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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
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
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
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
Steel, Corrosion-Resistant, Wire, 18Cr - 9.0Ni (302), Spring TemperAMS5688N (Current)6/1/2026
This specification covers a corrosion-resistant steel in the form of wire.
AMS F Corrosion and Heat Resistant Alloys Committee
Functional, Performance, and Safety Guidelines for Tire Pressure Monitoring Systems (TPMS) for AircraftARP6137A (Current)6/1/2026
This SAE Aerospace Recommended Practice (ARP) establishes the overall component and system function guidelines and minimum performance levels for a TPMS. These guidelines include, but are not limited to: Design recommendations for system components, which: Monitor tire inflation Are located in/on the tire/wheel assembly, landing gear axle, and/or aircraft avionics compartment Recommended performance and safety guidelines for a TPMS.
A-5 Aerospace Landing Gear Systems Committee
Time-Triggered EthernetAS6802A (Current)2/14/2023
This SAE Aerospace Standard (AS) defines a fault-tolerant synchronization strategy for building and maintaining synchronized time in a distributed system of end systems and switches (we use the term “end system” for data terminal equipment (DTE), as specified in IEEE 802.3), which can be used to support communication among these components for traffic, which may have different levels of time criticality. In particular, the standard defines algorithms for clock synchronization, clique detection, startup, and restart. These algorithms have been designed to allow scalable fault-tolerance and provide self-stabilization mechanisms. Time-triggered Ethernet supports the design of communication systems with mixed time criticality in which several applications of mixed time criticality share a single physical network. In particular, an Ethernet network can be used to transfer frames in a time-triggered mode (synchronous communication) and non-time-triggered modes (asynchronous communication as
AS-2D2 Deterministic Ethernet and Unified Networking
Manufacturing Management Program Standard + ChecklistAS6500A_CKLST (Current)9/27/2022
This compliance assessment tool supports the summary of requirements applicable to AS6500A, including potential documentation to demonstrate compliance along with tailoring options and company policies. The standard is applicable to all phases of the system acquisition life cycle. It is intended for use on all programs with manufacturing content. It requires proven manufacturing management practices with the goal of delivering affordable and capable systems to the extent that it is invoked contractually.
G-23 Manufacturing Management Committee
Steel, Corrosion-Resistant, Bars and Wire 18Cr - 9.0Ni (302) Solution Heat Treated, Cold Drawn and Stress Relieved 125 ksi (862 MPa) Tensile StrengthAMS5637K (Current)10/5/2023
This specification covers a corrosion-resistant steel in the form of bars and wire 0.75 inch (19 mm) and under in nominal diameter or distance between parallel sides (thickness).
AMS F Corrosion and Heat Resistant Alloys Committee
Steel, Corrosion and Heat-Resistant, Bars, Wire, Forgings, Mechanical Tubing, Rings and Forging Stock 18Cr - 11Ni - 0.60Cb(Nb) (347) Solution Heat TreatedAMS5646R (Current)12/13/2021
This specification covers a corrosion and heat-resistant steel in the form of bars, wire, forgings, mechanical tubing, flash welded rings, and stock for forging or flash welded rings.
AMS F Corrosion and Heat Resistant Alloys Committee
Nickel Alloy, Corrosion- and Heat-Resistant, Bars, Forgings, Rings, and Forging Stock 72Ni - 15.5Cr - 7.0Fe - 2.5Ti - 1.0Cb (Nb) - 0.70Al (X750) 2100 °F (1149 °C) Solution and Precipitation Heat TreatedAMS5668L (Current)6/10/2024
This specification covers a corrosion- and heat-resistant nickel alloy in the form of bars, forgings, flash-welded rings 10.0 inches (254 mm) and under in nominal diameter or distance between parallel sides, and stock of any size for forging, flash-welded rings, or heading.
AMS F Corrosion and Heat Resistant Alloys Committee
Steel, Corrosion- and Heat-Resistant, Bars, Wire, Forgings, Mechanical Tubing, Rings, and Stock for Forgings and Flash-Welded Rings 17Cr (430), AnnealedAMS5627J (Current)4/1/2024
This specification covers a corrosion- and heat-resistant steel in the form of bars, wire, forgings, mechanical tubing, flash-welded rings, and stock for forging or flash-welded rings.
