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Lithium and Lithium-Ion Cell and Battery Containment Performance Recommended PracticeJ3303_202510 (Current)10/2/2025
Prescribe test conditions to quantify the effectiveness of containment devices for containing thermal runaway hazards of lithium/lithium-ion cells, batteries, and equipment during storage resulting from the failure of a cell within the container. Due to the many storage locations (indoors, outdoors, etc.), the hazards shall be classified individually to allow for varying performance based on a given storage location.
Battery Transportation and Storage Committee
Use Cases for Customer Communication for Plug-In Electric VehiclesJ2836/5_202603 (Current)3/18/2026
This SAE Information Report establishes the Use Cases for communications and customer-focused Key Performance Indicators (KPI) between plug-in electric vehicles (PEVs) and their customers. The Use Case Scenarios define the information to be communicated related to customer convenience features for charge on/off control, charge power curtailment, customer preference settings, charging status, electric vehicle supply equipment (EVSE) availability/access, and electricity usage, plus customer information resulting from conflicts to charging preferences. It also addresses the KPI that can provide a uniform set of metrics to quantitively assess the charging experience. This document only provides the Use Cases that define the communications requirements to enable customers to interact with the PEV and the KPI to optimize their experience with charging a PEV. Specifications such as protocols and physical transfer methods for communicating information are not within the scope of this document.
Hybrid - EV Committee
Communication Between Plug-In Vehicles and CustomersJ2847/5_202509 (Current)9/10/2025
This SAE Recommended Practice establishes the communication for the variety of potential functions for plug-in electric vehicle (PEV) customers. This includes features for use case items in SAE J2836/3 that may be PEV/customer optional equipment, such as AC vehicle-to-load (V2L) and AC vehicle-to-vehicle systems. These systems conform to SAE J1772 with variations required to identify to the PEV bidirectional onboard charger (OBC) the mode of operation changes and output requirements. SAE has published multiple documents relating to PEV and vehicle-to-grid (V2G) interfaces. The various document series are listed below, with a brief explanation of each. Figure 1 shows the sequencing of these documents and their primary function (e.g., the SAE J2836 and SAE J2847/1 documents start with smart charging, SAE J2836 and SAE J2847/2 then add DC charging, etc.). The intent is to have subsequent slash sheets complement each other as more functions and features are included. The /6 series of documents add wireless charging items not already included in the proceeding slash sheets. These are all then included in interoperability in SAE J2953 and security in SAE J2931/7. SAE J3072 then includes the PEV to grid requirements for V2G power and communication to match the SAE J2836/3 use cases.
Hybrid - EV Committee
Laboratory Testing of Vehicle and Industrial Heat Exchangers for Durability Under Vibration-Induced LoadingJ1598_202605 (Current)5/15/2026
This SAE Recommended Practice is applicable to all liquid-to-gas, liquid-to-liquid, gas-to-gas, and gas-to-liquid heat exchangers used in vehicle and industrial cooling systems. This document outlines the test to determine durability characteristics of the heat exchanger from vibration-induced loading.
Cooling Systems Standards Committee
Recommended Practice for Performance Rating of Lead Acid and Nickel Metal Hydride Electric Vehicle Battery ModulesJ1798/1_202605 (Current)5/19/2026
This SAE Recommended Practice provides for common test and verification methods to determine lead acid and nickel metal hydride electric vehicle battery module performance. The document creates the necessary performance tests to determine (a) what the basic performance of EV battery modules is, and (b) if battery modules meet minimum performance specification established by vehicle manufacturers or other purchasers. Specific values for these minimum performance specifications are not a part of this document.
Battery Standards Testing Committee
Guide to Engine Lubrication System MonitoringAIR1828D (Current)5/15/2026
This SAE Aerospace Information Report (AIR) provides information and guidance for the selection and use of technologies and methods for lubrication system monitoring of gas turbine aircraft engines. This AIR describes technologies and methods covering oil system performance monitoring, oil debris monitoring, and oil condition monitoring. Both on-aircraft and off-aircraft applications are presented. A higher-level view of lubrication system monitoring as part of an overall engine monitoring system (EMS) is discussed in ARP1587. The scope of this document is limited to those lubrication system monitoring, inspection, and analysis methods and devices that can be considered appropriate for health monitoring and routine maintenance. This AIR is intended to be used as a technical guide. It is not intended to be used as a legal document or standard.
