9B AAS-100 Predesign, Prebid, and Preconstruction Conferences for Airport Grant Projects

Provides guidance for conducting predesign, prebid, and preconstruction conferences for projects funded under the FAA airport grant program. This version adds quality acceptance as a topic of discussion for the preconstruction conference, items to be addressed in the engineer’s report, details about what should be included in the phasing plan, and discussion of construction management plans.

09-30-2009
150/5320-6E AAS-100 Airport Pavement Design and Evaluation

Provides guidance to the public on the design and evaluation of pavements at civil airports.

Because of the size of the document, it is available as one large file (see Complete) or as four smaller files (see Parts 1-4).

See also related Airport Design Software.

09-30-2009
150/5340-26B AAS-100 Maintenance of Airport Visual Aid Facilities

Provides recommended guidelines for maintenance of airport visual aid facilities, including Runway Status Lights (RWSL) Systems, rotating beacons, lighted wind cone assemblies, runway and taxiway guidance signs, Precision Approach Path Indicator (PAPI) Systems, Visual Approach Slope Indicators (VASIs), Runway End Identifier Lights (REILs), Medium Approach Lighting Systems (MALS, MALSF, MALSR), Hazard Beacons And Obstruction Lights, and Airport Lighting Control And Monitoring Systems (ALCMS).

09-30-2009
150/5345-54B AAS-100 Specification for L-884, Power and Control Unit for Land and Hold Short Lighting Systems

Contains the FAA standards for power and control units for land and hold short lighting systems.

09-30-2009
150/5380-9 AAS-100 Guidelines and Procedures for Measuring Airfield Pavement Roughness

Provides guidelines and procedures for measuring and evaluating runway roughness as identified by surface profile data of rigid and flexible airport pavements. Provides technical procedures to quantify surface irregularities and to determine how surface irregularities may affect specific categories of airplanes.

09-30-2009
20-27G AIR-200 Certification and Operation of Amateur-Built Aircraft

This Advisory Circular (AC) provides information about Title 14, Code of Federal Regulations (14 CFR) part 21, Certification Procedures for Products and Parts, § 21.191(g) for the purpose of operating amateur-built aircraft.

09-30-2009
150/5200-12C AAS-300 First Responders’ Responsibility for Protecting Evidence at the Scene of an Aircraft Accident/Incident

Furnishes general guidance for airport employees, airport management, and other personnel responsible for aircraft rescue and firefighting (ARFF) operations at the scene of an aircraft accident on the proper preservation of evidence.  It explains the need for preservation of evidence and details operational actions which may be permitted if performed in the interest of preserving life.

09-28-2009
150/5210-17B AAS-300 Programs for Training of Aircraft Rescue and Firefighting Personnel

Provides information on courses and reference materials for training of Aircraft Rescue and Firefighting (ARFF) personnel.

09-23-2009
20-107B AIR-100 Composite Aircraft Structure

This AC sets forth an acceptable means, but not the only means of showing compliance with the provisions of Title 14 of the Code of Federal Regulations (14 CFR) parts 23, 25, 27, and 29 regarding airworthiness type certification requirements for composite aircraft structures involving fiber reinforced materials, e.g., carbon and glass fiber reinforced plastics. Guidance information is also presented on the closely related design, manufacturing, and maintenance aspects. The information contained herein is for guidance purposes and is not mandatory or regulatory in nature. 

09-08-2009
33.83-1 ANE-111 Comparative Method to Show Equivalent Vibratory Stresses and High Cycle Fatigue Capability for Parts Manufacturer Approval of Turbine Engine and Auxiliary Power Unit Parts

This advisory circular (AC) describes a comparative test and analysis method that may be used for turbine engine or auxiliary power unit (APU) blades or vanes when produced under parts manufacturer approval (PMA). PMA applicants may use this comparative modal and high-cycle fatigue (HCF) method to show the vibratory stresses and HCF capability of their proposed blades or vanes are equivalent to those of the type design parts. This method supports showing that the engine or APU still complies with part 33 of Title 14 of the Code of Federal Regulations (14 CFR part 33) or Technical Standard Order (TSO) C77.

09-08-2009
33.70-2 ANE-111 Damage Tolerance of Hole Features in High-Energy Turbine

 

This advisory circular (AC) provides definitions, guidance, and acceptable methods, but not the only methods, that may be used to demonstrate compliance with requirements in § 33.70 of Title 14 of the Code of Federal Regulations related to the integrity of engine life-limited parts. Section 33.70 contains requirements applicable to the design and life management of propulsion system life-limited parts, including high-energy rotating parts.   This AC presents a damage tolerance approach which can be used to address manufacturing and operationally-induced anomalies in turbine engine rotating part hole features. This approach can be readily integrated with the existing “safe-life” process for high-energy rotors to produce an enhanced life management process. This approach does not replace existing safe-life methodology but supplements it. In the context of damage tolerance, this AC is not intended to allow operation beyond the component manual life limit set using the existing safe life approach which limits the useful rotor life to the minimum number of flight cycles required to initiate a crack. Rotor failure modes for which full containment of high-energy debris can be demonstrated are excluded from the procedures outlined in this AC and need not be accounted for in the overall risk assessment.
08-28-2009
00-65 AFS-100 Towbar and Towbarless Movement of Aircraft

This advisory circular (AC) provides guidance for towbar and towbarless movement of aircraft.

08-27-2009
91-85 AFS-400 Approval of Aircraft and Operators for flight in Reduced Vertical 08-21-2009
33-8 ANE-111 Guidance for Parts Manufacturer Approval of Turbine Engine and Auxiliary Power Unit Parts under Test and Computation

This advisory circular (AC) provides guidance for developing substantiation data to support the design approval of critical and complex turbine engine and auxiliary power unit (APU) parts produced under parts manufacturer approval (PMA). This guidance is for the comparative test and analysis method used to show compliance to the airworthiness requirements under test and computation, per § 21.303 of Title 14 of the Code of Federal Regulations(14 CFR). This method supports showing the engine or APU still complies with 14 CFR part 33 and Technical Standard Order (TSO) C77.

b. Additionally, this AC provides information on developing a continued operational safety (COS) plan and part numbering for turbine engine parts.

08-19-2009
33.76-1A ANE-111 Bird Ingestion Certification Standards

This advisory circular (AC) provides guidance and acceptable methods, but not the only methods, that may be used to demonstrate compliance with the bird ingestion requirements of Title 14 of the Code of Federal Regulations (14 CFR) § 33.76. Although this AC does refer to regulatory requirements that are mandatory, this AC is not, in itself, mandatory. This AC neither changes any regulatory requirements, nor authorizes changes in, or deviations from, the regulatory requirements.

08-07-2009

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