AMS F Corrosion and Heat Resistant Alloys Committee
Balls, Steel, Corrosion-Resistant 17Cr AnnealedAMS7445E (Current)6/5/2017
This specification covers balls made of high-carbon corrosion-resistant steel of three carbon ranges.
AMS F Corrosion and Heat Resistant Alloys Committee
Steel Tubing, Seamless, Round 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130) 95 ksi (655 MPa) Tensile Strength Aircraft QualityAMS6374F (Current)6/17/2025
This specification covers an aircraft-quality, low-alloy steel in the form of round, non-welded tubing free from OD surface seams.
AMS E Carbon and Low Alloy Steels Committee
Direction Instrument, Magnetic, Non-Stabilized Type (Magnetic Compass)AS398B (Current)2/16/2008
This Aeronautical Standard covers two basic types of instruments as follows: Type I - Direct Reading Type II - Remote Indicating
A-4 Aircraft Instruments Committee
Aerospace Rod Scraper Gland Design StandardAS4088F (Current)11/3/2020
This SAE Aerospace Standard (AS) defines gland details for scrapers for rod diameters from 1/4 to 15-1/2 inch (6.35 to 393.70 mm) inclusive, corresponding to AS568 O-ring Dash No. sizes -108/-111, -206/-222, -325/-349, and -425/-460. The gland details herein allow the use of more stable, efficient, and reliable scraper devices than MS33675 glands.
A-6C2 Seals Committee
Flexure Testing of Bent Hydraulic TubingARP1321A (Current)11/1/2000
This recommended practice establishes a flexure test procedure for determining the fatigue strength of bent hydraulic tubing. The procedure is intended for conducting flexure fatigue testing of hydraulic and pneumatic tubing to determine the effects of tube fabrication methods, surface finishing, and other processing techniques on the fatigue performance of the tubing. A mean stress is applied by holding system pressure in the specimens and flexing in a rotary flexure test machine.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Ground Electrical Power Unit, Transportable 115/200 Volt AC (Nominal) 400 Hertz, 3-Phase 4-Wire (Grounded Neutral) Y-Connected SystemARP1148B (Current)10/22/2013
This Recommended Practice outlines the electrical performance characteristics for a continuous duty, diesel or gasoline engine driven brushless alternator unit for supplying 400-Hertz electrical power to commercial transport aircraft. It is intended to assist the airlines in standardizing recommendations for various sizes and configurations of equipment and it is a guide for the preparation of detailed specifications. The unit is primarily intended to supply power to the aircraft during passenger loading and unloading, and during servicing operations. The combination of the equipment specified herein and the interconnecting cables(s) between the 400-Hertz alternator and the aircraft shall provide power characteristics at the aircraft receptacle which meet MIL-STD-704 requirements for Category "B" equipment. Other limits which are necessary to meet specific conditions must be specified by the purchaser.
AGE-3 Aircraft Ground Support Equipment Committee
Steel, Mechanical Tubing 0.95Cr - 0.20Mo (0.33 - 0.38C) (SAE 4135)AMS6372P (Current)10/4/2022
This specification covers an aircraft-quality, low-alloy steel in the form of mechanical tubing.
AMS E Carbon and Low Alloy Steels Committee
HUB - WOOD PROPELLER - TAPER TYPE - NUMBER 0AS357 (Current)2/1/1958
Nickel Alloy, Corrosion- and Heat-Resistant, Bars, Forgings, and Rings 53Ni - 19Cr - 11Co - 9.8Mo - 3.2Ti - 1.6Al - 0.006B Vacuum Melted, Solution Heat Treated Precipitation HardenableAMS5712L (Current)8/17/2022
This specification covers a corrosion- and heat-resistant nickel alloy in the form of bars 3.00 inches (76.2 mm) and under in nominal diameter, thickness or for hexagons least distance between parallel sides, forgings, flash welded rings 3.00 inches (76.2 mm) and under in nominal radial thickness, and stock of any size for forging, flash welded rings, or heading (see 8.5).