E-32 Aerospace Propulsion Systems Health Management
Rating Air-Conditioner Evaporator Air Delivery and Cooling CapacitiesJ1487_202605 (Current)5/15/2026
The purpose of this SAE Recommended Practice is to establish uniform test procedures for measuring and rating air delivery and cooling capacity of truck and off-road self-propelled work machines used in earth moving, agriculture, and forestry air-conditioner evaporator assemblies. It is the intent to measure only the actual cooling capacity of the evaporator. It is not the intent of this document to rate and compare the performance of the total vehicle air-conditioning system.
Truck and Bus Windshield Wipers and Climate Control Comm
Advanced Composites Prepreg - Nominal 250 °F (121 °C) Cure - 12K Tow Carbon Fiber and Epoxy Resin, Plain Weave FabricAMS3914B (Current)5/15/2026
The intent of this specification is for the procurement of plain weave fabric epoxy prepreg product with 250 °F (121 °C) cure for aerospace applications; therefore, no qualification or equivalency threshold values are provided. Users that intend to conduct a new material qualification or equivalency program must refer to the production quality assurance section (see 4.3).
AMS P17 Polymer Matrix Composites Committee
Standard for Safety Glazing Materials for Glazing Motor Vehicles and Motor Vehicle Equipment Operating on Land Highways - Safety StandardSAEJ3097/ANSIZ26.1_202604 (Current)4/17/2026
Specifications, test methods, and usage provisions for safety glazing materials used for glazing of motor vehicles and motor vehicle equipment operating on land highways.
Glazing Materials Standards Committee
Standard Practice for Force Protection and SurvivabilitySAE1008A (Current)5/15/2026
According to SAE6906, Force Protection and Survivability (FPS) is the Human Systems Integration (HSI) domain that facilitates system operation and personnel safety during and after exposure to hostile situations or environments. Force protection refers to all preventive measures taken to mitigate hostile actions against Department of Defense (DoD) and Department of Homeland Security (DHS) (e.g., U.S. Coast Guard, Customs and Border Patrol, Immigration and Customs Enforcement, etc.) personnel. Survivability denotes the capability of the system and/or personnel manning the system to avoid or withstand man-made hostile environments without suffering an abortive impairment of his/her ability to accomplish its designated mission. Damage due to enemy or fratricidal action, or even equipment failure, will endanger the warfighters' well-being and place them into a life-threatening situation.
G-45 Human Systems Integration
Aluminum Alloy, Castings, 5.0Si - 1.2Cu - 0.50Mg (355.0-T51), Precipitation Heat TreatedAMS4210N (Current)4/24/2026
This specification covers an aluminum alloy in the form of castings (see 8.6).
AMS D Nonferrous Alloys Committee
Aluminum Alloy Castings, 7.0Si - 0.58Mg - 0.15Ti - 0.06Be (D357.0-T6), Solution and Precipitation Heat Treated, Dendrite Arm Spacing (DAS) ControlledAMS4241F (Current)4/24/2026
This specification covers an aluminum alloy in the form of castings.
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Clad One Side Sheet, 0.6Mg - 0.35Si - 0.28Cu (No. 23 Brazing Sheet), As FabricatedAMS4465C (Current)4/26/2026
This specification covers an aluminum alloy in the form of sheet, clad on one side.
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Clad Two Sides Sheet, 0.6Mg - 0.35Si - 0.28Cu (No. 24 Brazing Sheet), As FabricatedAMS4460C (Current)4/30/2026
This specification covers an aluminum alloy in the form of sheet, clad on two sides.
