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Aircraft Pressures and Temperatures – Resource DocumentAIR8471 (Current)
This SAE AIR covers Forced Air technology including: reference material, equipment, safety, operation, and methodology. It is intended to provide pressure and temperature (temps pages 26 & 31) information and minimum safety guidelines regarding use of equipment to remove frozen contaminants related to: i) Forced air ii) Forced air/fluid iii) Deicing fluid
G-12M Methods Committee
Aircraft Skin Pressures and TemperaturesAIR8469 (Current)
This information report covers all known aircraft with respect to deicing operations, especially with regard to OEM pressure and temperature limitations on the airframe. It provides data for airlines/operators on compliance with OEM limits and confirms that OEM limits are not exceeded during deicing operations.
G-12M Methods Committee
Missile Hydraulic Pumps and Their Power SourcesAIR560D (Current)
This AIR provides information about the specific requirements for missile hydraulic pumps and their associated power sources.
A-6C4 Power Sources Committee
COUPLING, MALE, 12 INCH AIR DUCTAS7365/3A (Current)6/11/2026
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
UNION, FLARELESS TUBE FITTING, INTERNALLY SWAGEDAS5530A (Current)6/11/2026
SCOPE IS UNAVAILABLE.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
FITTING, TEE, PIPE, INTERNAL THREADAS4857B (Current)6/11/2026
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
UNION, SHORT FLARELESS TUBE FITTING, INTERNALLY SWAGEDAS5531A (Current)6/11/2026
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
COUPLING, FEMALE, 12 INCH AIR DUCTAS7365/2A (Current)6/11/2026
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
BAND, FEMALE COUPLING, 12 INCH AIR DUCTAS7365/6A (Current)6/11/2026
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
ARP4754B Clarification NoticeAIR4757 (Current)6/11/2026
The purpose of this AIR is to provide additional information on some areas of ARP4754B/ED-79B that may need additional clarification in order to be put into practice. This document should be used in conjunction with ARP4754B/ED-79B. The contents are recommendations and should not be construed to be regulatory requirements. This document may be revised with additional information as ARP4754B/ED-79B is put into practice.
S-18 Aircraft and Sys Dev and Safety Assessment Committee
Identification and Assessment of Damage to Composite Aircraft Structures Training DocumentAIR6825 (Current)6/10/2026
Individuals who complete the applicable modules aligned with this training document will be able to define the type of damage, define the extent of damage, determine if further inspection is required, evaluate the damage against published allowable damage limits, and provide accurate documentation of the damage. The intended outcome of the training is increased safety such that no aircraft is released with unknown damage and that the aircraft meets continued airworthiness requirements. The goal is to change the culture from damage discovery to damage reporting while also reducing or eliminating flight delays due to incorrect or insufficient information. Teaching levels have been assigned to the curriculum to define the knowledge, skills, and abilities graduates will need. Minimum hours of instruction have been provided to ensure adequate coverage of all subject matter including lecture and practical exercise. These minimums may be exceeded and may include an increase in the total
AMS CACRC Commercial Aircraft Composite Repair Committee
Unidirectional Carbon Fiber Tape Epoxy Repair Prepreg, Vacuum Curing Part 2 - Qualification Program for Fiber, Carbon Fiber Tape Prepreg, and Film AdhesiveAMS6885/2 (Current)6/10/2026
AMS6885/2 gives specific information about the qualification program for unidirectional carbon fiber tape epoxy repair prepreg capable of curing under vacuum for repair of carbon fiber reinforced epoxy structures. The prepreg system shall include an epoxy film adhesive to be applied in a co-bonding process with the prepreg for solid laminate and sandwich bonding.