AMS F Corrosion and Heat Resistant Alloys 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
Steel, Corrosion-Resistant, Bars and Wire 18Cr - 9.0Ni (302) Solution Heat Treated and Cold Drawn 100 ksi (689 MPa) Tensile StrengthAMS5636H (Current)6/13/2023
This specification covers a corrosion-resistant steel in the form of bars and wire 0.75 inch (19 mm) and under in nominal diameter or distance between parallel sides (thickness).
AMS F Corrosion and Heat Resistant Alloys Committee
Yarn, Organic Fiber (Para-Aramid), High Modulus 1140 Denier (1270 d tex), 0.6% FinishAMS3901/3D (Current)7/30/2014
This specification covers one type of organic fiber in the form of yarn. The product shall be formed as a multiplicity of filaments drawn together and gathered into an approximately parallel arrangement.
AMS P17 Polymer Matrix Composites Committee
Glass Non-Woven Fiber Tape and Flat Sheet Epoxy Resin Impregnated, For Hand and Machine Layup GL-I-26 - 150 (302)AMS3906/3C (Current)10/12/2016
This specification covers one type of epoxy-resin-impregnated, non-woven, glass fiber in the form of tape for hand or machine layup and of flat sheet.
AMS P17 Polymer Matrix Composites Committee
Steel, Corrosion-Resistant, Bars, Wire, and Forgings and Forging Stock 17Cr - 0.52Mo (0.95 - 1.20C) (440C)AMS5630M (Current)8/26/2022
This specification covers a corrosion-resistant steel in the form of bars, wire, forgings, and forging stock.
AMS F Corrosion and Heat Resistant Alloys Committee
Iron Alloy, Corrosion- and Heat-Resistant, Welding Wire, 31Fe - 21Cr - 20Ni - 20Co - 3.0Mo - 2.5W - 1.0Cb - 0.15N (N-155), AnnealedAMS5794G (Current)10/3/2025
This specification covers a corrosion- and heat-resistant iron alloy in the form of welding wire.
AMS F Corrosion and Heat Resistant Alloys Committee
PLASTIC MOLDINGS, THERMOSETTING Silicone, Glass Roving Filled, Heat ResistantAMS3643A (Current)8/25/2011
This specification covers a glass-roving-filled silicone resin in the form of compression moldings or transfer moldings.
AMS P Polymeric Materials Committee
Plastic Moldings, Laminated, Thermosetting Resin Glass Cloth Reinforced Heat ResistantAMS3642E (Current)1/16/2012
This specification covers a glass-cloth-reinforced thermosetting resin in the form of laminated, pressure-bag or matched-die moldings.
AMS P Polymeric Materials Committee
Nickel Alloy, Corrosion- and Heat-Resistant, Bars, Forgings, and Rings and Stock for Forgings and Rings 74Ni - 15.5Cr - 8.0FeAMS5665R (Current)5/30/2023
This specification covers a corrosion- and heat-resistant nickel alloy in the form of bars and forgings, flash welded rings, and stock for forging or flash welded rings.
AMS F Corrosion and Heat Resistant Alloys Committee
Logistics Product Data HandbookGEIAHB0007B (Current)2/10/2014
LCLS Life Cycle Logistics Supportability
Inserts, Screw Thread, Helical Coil Metric Series Procurement Specification ForMA1565C (Current)12/8/2014
This SAE Metric Aerospace Standard defines the requirements for corrosion resistant steel helical coil metric series screw thread inserts made from formed wire, the inner surfaces of which, after assembly, provide internal threads of the diameter and pitch specified on the drawing.