AMS D Nonferrous Alloys Committee
Hardness and Conductivity Inspection of Wrought Aluminum Alloy PartsAMS2658E (Current)5/6/2026
This specification establishes hardness and electrical conductivity acceptance criteria for finished or semifinished parts made from wrought aluminum alloys after heat treatment (see 8.6).
AMS D Nonferrous Alloys Committee
SAE Architecture Analysis and Design Language (AADL) Annex Volume 2:Annex B: Data Modeling AnnexAnnex D: Behavior Model AnnexAnnex F: ARINC653 AnnexAS5506/2 (Current)10/10/2025
AS-2C Architecture Analysis and Design Language
Predicting Photometric Degradation of Exterior Aircraft LightsARP6621 (Current)9/15/2025
This Aerospace Recommended Practice provides guidance for designers and specifiers of aircraft exterior lighting. Typical causes of light degradation and methods of predicting performance degradation in the aircraft environment are given. Although the document considers only exterior lighting, many of the principles and methods discussed apply to interior or flight deck lighting as well.
A-20B Exterior Lighting Committee
Procedures for the Sampling and Measurement of Particle Size Distributions from Aircraft Turbine EnginesAIR7382 (Current)11/12/2025
This document, expanding upon AIR6037A, provides technical specifications and operational protocols for instruments commonly used to measure aircraft engine nonvolatile Particulate Matter (nvPM) Particle Size Distributions (PSDs). For each instrument type, its functionality, calibration, uncertainties, and known limitations are discussed to support the development of procedures that help ARP6320B nvPM system operators reliably determine PSDs. Practical setup considerations, such as sample conditioning and instrument positioning, are highlighted, together with guidelines for maintenance, data correction, and quality control to minimize measurement uncertainty.
E-31P Particulate Matter Committee
Sleeving, Identification, Heat Shrinkable, General SpecificationAS6976A (Current)12/16/2025
This SAE Aerospace Standard (AS) establishes the requirements for various types of identification sleeving that will shrink to a predetermined size upon the application of heat after it has been marked using AS23053 sleeves as basis material. This AS does not cover specific carrier configuration.
AE-8D Wire and Cable Committee
WIRE, ELECTRIC, FLUOROPOLYMER-INSULATED, TFE-GLASS-FEP, MEDIUM WEIGHT, SILVER-COATED COPPER CONDUCTOR, 600-VOLTAS22759/4B (Current)11/13/2025
AE-8D Wire and Cable Committee
Architecture Analysis & Design Language (AADL) Annex F: AADL Annex for the FACE™ Technical Standard Edition 3.0AS5506/4 (Current)10/13/2025
AS-2C Architecture Analysis and Design Language
Nitrogen Absorption/Desorption (Gas Dissolution) in Aircraft Shock AbsorbersAIR6942 (Current)8/1/2025
This document outlines the current state of the art in the understanding of gas in solution in shock absorber oils (hydraulic fluid, referred to hereafter as oil or fluid [refer to AIR5358B]) in unseparated shock absorbers. A literature review, overview of Henry’s law, Henry’s law coefficients for known gas and oil couples, in-service operational problems, lessons learned, and potential future work are discussed in the document.
A-5B Gears, Struts and Couplings Committee
Time‐Sensitive Networking for Aerospace Onboard Ethernet CommunicationsIEEE/SAEAS6675 (Current)11/7/2025
This standard specifies profiles of IEEE 802.1 Time-Sensitive Networking (TSN) and IEEE 802.1 Security standards for aerospace onboard bridged IEEE 802.3 Ethernet networks. The profiles select features, options, configurations, defaults, protocols, and procedures of bridges, end stations, and Local Area Networks to build deterministic networks for aerospace onboard communications.
