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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
Numerical Modeling Techniques for Jet Engine Test Cell AerodynamicsAIR6355 (Current)6/5/2026
This SAE Aerospace Information Report (AIR) has been written for individuals associated with ground level testing of turbofan and turbojet engines, and particularly for those who might be interested in investigating steady-state performance characteristics of a new test cell design or of proposed modifications to an existing test cell by means of numerical modeling and simulation. It is not the intent of this standard to provide specific test cell design recommendations, which are covered in the reference documentation.
EG-1E Gas Turbine Test Facilities and Equipment
BOLT, MACHINE - DOUBLE HEXAGON, EXTENDED WASHER HEAD, CLOSE TOLERANCE SHANK, UNS N07001, 165 KSI, .4375-20 UNJF-3AAS9727A (Current)6/3/2026
E-25 General Standards for Aerospace and Propulsion Systems
BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, PD SHANK, STEEL SAE 8740, CADMIUM PLATED, 125 KSI MIN UTS, .4375-20 UNJF-3AAS9918C (Current)6/3/2026
E-25 General Standards for Aerospace and Propulsion Systems
BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, PD SHANK, CUP WASHER LOCKED, CRES, UNS S66286, 130 KSI MIN, .1900-32 UNJF-3AAS9676C (Current)6/3/2026
E-25 General Standards for Aerospace and Propulsion Systems
Driveline Parking Brake Test Procedure for Medium Duty VehiclesJ2690_202606 (Current)6/3/2026
This SAE Recommended Practice establishes uniform test procedures for friction based parking brake components used in conjunction with hydraulic service braked vehicles with a gross vehicle weight rating greater than 4500 kg (10 000 lb). The components covered in this document are the primary actuation and the foundation park brake. Various peripheral devices such as application dashboard switches or indicators are not included. These test procedures include the following: a Brake Related Tests 1 Brake Functional Performance 2 Brake Dynamic Torque Performance 3 Brake Corrosion Resistance 4 Brake Endurance with Torque 5 Brake Endurance without Torque 6 Vibration Resistance 7 Brake Ultimate Static Load 8 Brake Lining Wear Adjuster Function b Actuation Related Tests 1 Mechanical Actuator Functional Performance 2 Mechanical Actuator Endurance 3 Mechanical Actuator Quick Release 4 Mechanical Actuator Ultimate Load 5 Spring Apply Actuator Functional Performance 6 Spring Apply Actuator
Truck and Bus Hydraulic Brake Committee
WASHER, KEY - 90°, LOCKING, CRES, UNS S32100AS9581D (Current)6/3/2026
E-25 General Standards for Aerospace and Propulsion Systems
Aluminum Alloy, Sheet and Plate 3.5mg 0.25crAMS4018C (Current)1/1/1989
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Sheet and Plate 4.5cu 1.5mg 0.60mn (2024-T36) Width 30 In. and UnderAMS4103 (Current)12/16/2002
AMS D Nonferrous Alloys Committee
Method Selection for Assessment of Nonconforming Levels in Parts Per Million (PPM)EIA554A (Current)9/1/2002
This standard is intended to provide guidance for selecting standardized methods for estimating the proportion nonconforming expressed as PPM. These methods are contained in EIA 554-1, EIA 554-2 and EIA 591.
Systems Management Council
Flange - ThermocoupleARP465C (Current)6/12/2024
This SAE Aerospace Recommended Practice (ARP) provides guidance for the design of flanges on temperature sensors intended for use in gas turbine engines. Three figures detail the configuration of standard size flange mounts with bolt holes, slotted flanges, and miniaturized flanges for small probes.
E-32 Aerospace Propulsion Systems Health Management
SNAP RING - PROPELLER HUB TAPER TYPE - NUMBER 0AS360 (Current)3/1/1962
Columbium (Niobium) Sheet, Strip, and FoilAMS7850F (Current)3/25/2026
This specification covers columbium in the form of sheet, strip, plate, and foil.
