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Test Document 314TESTMARCH14 (Current)
scope
G-41 Reliability
11012024-new-air110124-new-air (Current)
11012024-new-air
A-6 Aerospace Actuation, Control and Fluid Power Systems
Test 06 on 27-05-2025J270501_202510 (Current)10/13/2025
Test 06 on 27-05-2025
Battery Standards Truck Battery Committee
Hot Impulse Test for Hydraulic Brake Hose AssembliesJ1833_202510 (Current)10/13/2025
test
Automotive Brake and Steering Hose Standards Comm
Test Publishing DocumentARP090824B (Current)10/13/2025
Test Publishing Document6667
A-6 Aerospace Actuation, Control and Fluid Power Systems
Sponsor ChjangeARP050911 (Current)10/13/2025
Test
A-6A Systems Subsystem Integration Steering Group
TUBE BENDING RADIUSAS130A (Current)01/02/2013
This standard establishes basic design criteria including preferred bend radii, straight lengths between bends, flattening and surface conditions in the bend area. Also included is a table of preferred tubing sizes and wall thicknesses and a formula for determining a minimum bend radius for a given tube diameter.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Hose Assembly, Polytetrafluoroethylene, Metallic Braid Reinforced, 5080 psi (35,000 kPa), 400°F (204°C), Aircraft Hydraulic Systems (Supplement 1)..AS5960SUP1 (Current)09/24/2012
This supplement forms a part of the Aerospace Standard AS5960, Hose Assembly, Polytrafluoroethyloene, Metallic Braid Reinforced, 5080 psi (35,000 kPa), 400°F (204°C), Aircraft Hydraulic Systems, and shall be used to identify hose assembly standards citing this procurement specification.
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Fitting, Adapter, Port, ReducerAS5172F (Current)09/26/2025
Scope is unavailable.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Wire, Electrical, Fluoropolymer-Insulated, Crosslinked Modified ETFE, Low Fluoride, Normal Weight, 80 Microinch Silver-Coated, High-Strength Copper Alloy, 200 °C, 600 Volt, ROHSAS22759/49C (Current)10/01/2025
SCOPE IS UNAVAILABLE.
AE-8D Wire and Cable Committee
Hydraulic Pump and Motor Mounting and Drive DimensionsJ744_202510 (Current)10/01/2025
This SAE Standard applies to hydraulic pumps and motors used on off-road self-propelled work machines as described in SAE J1116.
CTTC C1, Hydraulic Systems
Terminal Board Assembly, Molded-in-Stud, ElectricAS27212E (Current)09/29/2025
Scope is unavailable.
AE-8C2 Terminating Devices and Tooling Committee
Electrical Interface Between Numerical Control and Machine ToolsEIARS431 (Current)07/01/2015
This standard covers both active and passive aspects of the electrical interface between the Numerical Control (NC) and the machine power and logic control, motor drive equipment, and other electrical apparatus on or associated with the machine tool. It covers:
Systems Management Council
Technical Committee GuidelinesTSB004_201411 (Current)11/04/2014
Executive Standards Committee
BOLT, MACHINE-DOUBLE HEX EXTENDED WASHER HEAD, CLOSE TOLERANCE SHANK, CORROSION RESISTANT STEEL (UNS S17400), 140 KSI UTS MIN, .1900-32, UNJF-3AAS3167B (Current)03/09/2020
E-25 General Standards for Aerospace and Propulsion Systems
Rules for SAE Use of SI (Metric) UnitsTSB003_199905 (Current)05/01/1999
This SAE Standard provides information on the International System of Units (abbreviated SI in all languages), and its application in measurement unit usage.
Executive Standards Committee
Grease, Aircraft, General Purpose, Low Temperature Range, Lithium ThickenedAMS3052B (Current)09/30/2025
Committee AMS-M is establishing an Industry Managed Qualification Program through the remit of the Performance Review Institute which requires this specification to be revised to reference the qualification process and controlling documentation.
AMS M Aerospace Greases Committee
Loss Budget Specification for Fiber Optic LinksAS5750B (Current)10/01/2025
This document defines a quantified means of specifying a digital fiber optic link loss budget: - Between end users and system integrators - Between system integrators and subsystem suppliers - Between subsystem suppliers and component vendors The standard specifies methods and the margin required for categories of links.
AS-3 Fiber Optics and Applied Photonics Committee
O-Ring Machined from AMS3650 MaterialAS9770A (Current)01/03/2020
This standard establishes the dimensional and visual quality requirements, lot requirements, and packaging and labeling requirements for O-rings machined from AMS3650 material. It shall be used for procurement purposes.