AS-1A Avionic Networks Committee
Pilot Training and Certification for VTOL-Capable AircraftAS7062 (Current)8/1/2025
This standard is intended for use by original equipment manufacturers (OEMs), regulators, operators, training organizations, and any others who wish to develop curricula for pilot, instructor, and evaluator training courses for new aircraft - VCA. Continuous updates to this standard will be necessary to incorporate advancements in VTOL technologies and training methods. This standard describes the knowledge, skills, and attitudes required to safely operate VCA for commercial purposes. A Civil Aviation Authority (CAA) may, at their discretion, use this standard to aid the development of existing or future regulations. OEMs and operators may use this standard to develop a curriculum for acceptance or approval by civil regulators. This standard includes a Pilot Training Program developed to address the theoretical and practical training and assessment for VTOL-capable pilot licensing/certification. Additionally, this standard contains the requirements for pilot training and licensing for the operation of VCA with pilots on board or remotely operated (also called off board). The Pilot Training Program will define on-board pilot training requirements and off-board (or remote pilot) training requirements in a parallel effort to ensure OEMs planning to operate without pilots on board the aircraft have a pathway toward pilot certification and licensing. Future standards will address fully autonomous operations of VCA. Compliance with this document is recommended as one means of assuring the safe operation of VCA under conditions normally encountered in routine aeronautical operations. This standard does not conflict with any regulatory conformity and is not intended to diverge from regulatory policy or guidance. The scope of this document includes standards for the use of flight simulation training devices (FSTD) in support of pilot training and licensing. This standard is intended to facilitate the development of and define the constraints for the effective use of flight simulation to support, augment, or replace in-aircraft flight training and testing in the demonstration of regulatory compliance while ensuring safe operations. These highly automated aircraft operations support a mission-based and performance-based approach to training and testing because current prescriptive training methodology inadequately addresses the needs of these aircraft and pilots. Pilot skills will differ from traditional airplanes and helicopters and need consideration in training program design. Because these aircraft may not have common characteristics, the need for a comprehensive approach to training and testing will initially support the broad scope of these designs. This training is intended to apply to VCA; however, the approach to training for emerging and advanced technologies can be broadly applied to conventional aircraft that incorporate new technologies. In the future, training programs will incorporate AI and machine learning to analyze pilot performance data, personalize training programs, and predict training needs. These technologies support the enhancement and effectiveness of training by providing real-time feedback and adaptive learning environments. The existing regulatory framework does not address specific criteria to meet the needs of pilot training for VCA operations. New and amended regulations must be implemented to safely enable future operations of new transportation modalities with pilots on board, off board, and autonomous operations. Initial licensing of pilots will depend on the availability of previously trained, appropriately qualified, and experienced (commercial airplane and/or helicopter licensed) pilots with additional type-specific training to address the unique distinctions of each VCA. These are highly automated, mostly single pilot operations, leading to remotely operated and future autonomous operations. This standard addresses the criteria necessary for existing commercial pilots, ab initio pilots,1 instructors, examiners, and both on-board and remote pilots who will need to be qualified through training and testing to achieve a type rating in a VCA. The introduction of new aircraft and new pilot licensing and certification supports a departure from traditional training toward a performance-based, competence-based training methodology. Traditional training is designed to ensure pilot candidates demonstrate the necessary minimum skill, knowledge, and experience to meet the qualification requirements for the license, rating, or privilege. The training methodology described in this standard is designed to ensure pilot candidates possess the required competencies to perform their assigned duties and responsibilities while operating the aircraft safely, efficiently, and effectively. This standard measures competence by evaluating total performance rather than singular tasks. This standard describes performance- and competence-based training that: Enables individuals to reach a level of safe operational capability while ensuring a fundamental level of competence as a minimum standard Enables individuals to cope with predictable and unforeseen situations Is relevant to the job and the context in which the job will be performed Is geared toward retaining and applying learning rather than passing a test Makes full use of available training tools and methodologies Supports continuous learning and performance improvement
G-35A Pilot Training and Certification Committee
BEARING, ROLLER, NEEDLE, DOUBLE ROW, HEAVY DUTY, TRACK ROLLER, SEALED, TYPE VI, INCHAS21439E (Current)9/9/2025
ACBG Rolling Element Bearing Committee
Blackening of Steel, Touch-Up MethodAMS2489B (Current)4/1/2026
This specification covers the requirements for an inorganic black coating applied at ambient temperature to steel to touch up black oxide coating in areas where the black oxide has been removed. This coating is intended only to visually change the surface to a black color, not to meet the requirements of any black oxide specification.
