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Nickel Alloy, Corrosion and Heat-Resistant, Investment Castings 52.5Ni - 19Cr - 3.0Mo - 5.1Cb(Nb) - 0.90Ti - 0.60Al - 18Fe Vacuum Melted Homogenization and Solution Heat TreatedAMS5383F (Current)11/3/2023
This specification covers a corrosion and heat-resistant nickel alloy in the form of investment castings.
AMS F Corrosion and Heat Resistant Alloys Committee
Cloth, Type "E" Glass, "B" Stage Epoxy-Resin-Impregnated 7781 Style Fabric, Flame ResistantAMS3821C (Current)7/6/2015
This specification covers a style 7781 glass cloth impregnated with a heat-curable epoxy resin system, the resin being processed to a "B" stage condition, and furnished in the form of continuous rolls.
AMS P17 Polymer Matrix Composites Committee
Identification Marking of Copper and Copper Base Alloy Mill ProductsAMSSTD185A (Current)3/17/2014
This standard establishes the physical item marking requirements for identification purposes for copper and copper-base alloy mill products procured and issued for government activities. Shipment and inspection acceptance markings are not within the scope of this standard.
AMS D Nonferrous Alloys Committee
Coating, Cadmium (Vacuum Deposited)AMSC8837A (Current)10/22/2015
This specification covers the requirements for three types and three classes for vacuum deposited cadmium coating.
AMS B Finishes Processes and Fluids Committee
Type 7 Virgin Polytetrafluoroethylene (PTFE) Moldings or Extrusions with 25% Carbon and GraphiteAMS3678/7B (Current)2/29/2016
This specification covers a polytetrafluoroethylene (PTFE) resin filled with carbon and graphite in the form of extruded or molded rods or tubes which are sintered after molding or, in the case of extrusions, sintered during the extrusion process.
AMS P Polymeric Materials Committee
Silver Alloy, Brazing Filler Metal 35Ag - 26Cu - 21Zn - 18Cd 1125 to 1295 °F (607 to 702 °C) Solidus-Liquidus RangeAMS4768J (Current)12/8/2015
This specification covers a silver alloy in the form of wire, rod, sheet, strip, foil, pig, powder, shot, and chips and a viscous mixture (paste) of powder in a suitable binder.
AMS D Nonferrous Alloys Committee
Requirements for Development, Implementation and Control of Aerospace Auditor TrainingAIR5493B (Current)7/29/2009
This document has been declared “CANCELLED” as of July 2009 and has been superseded by AS9104/3. By this action, this document will remain listed in the Numerical Section of the Aerospace Standards Index noting that it is superseded by AS9104/3.
G-14 Americas Aerospace Quality Standards Committee (AAQSC)
Supplier Self Verification Process, Delegation ProgramsAS9015A (Current)8/12/2016
This SAE Aerospace Standard (AS) further defines the requirements for a delegation process identified in Aerospace Quality Management System (AQMS) standards (i.e., AS9100, AS9110, AS9120). This standard establishes minimum requirements for the delegation of product verification to an organization's suppliers; outlining requirements for the initial delegation (qualification/selection), maintenance, and removal/withdrawal of delegations.
G-14 Americas Aerospace Quality Standards Committee (AAQSC)
COUPLING BODY, THREADLESS-FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF BONDINGAS5835 (Current)1/9/2013
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
CLAMP, LOOP TYPE, CUSHIONED SUPPORTAS5874 (Current)4/23/2015
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
FITTING END, THREADLESS-FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF BONDING MALE AND FEMALE DESIGN STANDARDAS5836 (Current)1/9/2013
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
Engine Rotation and Cylinder NumberingJ824_202206 (Current)6/29/2022
This SAE Standard was developed to provide a method for indicating the direction of engine rotation and numbering of engine cylinders. The document is intended for use in designing new engines to eliminate the differences which presently exist in industry.
Engine Power Test Code Committee
Off-Road Tire and Rim Selection and ApplicationJ1315_201911 (Current)11/20/2019
This SAE Standard provides general guidelines for the proper selection and application of off-road tires and rims, as defined in SAE J751 and applied to earthmoving machines described in SAE J1116 and ISO 6165.
MTC8, Tire and Rim
Unshielded High Voltage Primary CableJ1654_202107 (Current)7/1/2021
This SAE Standard covers unshielded cable, 22 gauge and larger, intended for use at a nominal system voltage up to 600 V or 1000 V (ACrms or DC). It is intended for use in surface vehicle electrical systems.