A-6C2 Seals Committee
Two-Speed Propeller Reduction Gear ControlAS178 (Current)05/01/1995
This standard is supplementary to AS 41 'Propeller Shaft Ends, Single Rotation', and AS 91 'Propeller Shaft Ends, Dual Rotation (Propeller Supplied Bearing)'. It is applicable to all engines that incorporate two-speed propeller reduction gears.
E-25 General Standards for Aerospace and Propulsion Systems
Billets and Preforms, 5Al 2Sn 2Zr 4Cr 4Mo 0.10O₂, Premium Quality, Powder-Metallurgy ProductAMS4995B (Current)02/01/1998
This specification covers a premium-quality, titanium alloy powder-metallurgy product in the form of billets and preforms for forgings.
AMS G Titanium and Refractory Metals Committee
DRIVES - SQUARE FLANGE .600 PD SPLINE ACCESSORYARP365B (Current)02/05/2013
E-25 General Standards for Aerospace and Propulsion Systems
Quality Program Guidelines for Deicing/Anti-Icing of Aircraft on the GroundARP5646A (Current)06/19/2019
The scope of the Quality Program Guidelines, in the format of a checklist, is to help ensure compliance with the current documents as listed in §2 "Applicable Documents " that meet Airline Operator's and regulatory requirements. It is the responsibility of all other personnel that performs the deicing/anti-icing task to adhere to these requirements.
G-12T Training and Quality Programs Committee
Propeller Control Installation ClearanceARP244B (Current)02/05/2013
E-25 General Standards for Aerospace and Propulsion Systems
Alloy Castings, Investment, Corrosion and Heat Resistant 65.5Co - 25Cr - 1.8Ni - 5.0W As CastAMS5375F (Current)03/07/2007
This specification covers a corrosion and heat resistant cobalt alloy in the form of investment castings.
AMS F Corrosion Heat Resistant Alloys Committee
Diglycidyl Ester ResinAMS3296 (Current)10/01/1995
AMS P Polymeric Materials Committee
Reducers, Pneumatic Pressure, MissileAS1297B (Current)10/06/2014
The complete specification for a pneumatic pressure reducer for high pressure pneumatic systems used in missiles comprises: (1) this standard, which includes many of the general performance requirements, (2) a detailed procurement specification describing envelope and operating conditions, and (3) the "Pneumatic Components, Aeronautical - General Specification For - MIL-P-8564" which covers general requirements common to all components for use in high pressure pneumatic systems.
A-6C5 Components Committee
R-1234yf (HFO-1234yf) Recovery/Recycling/Recharging Equipment for Flammable Refrigerants for Mobile Air-Conditioning SystemsJ2843_201907 (Current)07/15/2019
This SAE Standard applies to equipment to be used with R-1234yf refrigerant only. It establishes requirements for equipment used to recharge R-1234yf to an accuracy level that meets Section 9 of this document and purity levels defined in SAE J2099. Refrigerant service equipment is required to ensure adequate refrigerant recovery to reduce emissions and provide for accurate recharging of mobile air conditioning systems. Equipment shall be certified to meet all performance requirements outlined in this document and international/regional construction and safety requirements as outlined in this document.
Interior Climate Control Service Committee
CONNECTOR ACCESSORIES, ELECTRICAL, STRAIN RELIEF, 90°, SELF-LOCKING AND NON-SELF-LOCKING, CATEGORY 4C (FOR MIL-DTL-38999 SERIES III AND IV CONNECTORS)AS85049/39C (Current)09/23/2014
AE-8C1 Connectors Committee
CONNECTOR, PLUG, ELECTRIC, SOLDER CONTACT, UTILITYAS34361A (Current)03/09/2017
AE-8C1 Connectors Committee
Cockpit Display of Data Linked Weather InformationARP5740 (Current)01/12/2015
This SAE Aerospace Recommended Practice (ARP) addresses the information content for the electronic presentation of data linked weather Meteorological (MET) information used in the cockpit. It defines guidelines for the electronic presentation of MET information (including text, graphics, textures, icons, and symbology) to the flight crew. This ARP is applicable to certified equipment for the electronic display (whether installed or portable) of MET information in the cockpit. This ARP also provides a set of symbols that illustrate the depiction of data linked MET information on flight deck display systems such as Navigation Displays, Multi-function Displays, and Electronic Flight Bags. These recommendations complement standard symbology guidelines for airborne applications already in existence (see reference section for applicable documents).