AMS B Finishes Processes and Fluids Committee
Semiautomatic Headlamp Beam Switching DevicesJ565_202511 (Current)11/13/2025
This SAE Standard provides test procedures, performance requirements, and guidelines for semiautomatic headlamp beam switching (SHBSD) devices.
Road Illumination Devices Standards Committee
Hose Assembly, Polytetrafluoroethylene, Para-Aramid Reinforced, 3000/4000 psi, 275 °F, Standard Duty, Hydraulic, Aircraft Systems (Supplement 1)AS1975SUP1A (Current)12/1/2025
This supplement forms a part of AS1975, Hose Assembly, Polytetrafluoroethylene, Para-Aramid Reinforced, 3000/4000 psi, 275 °F, Standard Duty, Hydraulic, Aircraft Systems and shall be used to identify hose assembly standards citing this procurement specification.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Steel, Corrosion-Resistant, Investment Castings, 16Cr - 4.1Ni - 0.28Cb - 3.2Cu, Homogenization, Solution, and Precipitation Heat Treated (H900), 180 ksi (1241 MPa) Tensile Strength (17-4)AMS5344H (Current)12/1/2025
This specification covers a corrosion-resistant steel in the form of investment castings homogenized and solution and precipitation heat treated to 180 ksi (1241 MPa) tensile strength.
AMS F Corrosion and Heat Resistant Alloys Committee
Desmutter, Aluminum LiquidAMS1626D (Current)3/1/2026
This specification covers materials in the form of a liquid used to remove smut from aluminum surfaces treated with etch-type oxidation and corrosion removers.
AMS J Aircraft Maintenance Chemicals and Materials Committee
Aluminum Alloy Sheet, 1.0Mg - 0.8Si - 0.8Cu - 0.5Mn (6013-T4), Solution Heat Treated and Naturally AgedAMS4347F (Current)4/1/2026
This specification covers an aluminum alloy in the form of sheet from 0.020 to 0.249 inch (0.51 to 6.32 mm), inclusive, in thickness (see 8.6).
AMS D Nonferrous Alloys Committee
TERMINATION, SOLDER STYLE, INSULATED, HEAT-SHRINKABLE, ENVIRONMENT RESISTANT WITH MULTIPLE OPENING SEALANT, 150 °C AND 200 °CAS83519/4A (Current)1/1/2026
AE-8C2 Terminating Devices and Tooling Committee
Color-Coded Incandescent Flange Base T-1 and T-1 3/4 Lamps for Voltage IdentificationAS4156D (Current)12/1/2025
This document specifies that black is the only color that can be used for the insulator at the bottom of the base of T-1 and T-1 ¾ Flanged Base lamps.
A-20A Crew Station Lighting
High Mounted Stop and Turn Signal Lamp for Use on Vehicles 2032 mm or More in Overall WidthJ1432_202602 (Current)3/23/2026
This SAE Recommended Practice provides test procedures, requirements, and guidelines for high-mounted stop lamps and high-mounted turn signal lamps intended for use on vehicles 2032 mm or more in overall width. This document applies to trucks, motor coaches, van type trailers, and other vehicles with permanent structure greater than 2800 mm high. This document does not apply to school buses, truck tractors, pole trailers, flat-bed trailers, pick-up trucks with dual wheels, and trailer converter dollies. The purpose of the high-mounted stop lamp(s) and high-mounted turn signal lamp(s) is to provide a signal to the driver of following (approaching a signaling vehicle from the rear) or oncoming (approaching a signaling vehicle from the front) vehicles over intervening vehicles.
Heavy Duty Lighting Standards Committee
Materials for Use in Optical Parts Such as Lenses and Reflex Reflectors of Motor Vehicle Lighting DevicesJ576_202601 (Current)1/1/2026
This SAE Recommended Practice is intended as a guide toward standard practice and is subject to change to keep pace with experience and technical advances. This document establishes additional performance requirements and provides test methods and requirements to evaluate the suitability of materials intended for optical applications in motor vehicles. The tests are intended to determine physical and optical characteristics of the materials only. Performance expectations of finished assemblies, including plastic components, are to be based on tests for lighting devices, as specified in SAE Standards and Recommended Practices for motor vehicle lighting equipment. Glass and materials inclusive to the light source are not in scope for this method.