AMS CACRC Commercial Aircraft Composite Repair Committee
SLEEVE, FLARELESS TUBE FITTING, INTERNALLY SWAGEDAS5529A (Current)6/10/2026
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
FITTING, FERRULE END - THREADED COUPLING, RIGID, SELF-BONDING, DESIGN STANDARDAS5947A (Current)6/10/2026
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Unidirectional Carbon Fiber Tape Epoxy Repair Prepreg, Vacuum Curing Part 1 - General RequirementsAMS6885/1 (Current)6/10/2026
AMS6885/1 gives information about the technical requirements and qualification procedure for unidirectional carbon fiber tape epoxy repair prepreg capable of curing under vacuum for repair of carbon fiber reinforced epoxy structures. The repair system includes an epoxy film adhesive to be applied in a co-bonding process with the prepreg for solid laminate and sandwich bonding.
AMS CACRC Commercial Aircraft Composite Repair Committee
Unidirectional Carbon Fiber Tape Epoxy Repair Prepreg, Vacuum Curing Part 0 - IntroductionAMS6885 (Current)6/10/2026
This document (Technical Specification) gives information about qualification rules and the relation between the different specification parts involved, such as the Technical Specification (TS), the Material Specification (MS), and the Purchasing Specifications (PS).
AMS CACRC Commercial Aircraft Composite Repair Committee
STUD, LOCKED IN, KEY LOCKED, UNS S66286, 140 KSI/1200 °F LIGHTWEIGHT, SELF-BROACHING KEYSAS3543B (Current)6/10/2026
E-25 General Standards for Aerospace and Propulsion Systems
Conducting Measurement Systems Analysis for Rotor Balancing TasksAIR6966 (Current)6/10/2026
This AIR provides a general guideline on how to perform effective measurement systems analysis study (MSA) for rotor balancing tasks. The document also includes applicable data analysis methods and result interpretation.
EG-1A Balancing Committee
Rolling Element Bearing Axial and Radial Internal ClearanceARP5483/3B (Current)6/10/2026
This test method outlines the standard procedure for measuring the radial and axial internal clearance of rolling element bearings used in airframe controls.
ACBG Rolling Element Bearing Committee
Aircraft Surface Coating Interaction with Aircraft Deicing/Anti-Icing FluidsAIR6232 (Current)6/10/2026
This SAE Aerospace Information Report (AIR) provides descriptions of test methods for determining if an aircraft surface coating of any thickness has adverse effects on aircraft deicing/anti-icing fluids with respect to fluid holdover time performance and aerodynamic performance. Although not the primary mandate of the G-12 Aircraft Ground Deicing Committee, this document also provides descriptions of suggested test methods for evaluating aircraft surface coatings with respect to durability, hardness, weathering, aerodynamic drag, ice adhesion, ice accumulation, contact angle, and thermal conductivity. These additional tests can provide informational data for characterizing the coatings and may be useful to operators when evaluating the coatings.
G-12ADF Aircraft Deicing Fluids
Aircraft Fuel System Design GuidelinesAIR7975A (Current)6/9/2026
This document describes the major design drivers and considerations when designing a fuel system for a large commercial aircraft. While not intended as a design manual for individual system components, it does refer out to other SAE specifications where more detail on specific components and subsystems is given. It does include examples of a number of calculations associated with sizing of fuel systems, based on those given in NAVAIR 06-5-504, as well as an appendix summarizing basic fluid mechanical equations that are key for fuel system design. It is acknowledged that most of these calculations would today be performed by modeling tools rather than by hand, but it is considered important for the designer to understand the principles. Some details specific to military aircraft are included, but it is intended that later issues of this document will include appendices that give specific considerations for military aircraft, smaller commercial aircraft, and rotorcraft. Features unique
AE-5A Aerospace Fuel, Inerting and Lubrication Sys Committee
BEARING, BALL, AIRFRAME, ANTIFRICTION, INTERMEDIATE DUTY CORROSION RESISTANT NITROGEN STEEL (CREN)AS27649/1A (Current)6/9/2026
ACBG Rolling Element Bearing Committee
BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, DRILLED, PD SHANK, UNS S66286, SILVER PLATED, .3750-24 UNJF-3AAS9577C (Current)6/8/2026
E-25 General Standards for Aerospace and Propulsion Systems
TERMINAL JUNCTION SYSTEM, TERMINAL JUNCTION BLOCKS, SECTIONAL, BUSSING MODULES, FEEDBACK TYPE, SIZE 22D, SERIES IAS81714/17D (Current)6/8/2026
AE-8C2 Terminating Devices and Tooling Committee
Nickel Alloy, Corrosion- and Heat-Resistant, Sheet, Strip, and Foil, 62Ni - 21.5Cr - 9.0Mo - 3.7Cb (Nb) (Alloy 625), Consumable Electrode Remelted, Cold Rolled and AnnealedAMS5879F (Current)6/8/2026
This specification covers a corrosion- and heat-resistant nickel alloy in the form of sheet, strip, and foil 0.100 inch (2.54 mm) and under in nominal thickness.