G-10 W Weather Information Systems Committee
Standardization of Drive End of Hydraulic or Geared Torque Wrenches for Use to an Upper Limit of 500,000 inch poundsARP1135B (Current)12/05/2012
This SAE Aerospace Recommended Practice (ARP) covers the dimensions of an inside splined driver-wrench adapter, envelope of the housing-wrench reaction, the mechanical method of adapting the driver-wrench adapter to the wrench adapter driven end, and the housing-wrench reaction to the holder-counter torque.
AGE-4 Packaging, Handling and Transportability Committee
SCREW - FLAT FILLISTER, DRILLED HEAD, CADMIUM PLATED, STEEL UNS G87400, 125 KSI MIN .3125-18 UNC-3AAS115951C (Current)07/08/2014
E-25 General Standards for Aerospace and Propulsion Systems
Tolerances, Metric, Corrosion and Heat Resistant Steel, Iron Alloy, Titanium, and Titanium Alloy Sheet, Strip, and PlateMAM2242D (Current)09/13/2007
This specification covers established manufacturing tolerances applicable to sheet, strip, and plate of corrosion and heat resistant steels, iron alloys, titanium, and titanium alloys ordered to metric dimensions. These tolerances apply to all conditions, unless otherwise noted. The term 'excl' is used to apply only to the higher figure of the specified range.
AMS F Corrosion Heat Resistant Alloys Committee
Design Guidelines for Fiberboard MaterialsJ1774_201909 (Current)09/25/2019
This document provides information on the various fiberboard products, which are available for automotive application. It is intended to give engineers and designers a better understanding of product usage, characteristics, properties and industry terminology. The following sections cover these topics: 2 General Product Information 3 Design Characteristics 4 Physical/Mechanical Properties 5 Fiberboard Definitions In sections 2, 3 and 4 the fiberboard products are categorized. These sections give an overview of product types, with general information about characteristics and properties. In cases where product categories encompass more than one material or material grade, ranges were established to cover all of the products in that category. The individual companies that supply fiberboard products should be consulted for specific information about a particular product or application.
Textile and Flexible Plastics Committee
National Aerospace and Defense Contractors Accreditation Program Requirements for Elastomer SealsAS7115A (Current)06/19/2017
This document has been declared "CANCELLED" as of June 2017 and has been superseded by PRI AC7115. By this action, this document will remain listed in the Numerical Section of the Aerospace Standards Index noting that it is superseded by PRI AC7115. Cancelled specifications are available from SAE.
Nadcap Management Council
Passenger Car Side Door Latch SystemsJ839_201910 (Current)10/09/2019
This SAE Recommended Practice establishes minimum performance requirements and test procedures for evaluating and testing passenger car side door latch systems. It is limited to tests that can be conducted on uniform test fixtures and equipment in commercially available laboratory test facilities. The test procedures and minimum performance requirements outlined in this document are based on currently available engineering data. It is intended that all portions of the document will be periodically reviewed and revised, as additional knowledge regarding vehicle latch performance under impact conditions is developed.
Motor Vehicle Council
Human Factors Minimum Requirements and Recommendations for the Flight Deck Display of Data Linked Notices to Airmen (NOTAMs)ARP6467 (Current)02/13/2014
This SAE Aerospace Recommended Practice (ARP) includes the minimum human factors requirements and recommendations for the flight deck display of data linked Aeronautical Information (AI), specifically Notices to Airmen (NOTAMs). The goal of human factors is to make it easy for users to do things right and hard to do them wrong. The guidance in this ARP supports this goal by defining minimum requirements and recommendations that focus on the text and potential graphics for NOTAMs as well as the human’s interaction with these on the flight deck. In this ARP “flight deck” includes both single pilot flight decks as well as multi-pilot flight decks. The FAA defines NOTAMs1 as any information concerning the establishment, condition, or change in any component of, or hazard to, the National Airspace System. ICAO Annex 15 defines a NOTAM as “a notice distributed by means of telecommunication containing information concerning the establishment, condition, or change in any aeronautical facility
G-10A Aeronautical Information System Committee
Automotive V-Ribbed Belt Drives and Test MethodsJ1596_201909 (Current)09/24/2019
The following information covers engine accessory drive layout details and testing methods and includes test configurations, pulley diameters, power loads, and guidance for interpreting test data. This information has been prepared from existing literature, including standards and data supplied by both producers and users of V-ribbed belts.