Lighting Materials Standards Committee
Methyl Propyl KetoneAMS7297 (Current)4/1/2026
This specification establishes the physical and chemical characteristics for two grades of Methyl Propyl Ketone (MPK) solvent. MPK is also known as 2-Pentanone and Pentan-2-one.
AMS G9 Aerospace Sealing Committee
HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE CRES BRAID REINFORCED, 400 °F, 5080 PSI FLARELESS, 90° ELBOW TO 90° ELBOWAS5966C (Current)12/1/2025
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
CONNECTOR ACCESSORIES, ELECTRICAL, BACKSHELL, REPOSITIONABLE TO STRAIGHT, 45° AND 90°, ENVIRONMENTAL, CABLE SEALING, SHIELD TERMINATION, CATEGORY 1A, (FOR MIL-DTL-83723 SERIES III, AS50151 CRIMP, AS81703 SERIES 3, MIL-DTL-26482 SERIES 2, AND AS95234 CONNECTORS)AS85049/150B (Current)12/1/2025
AE-8C1 Connectors Committee
Standard Exposed Junction Thermocouple for Controlled Conduction Errors in Measurement of Air or Exhaust Gas TemperatureARP690A (Current)4/1/2026
The thermocouple design recommended herein is presented as one for which the correction to the observed emf, because of thermal conduction along the stem and wires, is within the limits presented in the accompanying figure. On referring to the figure, it is seen that no restriction is placed upon the diameter of the thermocouple or stem, and the longitudinal dimensions are expressed in terms of wire and stem diameters. The type of stem, such as packed ceramic stock, refractory insulating tubing, etc., also is left open to choice. Thus the sizes of wires and supporting stems may be varied over wide ranges to match particular requirements where conduction errors are to be limited or controlled.
E-32 Aerospace Propulsion Systems Health Management
Low Voltage Primary CableJ1128_202508 (Current)8/22/2025
This SAE Standard covers low voltage primary cable intended for use at a nominal system voltage of 60 VDC (25 VAC) or less in surface vehicle electrical systems. The tests are intended to qualify cables for normal applications with limited exposure to fluids and physical abuse.
Cable Standards Committee
Nickel Alloy, Corrosion- and Heat-Resistant, Powder for Additive Manufacturing, 50Ni - 20Co - 17Cr - 3.1W - 2.3Ti - 2.1Al - 2.1Mo - 1.8Cb(Nb) - 1.5Ta - 0.04C - 0.005BAMS7075 (Current)1/1/2026
This specification covers a corrosion- and heat-resistant nickel alloy in the form of pre-alloyed powder.
AMS AM Additive Manufacturing Metals
Cobalt Alloy, Corrosion- and Heat-Resistant, Bars, Forging Stock, Forgings, and Rings, 52Co - 20Cr - 10Ni - 15W (L-605)AMS5759P (Current)4/1/2026
This specification covers a corrosion- and heat-resistant cobalt alloy in the form of bars, forgings, flash-welded rings, and stock for forging, flash-welded rings, or heading.
AMS F Corrosion and Heat Resistant Alloys Committee
Alloy, Corrosion- and Heat-Resistant, Bars, Forgings, and Forging Stock, 21Cr - 32.5Ni - 0.38Ti - 0.38Al - 45Fe, (Alloy 800), Solution Heat TreatedAMS5766G (Current)4/1/2026
This specification covers a corrosion- and heat-resistant iron-nickel-chromium alloy in the form of bars and forgings 4.0 inches (102 mm) and under and forging stock of any size.
AMS F Corrosion and Heat Resistant Alloys Committee
Aircraft Position LightsAS271B (Current)12/1/2025
This specification covers three types of aircraft position lights.