AMS G Titanium and Refractory Metals Committee
TechAmerica Technical Fellow and Associate Technical Fellow Nomination and Selection HandbookGEIAOP0003 (Current)4/1/2007
This handbook details the TechAmerica Technical Fellowship Selection Process. It identifies the tasks to be performed and associates them with participants in the process. The focus is intended to keep the process implementation as uniform as possible. There are three types of information in this handbook: Process details Candidate Application Package format Process infrastructure and description Each Section of this handbook describes a significant segment of the selection process. There are also appendices that contain a variety of supporting material relevant to the different process participants.
Systems Management Council
Vehicle, Magnetic Particle Inspection Petroleum BaseAMS2641D (Current)9/12/2025
This specification covers two types of refined hydrocarbon compounds in the form of liquids. This specification only covers newly manufactured materials.
AMS K Non Destructive Methods and Processes Committee
Wheel and Brake (Sand and Permanent Mold) Castings - Minimum Requirements for Aircraft ApplicationsAS586C (Current)1/6/2011
This SAE Aerospace Standard (AS) sets forth the minimum quality required for aircraft wheel and brake castings. Its use will establish minimum acceptable requirements for internal structure and surface conditions and is predicated on the use of a casting factor for the ultimate load of more than 1.51 through 2.00. When casting factors of 1.25 through 1.50 are used, visual, penetrant, and radiographic or other approved equivalent nondestructive inspection methods shall all be required on each production casting. Where specific parts, or areas of parts, require a quality level exceeding that described by this document, the requirements shall be established by negotiation between the purchaser and vendor.
A-5A Wheels, Brakes and Skid Controls Committee
BEARING, ROLLER, NEEDLE-SINGLE ROW, HEAVY DUTY, SELF-ALIGNING, TYPE III, ANTIFRICTION, INCHAS24463E (Current)3/16/2026
ACBG Rolling Element Bearing Committee
Unit Production Cost Tracking Model UPCT 6EDIB1B (Current)8/1/2015
G-47 Systems Engineering
Steel, Corrosion-Resistant, Investment Castings, 16Cr - 1.9Ni - 0.08N (431), As CastAMS5353G (Current)4/12/2026
This specification covers a corrosion-resistant steel in the form of investment castings.
AMS F Corrosion and Heat Resistant Alloys Committee
Beryllium Bars, Rods, Tubing, and Shapes, Instrument GradeAMS7907E (Current)12/10/2024
This specification covers beryllium in the form of bars, rods, tubing, and machined shapes fabricated from vacuum hot-pressed powder.
AMS G Titanium and Refractory Metals Committee
Aluminum Alloy 2014, Bar, Rod, Shapes, Tube, and Wire, ExtrudedAMSQQA200/2B (Current)2/1/2014
This specification covers the specific requirements for aluminum alloy 2014 bar, rod, shapes, tube, and wire produced by extrusion.
AMS D Nonferrous Alloys Committee
CONNECTOR ACCESSORIES, ELECTRICAL, MOUNTING DEVICE, FLANGE TYPE, CATEGORY 7, 1/4 PERIMETERAS85049/96C (Current)4/26/2021
AE-8C1 Connectors Committee
Steel, Welding Wire 1.05Cr - 0.55Ni - 1.0Mo - 0.08V (0.26 - 0.32C) Vacuum Melted, Environment-Controlled PackagingAMS5027H (Current)10/16/2023
This specification covers a low-alloy steel in the form of welding wire.
AMS E Carbon and Low Alloy Steels Committee
Steel Castings, Sand and Centrifugal, Corrosion and Heat Resistant, 18.5Cr - 13.5Ni - 2.1Mo, Solution Heat TreatedAMS5361G (Current)1/10/2019
This specification covers a corrosion and heat-resistant steel in the form of sand or centrifugal castings.
AMS F Corrosion and Heat Resistant Alloys Committee
Cleaner for Aircraft Exterior Surfaces Wipe-On, Wipe-Off, Emulsion-TypeAMS1532D (Current)8/23/2018
This specification covers an emulsion-type cleaner in the form of a liquid.