Cable Standards Committee
WIRE, THERMOCOUPLE, CROSSLINKED POLYALKENE INSULATED NICKEL/CHROMIUM (KP); NICKEL/ALUMINUM/MANGANESE (KN) THERMOCOUPLE EXTENSION, LIGHT WEIGHT, 150 °CAS5419/4A (Current)12/7/2018
AE-8D Wire and Cable Committee
Ramp MarkingsARP5910A (Current)9/30/2021
This SAE Aerospace Recommended Practice (ARP) outlines recommended ramp pavement marking standards for proper guidance and positioning of GSE on commercial transport aircraft parking and handling stands (gates), in line with International Civil Aviation (ICAO) recommendations applicable to airport aprons. Throughout this document, the minimum essential criteria are identified by use of the key word “shall”. Recommended criteria are identified by use of the key word “should” and, while not mandatory, are considered to be of primary importance in providing safety effective ramp markings. Deviation from recommended criteria should only occur after careful consideration and thorough service evaluation have shown alternate methods to provide an equivalent level of safety.
AGE-3 Aircraft Ground Support Equipment Committee
Silver Alloy Brazing Filler Metal, 56Ag 22Cu 17Zn 5.0Sn, 1152 - 1203°F (622 - 651°C) Solidus-Liquidus RangeAMS2663A (Current)1/1/1992
This specification has been declared "SUPERSEDED" by the Aerospace Materials Division, SAE.
AMS D Nonferrous Alloys Committee
Aluminum Rivets, UNS A91100, 99Al (1100-H14)AS7220A (Current)3/30/2022
This procurement specification covers rivets fabricated from an aluminum alloy designated as 1100-H14, strain hardened.
E-25 General Standards for Aerospace and Propulsion Systems
Determination of Cost Benefits from Implementing a Blockchain SolutionARP6984 (Current)8/19/2021
This SAE Aerospace Recommended Practice (ARP) provides insights on how to perform a Cost Benefit Analysis (CBA) to determine the Return on Investment (ROI) that would result from implementing a blockchain solution to a new or an existing business process. The word “blockchain” refers to a method of documenting when data transactions occur using a distributed ledger with desired immutable qualities. The scope of the current document is on enterprise blockchain which gives the benefit of standardized cryptography, legal enforceability and regulatory compliance. The document analyzes the complexity involved with this technology, lists some of the different approaches that can be used for conducting a CBA, and differentiates its analysis depending on whether the application uses a public or a private distributed network. This document is intended for people who do not have a deep technical understanding or familiarity with blockchain solutions to qualify and quantify its economic benefits
G-31 Digital Transactions for Aerospace
INSERT - THIN WALL, SHORT AND LONG HOLE PREPARATION FORAS3508A (Current)1/31/2026
E-25 General Standards for Aerospace and Propulsion Systems
Airline Tow Tractor - Baggage/Cargo Factors for Design ConsiderationAIR1316C (Current)4/24/2025
This document outlines the functional and design requirements for baggage/cargo tow tractors used for airline services.
AGE-3 Aircraft Ground Support Equipment Committee
HOSE ASSEMBLY, POLYTETRAFLUOROTHYLENE, PARA ARAMID REINFORCED, 275 °F, 4000 PSI MAX, FLARELESS, TITANIUM FITTINGS, STRAIGHT TO 45 DEGREEAS6014B (Current)4/17/2019
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
PIN-LOCK, BRASSAS150301A (Current)7/8/2014
E-25 General Standards for Aerospace and Propulsion Systems
TS95AR-10 Amendment Record for Technical Specification No. TS95TS95AR-10 (Current)2/19/2020
No scope available.
Engine and Airframe Technical Standards Committee (TSC)
NUT, SELF-LOCKING, PLATE, TWO LUG, LOW HEIGHT, UNS S66286, CLASS: 125 KSI/800 °FAS3478E (Current)6/12/2026
E-25 General Standards for Aerospace and Propulsion Systems
Aircraft Wheel Inflation Valves Incorporating an Inflation Pressure GaugeARP5543A (Current)10/26/2020
This specification covers the recommended design, construction, performance and testing requirements for aircraft wheel inflation valves incorporating an inflation pressure gauge which are mounted on the aircraft wheel. These valve/gauge assemblies should be appropriate for use on all aircraft types supported by tubeless tire/wheel assemblies.