A-20B Exterior Lighting Committee
BAND INSTALLATION TOOL, HAND, ONE-STEP, FOR AS85049/128 CONNECTOR ACCESSORY CABLE SHIELD TERMINATING BANDSAS81306/1D (Current)1/1/2026
AE-8C2 Terminating Devices and Tooling Committee
TERMINAL JUNCTION SYSTEM, TERMINAL JUNCTION BLOCKS, SECTIONAL, WIRE IN-LINE JUNCTIONS, SINGLE, SERIES IAS81714/11C (Current)1/1/2026
AE-8C2 Terminating Devices and Tooling Committee
Failure Mode and Effects Analysis (FMEA) Includes Criticality Analysis and Design, Supportability, Software, and Process FMEASAE1025 (Current)1/1/2026
FMEA is a systematic approach aimed at identifying and mitigating potential risks in the design, manufacture, and maintenance of a product. Implementing FMEA provides a range of benefits, such as: Preventing potential failures early in the life cycle. Identifying risk - establishing clear linkages ensures that no potential failure mode is overlooked across the life cycle of the product. Improving product safety, reliability, performance, and supportability. Enhancing collaboration - the framework fosters cross-functional communication, enabling design, manufacturing, and maintenance teams to work in harmony. Achieving effectiveness - by integrating analyses and plans, organizations can streamline workflows and reduce redundancies. Reducing costs associated with product failures. Enhancing customer satisfaction through consistent quality and reliability. Improving product quality - comprehensive linkage reduces errors and ensures a robust design and manufacturing process. Providing the basis for developing product support requirements through supportability analysis FMEA is versatile and shall be applied across various dimensions of product and process management. This standard provides terms, definitions, defined data elements, and essential information within each category of FMEA. The are many types of FMEA, but the primary types defined in this standard include: DFMEA: Focuses product design deficiencies during the design phase of a product and is updated based on product design changes throughout the life of the product design. SwFMEA: Addresses risks and issues specific to software during the design phase of a product and is updated based on software changes throughout the life of the product design. SupFMEA: Evaluates factors affecting product support and maintenance during the design phase of a product and is updated throughout the life of the product design. PFMEA: Concentrates on manufacturing and operational processes to identify and mitigate risks during the design phase of a product and is updated based on product or process changes throughout the life of the product design. Quantitative Criticality Analysis: Focuses on determining the risk of failure based on calculated or estimated failure rates. An essential part of the FMEA process is to identify and communicate potential issues that need to be addressed. When significant risks are discovered, it is incumbent on the FMEA team to communicate quickly to key stakeholders so that the project team can address as soon as feasible and not wait until the contracted deliverable is completed. FMEA is a dynamic and living process, the result of which is improved designs, manufacturing processes, and supportability, not forms or databases that are filled out. This standard applies to any product, process, or software in all phases of their life cycle. As a standard, this document contains requirements (“shall”) and recommendations (“should”) to guide the user through FMEA methods.
G-41 Reliability
Interior DoorsARP499D (Current)1/27/2026
The purpose of this SAE Aerospace Recommended Practice (ARP) is to provide recommendations which will lead to the standardization of interior door design and operation in all transport aircraft. Interior doors are broadly classified into two main categories which include egress path doors and non-egress path doors. The scope of this ARP does not include crew rest doors, secondary barriers to the flight deck, or doors incorporated in furniture surrounding passenger seats as defined in AS6960.
S-9B Cabin Interiors and Furnishings Committee
CONNECTORS, PLUG, ELECTRIC, 45° ASSEMBLY, CRIMP CONTACT, AN TYPEAS34091B (Current)12/1/2025
AE-8C1 Connectors Committee
Guidelines and Procedures for Horizontal Directional Drilling (HDD) Machine Tracking Equipment OperatorsJ2519_202601 (Current)1/1/2026
These general guidelines and precautions apply to personnel operating directional drilling tracking equipment when used with horizontal directional drilling (HDD) machines as defined in ISO 21467:2023.
MTC9, Trenching and Horizontal Earthboring Machines
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