Belt Drive (Automotive) Systems Committee
Foam, Flexible Polyurethane (Pur) Open Pore, Polyvinylchloride(Pvc) CoatedAMS3569 (Current)10/01/1995
AMS P Polymeric Materials Committee
Steel Bars, Forgings, and Tubing, 1.0Cr (0.98 - 1.10C) (SAE 51100), Consumable Electrode Vacuum MeltedAMS6443G (Current)09/22/2005
TThis specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
AMS E Carbon and Low Alloy Steels Committee
Recommended Test Fluids for Electrical Components Used on Aircraft Exterior or for Ground Support Near AircraftARP5062A (Current)11/21/2012
The purpose of this SAE Aerospace Recommended Practice (ARP) is to provide recommended test fluids for testing of electrical components used on aircraft exterior or for ground support near aircraft. These fluids were selected based on a consolidation of test fluids used by military and commercial sources and on review of national and international component specifications. These recommendations are general guidelines. Safety factors for any unusual testing applications or operating conditions should be given special consideration by the designer. The test fluids provided are intended to be recommendations and are not intended to limit or supersede those recommended by aircraft or ground support equipment manufacturers.
AE-8A Elec Wiring and Fiber Optic Interconnect Sys Install
Comparison of Hydraulic System Cleanliness Procedures and Requirements for Ten Aerospace CompaniesAIR1918A (Current)12/13/2013
A-6C1 Contamination and Filtration Committee
Aircraft Jacking Pads Adapters and Sockets Design and Installation ofAS8091A (Current)03/29/2019
This SAE Aerospace Standard (AS) provides requirements for design and installation of aircraft jacking pad adapters and the mating jack socket interface to permit use of standard jacking equipment to be used in civil and military transport aircraft. The adapter defined herein shall be the key interface between the aircraft and the aircraft jack(s).
AGE-3 Aircraft Ground Support Equipment Committee
Life RaftsAS1356 (Current)05/02/2017
This SAE Aerospace Standard (AS) establishes Minimum Performance Standards (MPS) for life rafts carried on board aircraft. This document is not intended to specify particular design methods, mechanisms, or equipment to be used to accomplish the objectives established herein.
S-9A Safety Equipment and Survival Systems Committee
Multiplex Data Bus Networks for MIL-STD-1760 StoresAIR4013C (Current)08/22/2012
This SAE Aerospace Information Report (AIR) will examine network aspects of open and shorted stubs, line reflections and bus loading due to network changes. Single network level is assumed, that is, no carriage store hierarchical levels. However, two passive network coupling variants called "branched bus" and "branched stub" will be introduced that possibly could be used in a stores management network. This report assumes familiarity with MIL-STD-1553B.
AS-1B Aircraft Store Integration Committee
STUD, SHOULDERED, STEPPED, HEX, WRENCHING, STEEL UNS G87400, CADMIUM PLATED, 125 KSI MIN, .2500-28 UNF-3A X .3125-24 UNF-3AAS9306C (Current)08/20/2014
E-25 General Standards for Aerospace and Propulsion Systems
Test Cell InstrumentationAIR5026B (Current)10/21/2020
This document discusses, in broad general terms, typical present instrumentation practice for post-overhaul gas turbine engine testing. Production engine testing and engine development work are outside the scope of this document as they will typically use many more channels of instrumentation, and in most cases will have requirements for measurements that are never made in post-overhaul testing, such as fan airflow measurements, or strain measurements on compressor blades. The specifications for each parameter to be measured, in terms of measurement range and measurement accuracy, are established by the engine manufacturers. Each test cell instrument system should meet or exceed those requirements. Furthermore, each instrument system should be recalibrated regularly, to ensure that it is still performing correctly.
EG-1E Gas Turbine Test Facilities and Equipment
Fine Wire Mesh for Filter ElementsAIR888C (Current)09/24/2012
This SAE Aerospace Information Report (AIR) discusses the terminology, types, method of manufacture and chemistry of the fine wire meshes used for filtration of hydraulic, lubrication fuel systems, and similar applications. Information contained herein may be used for quality assurance testing to insure that a high performance filter grade wire mesh is acceptable for use in an aerospace application.
A-6C1 Contamination and Filtration Committee
FITTING, BUSHING-SCREW THREAD EXPANDER FOR SEAL RINGAS4308C (Current)02/10/2015
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
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