AMS J Aircraft Maintenance Chemicals and Materials Committee
Electrical Connectors for Aerospace, Shipboard, Ground Vehicles and Associated EquipmentARP1308D (Current)1/21/2020
The intent of this ARP is to identify electrical connectors maintained by the AE-8C1 Committee, to provide their general application characteristics, associated configuration options, and recommendations for new design (see 6.1.1), repair, and retrofit purposes (see 6.1). It is acknowledged the connectors listed herein will not completely satisfy all mobility vehicle and equipment requirements, but optimization of the use of these components will facilitate standardization in the form of maximum utilization of a minimum variety of connectors. This ARP only pertains to AS connector standards. See MIL-STD-1353 for U.S. military specification connector information.
AE-8C1 Connectors Committee
Urea Compound, ShottedAMS1730B (Current)3/1/1994
This specification has been designated as "SUPERSEDED" by the Aerospace Materials Division, SAE, as of May 17, 1993. The requirements of this specification are embodied in the latest issue of AMS 1431.
G-12RDP Runway Deicing Product Committee
INTERRELATION OF ENGINE DESIGN AND BURNER CONFIGURATION WITH SELECTION AND PERFORMANCE OF ELECTRICAL IGNITION SYSTEMS FOR GAS TURBINE ENGINESAIR784C (Current)6/1/1995
To describe typical ignition systems in general usage and their parameters that warrant consideration during the development of a gas turbine engine. To describe those parameters in gas turbine engine design and, in particular, burner configurations that influence the type selection and performance of the ignition system. To indicate the areas where future work may uncover important effects having a direct bearing on certain interrelated parameters, with resultant benefits to both the engine and ignition designers.
E-30 Propulsion Ignition Systems Committee
Bolts and Screws, Steel, UNS S66286 Tensile Strength 130 ksi, Procurement SpecificationAS7477K (Current)12/16/2025
This document covers bolts and screws made from a corrosion- and heat-resistant, precipitation-hardenable, iron base alloy of the type identified under the Unified Numbering System as UNS S66286.
E-25 General Standards for Aerospace and Propulsion Systems
Qualification of Hydraulic Tube Joints to Specified Flexure Fatigue RequirementsARP1258B (Current)1/2/2013
This SAE Aerospace Recommended Practice (ARP) establishes the method for qualification testing of tube joints and fitting attachments, using the flexure test method described in ARP1185. This qualification test method allows the determination of S-N type stress versus cycles or D-N type deflection versus cycles curves, as illustrated in ARP1418 as an alternate to flexture testing to a minimum endurance stress level.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Nickel Alloy, Corrosion- and Heat-Resistant, Investment Castings, 53.3Ni - 16.5Cr - 17Mo - 4.5W - 5.8Fe - 0.40V (CW-12MW), As-CastAMS5388L (Current)9/12/2025
This specification covers a corrosion- and heat-resistant nickel alloy in the form of investment castings.
AMS F Corrosion and Heat Resistant Alloys Committee
Steel, Corrosion- and Heat-Resistant, Welding Wire 20.5Cr - 9.0Ni - 0.50Mo - 1.5W - 1.2Cb - 0.20Ti Vacuum Induction MeltedAMS5782J (Current)4/1/2024
This specification covers a corrosion- and heat-resistant steel in the form of welding wire.
AMS F Corrosion and Heat Resistant Alloys Committee
ALUMINUM ALLOY WELDING WIRE 5.0Si - 1.2Cu - 0.50Mg (C355.0)AMS4188/3 (Current)12/16/2002
This specification covers an aluminum alloy in the form of extruded or drawn welding wire.
AMS D Nonferrous Alloys Committee
EQUIPMENT FRAGILITY DATAARP467 (Current)5/1/1975
Cover - Engine Accessory Drive, Round, 10.000 Bolt Circle, AMS4490 (UNS M11910)AS3225D (Current)4/28/2018
E-25 General Standards for Aerospace and Propulsion Systems
Steel, Mechanical Tubing 0.95Cr - 0.20Mo (0.38 - 0.43C) (SAE 4140)AMS6381K (Current)11/2/2022
This specification covers an aircraft-quality, low-alloy steel in the form of mechanical tubing.