AMS F Corrosion and Heat Resistant Alloys Committee
SCREW, DRIVE, ROUND HEAD, TYPE U AMS5504 (UNS S41000)AS3568B (Current)6/8/2026
E-25 General Standards for Aerospace and Propulsion Systems
Plating, GoldAMS2422G (Current)6/8/2026
This specification covers the requirements for electrodeposited gold plate.
AMS B Finishes Processes and Fluids Committee
BOLT, MACHINE - DOUBLE HEX EXTENDED WASHER HEAD, DRILLED, CLOSE TOL SHANK, AMS5643 (UNS S17400), 140 KSI, .5000-20 UNJF-3AAS3179C (Current)6/8/2026
E-25 General Standards for Aerospace and Propulsion Systems
Safety Considerations for Aircraft-Mounted Lasers Projected into the Navigable AirspaceARP5674A (Current)6/8/2026
This SAE Aerospace Recommended Practice (ARP) is intended to be used for laser systems mounted on aircraft and propagated into navigable airspace. This does not include lasers onboard aircraft where the beam is contained within an enclosure so that the beam cannot enter into airspace, nor does it include lasers from satellites and spacecraft in outer space. It may be used in conjunction with AS4970, ARP5535, ARP5572, ARP5293, and the ANSI Z136 laser safety standards.
G-10T Laser Safety Hazards Committee
BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, DRILLED, PD SHANK, SILVER PLATED, CORROSION AND HEAT RESISTANT STEEL, SIMILAR TO UNS S66286, 130 KSI MIN, .2500-28 UNJF-3AAS9575F (Current)6/8/2026
E-25 General Standards for Aerospace and Propulsion Systems
Guide to Certification of Aircraft in a High-Intensity Radiated Field (HIRF) EnvironmentARP5583B (Current)6/8/2026
This document and the EUROCAE equivalent, ED-107, provides detailed information, guidance, and methods in support of the Federal Aviation Administration (FAA) Advisory Circular (AC) 20-158 and to the European Union Aviation Safety Agency (EASA) AMC 20-158. AC 20-158 provides a means, but not the only means, for demonstrating compliance with Title 14 of the Code of Federal Regulations (14 CFR) 23.1308 (Amendment 57 and lower), 23.2520 (Amendment 64 and higher), 25.1317, 27.1317, 29.1317, and applicable FAA HIRF special conditions addressing HIRF Protection. AMC 20-158 is applicable to Certification Specifications CS 23.1308 (Amendment 4 and lower), 23.2520 (Amendment 5 and higher), 25.1317, 27.1317, and 29.1317. It should be noted that this document is neither mandatory nor regulatory in nature and does not constitute a regulation or legal interpretation of the regulation. Therefore, an applicant may elect to establish an alternative method of compliance that is acceptable to the
AE-4 Electromagnetic Compatibility (EMC) Committee
WASHER, KEY - SINGLE, BEARING RETAINING, AMS6350 (UNS G41300)AS172201C (Current)6/8/2026
SCOPE IS UNAVAILABLE.