A-5C Aircraft Tires Committee
Steel, Corrosion- and Heat-Resistant, Bars, Forgings, and Mechanical Tubing 14.5Cr - 2.3Ni - 12.5Co - 4.0Mo - 0.60V - 0.03Cb(Nb) Carburizing, Premium Aircraft-Quality, Double Vacuum MeltedAMS5932C (Current)11/18/2022
This specification covers a premium aircraft-quality corrosion and heat-resistant steel in the form of bars, forgings, mechanical tubing, and forging stock.
AMS F Corrosion and Heat Resistant Alloys Committee
Titanium Alloy, Investment Castings 6Al - 4V Hot Isostatically PressedAMS4962B (Current)12/6/2016
This specification covers a premium grade titanium alloy in the form of investment castings.
AMS G Titanium and Refractory Metals Committee
Adhesive, Film Form Metallic Structural Sandwich ConstructionAMSA25463 (Current)10/4/2022
This specification covers the requirements for adhesives in film form for bonding metal facings to metal cores and to metal components of sandwich panels which are intended for use in primary and secondary structural airframe parts that may be exposed to temperatures up to 500°F (260°C).
AMS P17 Polymer Matrix Composites Committee
CONTACTS, ELECTRICAL CONNECTOR, SOCKET, CRIMP REMOVABLE, SHIELDED (FOR MIL-DTL-26482 SERIES 1 CONNECTORS)AS39029/26C (Current)2/25/2025
AE-8C1 Connectors Committee
ENGINE OIL PUMP PERFORMANCE AND DURABILITY TEST PROCEDURESUSCAR46 (Current)3/23/2023
SAE/USCAR-46 defines test methods and outputs for engine oil pump bench testing. Performance and durability testing are the primary focus of this standard. This is written to specifically address testing of electronically controlled variable displacement pumps but can be adapted to mechanically controlled pumps and other pump technologies as needed. This standard outlines critical inputs and outputs in order to perform the testing and report results, but does not specifically set the acceptance standards or pass/fail criteria. Acceptance criteria must be set by the customer.
USCAR
Ergonomic Guidelines for Carts and DolliesUSCAR41 (Current)3/13/2015
This document describes the assessment methods and physical requirements associated with the manual handling of carts and dollies, specific to material handling systems. All possible designs and applications could not be anticipated in creating these guidelines. Where there are questions of adherence to this document, such as use of an “off-the shelf” design, always consult the responsible Ergonomics Department. Force guidelines were primarily developed referencing the push/pull psychophysical Snook data contained in A Guide to Manual Materials Handling (second edition) by Mital, Nicholson and Ayoub (NY: Taylor & Francis, 1997). The force guidelines accommodate 75% of female capabilities and 99% of male capabilities. Factors that were included in the established guideline include: push / pull distances, vertical hand height, horizontal hand height, frequency and wheel / castor alignment and load rating. These factors were used to develop a conservative force guideline. The guidelines
USCAR
WIRE, ELECTRICAL, POLYVINYL CHLORIDE INSULATED, POLYAMIDE JACKET, TIN-COATED COPPER CONDUCTOR, MEDIUM WEIGHT, 600-VOLT, 105 °CAS50861/7B (Current)8/19/2025
AE-8D Wire and Cable Committee
Batch Qualification Procedure for Tensile Strength, Elongation and Specific Gravity of Polytetrafluoroethylene (PTFE) Resins, Virgin, Modified, Pigmented and Filled Compounds Used for Compression MoldingAS4720A (Current)11/6/2013
This SAE Aerospace Standard (AS) covers batch qualification procedure for virgin and compounded polytetrafluoroethylene (PTFE) resins used for compression molding. AS9100 requires virgin and modified PTFE as a testing material be representative of production PTFE and/or parts. The testing specified herein is limited to tensile strength, elongation and specific gravity. Any other tests required by the purchaser must be specified separately.
AMS P Polymeric Materials Committee
AS44725 Amendment Record for Drawing Standard No. AS44725AS44725AR-2 (Current)5/1/2017
No Scope available.
Engine and Airframe Technical Standards Committee (TSC)
FITTING ASSEMBLY, STRAIGHT, BULKHEAD FLARELESS, AXIALLY SWAGED, HYDRAULIC, 3000 PSIAS5791B (Current)4/28/2020
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Network End-to-End Data Link Evaluation System Transceiver Health MonitoringAIR6552/3 (Current)12/22/2020
This document establishes methods to obtain, store, and access data about the health of a fiber optic network using commercial sensors located in or near the transceiver. This document is intended for: Managers, Engineers, Contracting Officers, Third Party Maintenance Agencies, and Quality Assurance.