AMS E Carbon and Low Alloy Steels Committee
Titanium Alloy Sheet, Strip, and Plate 3Al - 8V - 6Cr - 4Mo - 4Zr Solution Heat TreatedAMS4939D (Current)5/16/2022
This specification covers a titanium alloy in the form of sheet, strip, and plate through 4.000 inches (101.60 mm) nominal thickness.
AMS G Titanium and Refractory Metals Committee
Flexure Testing of Hydraulic Tubing Joints and FittingsARP1185C (Current)4/23/2019
This SAE Aerospace Recommended Practice (ARP) establishes flexure test procedures to determine and classify the fatigue strengths of reconnectable or permanent hydraulic tube joints. The procedure is intended for conducting flexure tests of fittings and joints for hydraulic tubing materials such as AMS 5561 (21Cr-6Ni-9Mn) steel or AMS 4944 (3AL-2.5V) titanium. A mean stress is applied by holding system pressure in the specimens and flexing in a rotary or planar bending test machine.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Nickel Alloy, Corrosion- and Heat-Resistant, Investment Castings 62Ni - 21.5Cr - 9.0Mo - 3.6Cb (Nb) Vacuum Melted, Vacuum Cast As CastAMS5401C (Current)5/16/2023
This specification covers a corrosion and heat-resistant, vacuum melted, nickel alloy in the form of investment castings.
AMS F Corrosion and Heat Resistant Alloys Committee
Steel, Corrosion-Resistant, Investment Castings 16Cr - 4.1Ni - 0.28Cb - 3.2Cu Homogenization and Solution Heat Treated or Homogenization, Solution, and Precipitation Heat TreatedAMS5355J (Current)11/18/2022
This specification covers a corrosion resistant steel in the form of investment castings.
AMS F Corrosion and Heat Resistant Alloys Committee
Steel Castings, Sand, Corrosion and Heat Resistant, 15cr 4.0ni 2.3mo 0.08n, Solution Heat TreatedAMS5359E (Current)3/7/2007
This specification covers a corrosion and heat resistant steel in the form of sand castings.
AMS F Corrosion and Heat Resistant Alloys Committee
Steel, Corrosion- and Heat-Resistant, Sheet, Strip, and Plate, 13Cr - 2.0Ni - 3.0W (Greek Ascoloy), AnnealedAMS5508H (Current)10/15/2025
This specification covers a corrosion- and heat-resistant steel in the form of sheet, strip, and plate.
AMS F Corrosion and Heat Resistant Alloys Committee
Steel Castings, Sand, 0.80cr 1.8ni 0.35mo (0.28-0.36c) AnnealedAMS5329F (Current)7/1/2001
This specification has been declared "NONCURRENT" by the Aerospace Materials Division, SAE, as of January 1995. It is recommended, therefore, that this specification not be specified for new designs.
AMS E Carbon and Low Alloy Steels Committee
Corrosion Removing Compound for Aircraft SurfacesAMS1640D (Current)2/12/2024
This specification establishes requirements for a corrosion-removing compound in the form of a liquid concentrate.
AMS J Aircraft Maintenance Chemicals and Materials Committee
Cleaner, Water Base, Aircraft interior Hard Surface MaterialsAMS1550B (Current)2/23/2012
This specification covers a water-base cleaner in the form of a concentrated liquid.
AMS J Aircraft Maintenance Chemicals and Materials Committee
Liquid Filter Ratings, Parameters and TestsAIR887C (Current)4/29/2021
This SAE Aerospace Information Report (AIR) identifies and explains the meaning of various ratings and terms used to describe the physical characteristics of liquid filter elements. The significance of various filter parameters is discussed. In addition, a number of filter test methods are briefly described. This AIR and the data presented are only applicable where the system liquid wets the filter elements.
A-6C1 Fluids and Contamination Control Committee
Remover, Anti-Galling Compound Aircraft Turbine Engine Components Room Temperature ApplicationAMS1387B (Current)11/26/2018
This specification covers an anti-galling compound remover in the form of a water-soluble powder, a concentrated liquid for dilution with water, or a ready-to-use liquid.
AMS J Aircraft Maintenance Chemicals and Materials Committee
PULLER - IMPACT - UNIVERSALAS356 (Current)2/1/1958
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