E-25 General Standards for Aerospace and Propulsion Systems
Uphill Quenching of Aluminum Alloy ProductAMS2767B (Current)6/8/2026
This specification establishes the engineering requirements for the uphill quenching process of aluminum alloy product. Uphill quenching immerses product in liquid nitrogen followed by exposure to a high-pressure/high-velocity steam blast or boiling water.
AMS D Nonferrous Alloys Committee
Leaded Phosphor Bronze Strip, 88.5Cu - 4.0Sn - 4.0Pb - 3.0Zn - 0.26P, Cold Rolled, Half Hard (H02)AMS4520N (Current)6/8/2026
This specification covers a copper alloy in the form of strip (see 8.6).
AMS D Nonferrous Alloys Committee
Systems Engineering Capability Model Appraisal MethodEIAIS731_2 (Current)7/1/2015
G-47 Systems Engineering
Assessment Guide for Process CertificationEIA681 (Current)8/1/2015
This Assessment Guide is applicable to any assessment technique that wishes to embrace the principles and concepts presented in the EIA-599 National Electronic Process Certification Standard.
Systems Management Council
Engineering & Operations Council Guide for Committee Review of Government DocumentsEIAEP12A (Current)7/1/2015
Systems Management Council
CDIF - Framework for Modeling and ExtensibilityEIAIS107 (Current)7/1/2015
Systems Management Council
CDIF - Transfer Format Encoding - ENCODING.1EIAIS110 (Current)7/1/2015
The CDIF Family of Standards is primarily designed to be used as a description of a mechanism for transferring information between CASE tools. It facilitates a successful transfer when the authors of the importing and exporting tools have nothing in common except an agreement to conform to CDIF. The language that is defined for the Transfer Format also has applicability as a general language for Import/Export from repositories. The CDIF Integrated Meta-model defined for CASE also has applicability as the basis of standard definitions for use in repositories. The standards which form the complete family of CDIF Standards are documented in EIA/IS-106 CDIF - CASE Data Interchange Format - Overview. These standards cover the overall framework, the transfer format and the CDIF Integrated Meta-model. The diagram in Figure 1 depicts the various standards that comprise the CDIF Family of Standards. The shaded box depicts this Standard and its position in the CDIF Family of Standards. This
Systems Management Council
Operator Interface Functions of Numerical ControlsEIA441 (Current)7/1/2015
This Standard is intended to serve as a guide in the coordination of system design to promote uniformity of the nomenclature and description of the operator devices.
Systems Management Council
CDIF - Integrated Meta-model Common Subject AreaEIAIS112 (Current)7/1/2015
The CDIF Family of Standards is primarily designed to be used as a description of a mechanism for transferring information between CASE tools. It facilitates a successful transfer when the authors of the importing and exporting tools have nothing in common except an agreement to conform to CDIF. The language that is defined for the Transfer Format also has applicability as a general language for Import/Export from repositories. The CDIF Integrated Meta-model defined for CASE also has applicability as the basis of standard definitions for use in repositories. The standards that form the complete family of CDIF Standards are documented in EIA/IS-106 CDIF - CASE Data Interchange Format - Overview. These standards cover the overall framework, the transfer format and the CDIF Integrated Meta-model. The diagram in Figure 1 depicts the various standards that comprise the CDIF Family of Standards. The shaded box depicts this Standard and its position in the CDIF Family of Standards. This
Systems Management Council
Lot Acceptance Procedure for Verifying Compliance With the Specified Quality Levels (SQL) in PPMEIA555 (Current)8/1/2015
This Specification covers a statistical sampling plan for lot inspection by attributes. It verifies that the customer's specified quality level (SQL) is not being exceeded. The estimate of fraction nonconforming determined by EIA Interim Standard No. EIA-554 is used to select the optimum sample plan for verifying that a given lot meets the specified quality level (SQL).