E-25 General Standards for Aerospace and Propulsion Systems
STUDS, LOW-ALLOY STEEL Heat Treated, Rolled ThreadedAMS7456J (Current)5/1/1995
AMS E Carbon and Low Alloy Steels Committee
BOLTS AND SCREWS, CORROSION HEAT RESISTANT NICKEL ALLOY Upset Headed, Heat Treated, Roll Threaded 2050°F (1121°C) Solution and 1650°F (899°C) Precipitation Heat TreatedAMS7469C (Current)5/1/1995
AMS F Corrosion and Heat Resistant Alloys Committee
Aluminum Alloy, Heat-Resistant, Castings 5.0Cu - 1.5Ni - 0.25Mn - 0.25Sb - 0.25Co - 0.20Ti - 0.20Zr (203.0-T6) Solution Heat Treated and Precipitation Heat TreatedAMS4225F (Current)5/14/2026
This specification covers an aluminum alloy in the form of castings.
AMS D Nonferrous Alloys Committee
Steel, Corrosion-Resistant, Rivet Wire, 18Cr - 11.5Ni (SAE 305) Solution Heat TreatedAMS5686J (Current)6/13/2024
This specification covers a corrosion-resistant steel in the form of wire.
AMS F Corrosion and Heat Resistant Alloys Committee
Steel, Corrosion- and Heat-Resistant, Bars, Forgings, Rings, and Forging Stock 13.5Cr - 13.5Ni - 0.35Mo - 2.2W AnnealedAMS5700H (Current)11/2/2022
This specification covers a corrosion- and heat-resistant steel in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings.
AMS F Corrosion and Heat Resistant Alloys Committee
Extrusions, Nickel-Aluminum Bronze, Martensitic 78.5Cu – 10.5Al – 5.1Ni – 4.8Fe Quenched and Tempered (TQ50)AMS4590D (Current)12/1/2021
This specification covers one type of nickel-aluminum bronze in the form of extruded bars, rods, and tubes.
AMS D Nonferrous Alloys Committee
Aluminum Alloy Castings 7.0Si - 0.35Mg (A356.0-T6) (Formerly T6P Temper) Solution and Precipitation Heat TreatedAMS4218J (Current)10/29/2015
This specification covers an aluminum alloy in the form of sand, permanent mold, composite mold, and investment castings.
AMS D Nonferrous Alloys Committee
Performance Testing for Aerospace and High Performance Electronic Interconnects Containing Pb-free Solder and FinishesGEIASTD0005_3A (Current)2/12/2018
This document defines: 1 A default method for those companies that require a pre-defined approach and 2 A protocol for those companies that wish to develop their own test methods. The default method (Section 4 of the document) is intended for use by electronic equipment manufacturers, repair facilities, or programs which, for a variety of reasons, may be unable to develop methods specific to their own products and applications. It is to be used when little or no other information is available to define, conduct, and interpret results from reliability, qualification, or other tests for electronic equipment containing Pb-free solder. The default method is intended to be conservative, i.e., it is biased toward minimizing the risk to users of AHP electronic equipment. The protocol (Section 5 of the document) is intended for use by manufacturers or repair facilities which have the necessary resources to design and conduct reliability, qualification, or process development tests that are
G-24 Pb-free Risk Management Committee for ADHP
Oxygen System and Component CleaningARP1176B (Current)9/23/2025
This SAE Aerospace Recommended Practice (ARP) provides recommended practices for the cleaning of aircraft oxygen equipment, both metallic and non-metallic articles, such as oxygen lines (tubes, hoses, etc.), components (including regulator and valve parts), cylinders, and ground-based equipment that may be used to support aircraft oxygen systems. This document also specifies work area details, methods for selecting suitable cleaning agents, cleaning methods, and test methods for verifying levels of cleanliness. The cleanliness coding scheme specified in this document provides a method for documenting minimum cleanliness level requirements and for identifying compliance.
A-10 Aircraft Oxygen Equipment Committee
American National Standard Code for Information Interchange for Numerical Machine ControlEIA358C (Current)9/1/2015
This Standard describes the use of ANSI X3.4 for numerically controlled machines, attached communication equipment, and associated perforated tape preparation equipment.
Systems Management Council
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
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
CONNECTOR ACCESSORIES, ELECTRICAL, MOUNTING DEVICE, FLANGE TYPE, CATEGORY 7, 1/4 PERIMETERAS85049/96C (Current)4/26/2021
AE-8C1 Connectors Committee
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