AS-3 Fiber Optics and Applied Photonics Committee
High Speed Network for MIL-STD-1760AS5653B (Current)4/28/2025
AS5653 may be applied to Air Vehicles and Stores implementing MIL-STD-1760 Interface Standard for Aircraft/Store Electrical Interconnection System.
AS-1A Avionic Networks Committee
Automated Data Management GuidelineDMG2 (Current)10/1/2014
This document provides guidance in the developing, managing, controlling and transmitting of data in the current electronic environment.
EIDM Enterprise Information and Data Management
Nadcap Requirements for Diffusion WeldingAS7110/8D (Current)3/6/2007
This document has been declared "CANCELLED" as of March 2007 and has been superseded by PRI AC7110/8. By this action, this document will remain listed in the Numerical Section of the Aerospace Standards Index noting that it is superseded by PRI AC7110/8. Cancelled specifications are available from SAE.
Nadcap Management Council
614 Standard Firmware Loader for Avionics ShopsARINC614 (Current)9/1/1989
This standard describes the characteristics of a standard firmware loader for avionic shops. It is capable of copying digital information into memory devices installed in circuit card assemblies, Line Replaceable Modules (LRMs) and On-Board Replaceable Modules (OBRMs). It contains the recommendations of the air transport community concerning the design and development of firmware loader equipment.
Airlines Electronic Engineering Committee, Avionics Maintenance Committee
606A Guidance for Electrostatic Sensitive Utilization and ProtectionARINC606A (Current)11/1/2004
This document provides guidance for using industry standards for developing an ESD control program tailored to meet specific user requirements. In addition, it provides uniform guidance for maintenance facilities based on industry ESD standards, and therefore should be accepted throughout the air transport industry. This document is not a stand-alone document - it is intended to be used with the referenced international industry standards.
Airlines Electronic Engineering Committee, Avionics Maintenance Committee
608A Design Guidance for Avionics Test Equipment, Part 1 - System DefinitionARINC608A (Current)1/1/1993
This standard is a top-level guidance standard intended for the design of Automatic Test Equipment (ATE). It includes the definition of hardware and software needed for analog and digital signal testing using a Test Unit Adapter common interface. This standard describes the overall ATE system concept as well as the definition of the specific elements of those systems.
Airlines Electronic Engineering Committee, Avionics Maintenance Committee
440 Guidelines for the Provisioning and Support of Training Equipment DataARINC440 (Current)10/1/2005
This document provides guidelines for the aviation industry to ensure that data and solutions for training are adequately provided in content and schedule, are cost effective, and are completely supported throughout the life of the equipment. It should be used at all appropriate levels within a company (e.g., Purchasing, Operations, Training) when purchasing or developing new aircraft, major aircraft modifications or training systems.
Flight Simulator Engineering and Maintenance Committee
Gas Turbine Engine Test Facility Vibration MeasurementARP6068A (Current)12/17/2025
The test procedure per the applicable Engine Manual does require a vibration check for the low/intermediate and high speed rotor systems. Release of an engine with high vibrations can result in: On-wing vibration complaints, with subsequent troubleshooting Rotor system failures Premature engine removals Limits are provided for transient conditions and steady state data points. Troubleshooting recommendations are limited to verification of the proper signal input and tracking. This practice provides recommendations for: Correct cable and transmitter installation and connections Calibration Recorded data interpretation and data analysis
EG-1E Gas Turbine Test Facilities and Equipment
609 Design Guidance for Aircraft Electrical Power SystemsARINC609 (Current)1/1/1987
This standard describes electrical power system design and performance standards brought about by extensive use of digital avionics. This Report provides guide lines for designers of aircraft power system components and of power utilization components, both avionics and power converters such as motors and heaters.
Airlines Electronic Engineering Committee
FITTING END, FLARED TUBE, FOR SEAL RING, STANDARD DIMENSIONS FOR, DESIGN STANDARDAS1098B (Current)10/16/2014
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Steel Bars and Forgings, Corrosion and Heat Resistant 13.5cr 26ni 3mo 1.8tiAMS5733E (Current)1/1/1990
A vendor shall mention this specification number and its revision letter in all quotations and when acknowledging purchase orders. Bars, forgings, and stock for forging or heading. Primarily for parts and assemblies, requiring high strength up to 1250 degrees F (677 degrees C).
AMS F Corrosion and Heat Resistant Alloys Committee
Wire, Electrical, Polyvinyl Chloride Insulated, PVC-Glass-PVC-Nylon, Tin-Coated Copper Conductor, 600-Volt, 105°CAS50861/3A (Current)12/7/2017
AE-8D Wire and Cable Committee
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