Systems Management Council
Library of Parameterized Modules (LPM) Version 210EIAIS103A (Current)7/1/2015
Systems Management Council
CDIF - CASE Data Interchange Format - OverviewEIAIS106 (Current)7/1/2015
The CDIF Family of Standards is primarily designed to be used as a description of a mechanism for transferring information between CASE tools. It facilitates a successful transfer when the authors of the importing and exporting tools have nothing in common except an agreement to conform to CDIF. The CDIF Family of Standards includes an Integrated Meta-model and a Transfer Format definition. It also includes the specification of a meta-meta-model and associated rules that define a framework for the Integrated Meta-model and the Transfer Format. The language that is defined for the Transfer Format also has applicability as a general language for Import/Export for repositories. The CDIF Integrated Meta-model also has applicability as the basis of standard definitions for use in repositories. The diagram in Figure 1 depicts the various standards that comprise the CDIF Family of Standards. The shaded box depicts this Standard and its position in the CDIF Family of Standards. This document
Systems Management Council
Harmonizing CALS Product Data Description StandardsEIACALS (Current)7/1/2015
Systems Management Council
CDIF - Integrated Meta-model Foundation Subject AreaEIAIS111 (Current)7/1/2015
The CDIF Family of Standards is primarily designed to be used as a description of a mechanism for transferring information between CASE tools. It facilitates a successful transfer when the authors of the importing and exporting tools have nothing in common except an agreement to conform to CDIF. The language that is defined for the Transfer Format also has applicability as a general language for Import/Export from repositories. The CDIF Integrated Meta-model defined for CASE also has applicability as the basis of standard definitions for use in repositories. The standards which form the complete family of CDIF Standards are documented in EIA/IS-106 CDIF - CASE Data Interchange Format - Overview. These standards cover the overall framework, the transfer format and the CDIF Integrated Meta-model. The diagram in Figure 1 depicts the various standards that comprise the CDIF Family of Standards. The shaded box depicts this Standard and its position in the CDIF Family of Standards. This
Systems Management Council
T-BOLT, A-286, 1000 °F BUSHING HEADAS4108/2B (Current)11/17/2025
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
CDIF - Integrated Meta-model Data Modeling Subject AreaEIAIS114 (Current)7/1/2015
The CDIF Family of Standards is primarily designed to be used as a description of a mechanism for transferring information between CASE tools. It facilitates a successful transfer when the authors of the importing and exporting tools have nothing in common except an agreement to conform to CDIF. The language that is defined for the Transfer Format also has applicability as a general language for Import/Export from repositories. The CDIF Integrated Meta-model defined for CASE also has applicability as the basis of standard definitions for use in repositories. The standards that form the complete family of CDIF Standards are documented in EIA/IS-106 CDIF - CASE Data Interchange Format - Overview. These standards cover the overall framework, the transfer format and the CDIF Integrated Meta-model. The diagram in Figure 1 depicts the various standards that comprise the CDIF Family of Standards. The shaded box depicts this Standard and its position in the CDIF Family of Standards. This
Systems Management Council
Requirements for the Control of Electromagnetic Interference Emissions and Susceptibility Characteristics of Equipment Intended to Operate in Severe Electromagnetic EnvironmentsEIAIS647 (Current)7/1/2015
This standard establishes the performance requirements for the control of the electromagnetic emission and susceptibility characteristics of electronic, electrical, and electromechanical equipment and subsystems designed or procured for use in severe electromagnetic environments such as ships, aircraft, spacecraft, armored vehicles, etc. Such equipment and subsystems may be used independently or as an integral part of other subsystems or systems.
PNT Position, Navigation, and Timing
Systems Engineering Capability ModelEIAIS731_1 (Current)7/1/2015
The purpose of this Interim Standard is to support the development and improvement of systems engineering capability.
G-47 Systems Engineering
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