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Aircraft Pressures and Temperatures – Resource Document

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 Temperatures

AIR8469 (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 Sources

AIR560D (Current)

This AIR provides information about the specific requirements for missile hydraulic pumps and their associated power sources.

A-6C4 Power Sources Committee

BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, PD SHANK, STEEL SAE 8740, CADMIUM PLATED, 125 KSI MIN UTS, .4375-20 UNJF-3A

AS9918C (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-3A

AS9727A (Current)

6/3/2026

E-25 General Standards for Aerospace and Propulsion Systems

Driveline Parking Brake Test Procedure for Medium Duty Vehicles

J2690_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.

Truck and Bus Hydraulic Brake Committee

BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, PD SHANK, CUP WASHER LOCKED, CRES, UNS S66286, 130 KSI MIN, .1900-32 UNJF-3A

AS9676C (Current)

6/3/2026

SCOPE IS UNAVAILABLE.

E-25 General Standards for Aerospace and Propulsion Systems

WASHER, KEY - 90°, LOCKING, CRES, UNS S32100

AS9581D (Current)

6/3/2026

SCOPE IS UNAVAILABLE.

E-25 General Standards for Aerospace and Propulsion Systems

Functional, Performance, and Safety Guidelines for Tire Pressure Monitoring Systems (TPMS) for Aircraft

ARP6137A (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

Steel, Corrosion-Resistant, Wire, 18Cr - 9.0Ni (302), Spring Temper

AMS5688N (Current)

6/1/2026

This specification covers a corrosion-resistant steel in the form of wire.

AMS F Corrosion and Heat Resistant 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) Controlled

AMS4241F (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 Fabricated

AMS4465C (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, Castings, 5.0Si - 1.2Cu - 0.50Mg (355.0-T51), Precipitation Heat Treated

AMS4210N (Current)

4/24/2026

This specification covers an aluminum alloy in the form of castings (see 8.6).

AMS D Nonferrous Alloys Committee

OBD-II Scan Tool: First Generation Protocols

J1978-1_202604 (Current)

4/20/2026

SAE J1978-1 specifies a complementary set of functions to be provided by an OBD-II scan tool. These functions provide complete, efficient, and safe access to all regulated OBD (on-board diagnostic) services on any vehicle which complies to SAE J1979. The content of this document is intended to satisfy the requirements of an OBD-II scan tool as required by current U.S. OBD regulations. This document specifies: A means of establishing communications between an OBD-equipped vehicle and an OBD-II scan tool. A set of diagnostic services to be provided by an OBD-II scan tool in order to exercise the services defined in SAE J1979. In addition, SAE J1978-1 covers first generation protocol functionality defined in SAE J1979 plus automatic protocol determination for all SAE J1979/J1979-2/J1979-3 application content. The presentation of the SAE J1978 document family, where SAE J1978-1 covers first generation protocol functionality defined in SAE J1979 and protocol determination for SAE J1979, SAE

Vehicle E E System Diagnostic Standards Committee

Time-Triggered Ethernet

AS6802A (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 + Checklist

AS6500A_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

Potting Compound, Epoxy, Filled 10 - 15 Cte, 225 Hdt

AMS3735C (Current)6/1/1996

This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of June, 1996, and has been superseded by AMS 3731 & /2.

AMS P Polymeric Materials Committee

Potting Compound, Epoxy, Unfilled General Purpose Room Temperature Cure

AMS3734B (Current)6/1/1996

This specification has been declared "CANCELLED" by the Aerospace Materials Division, SAE, as of June, 1996, and has been supersed by AMS 3731 and /10.

AMS P Polymeric Materials Committee

POTTING COMPOUND, EPOXY, FILLED 15 – 20 GTE, 225 HDT Free Machining

AMS3740 (Current)

12/1/1994

AMS P Polymeric Materials Committee

Potting Compound, Epoxy Flexible, Thermal Shock Resistant, Heat Cure

AMS3731/9C (Current)9/22/2016

This specification covers a flexibilized epoxy resin formulation, supplied as a two-component system, requiring an oven cure for attainment of maximum properties.

AMS P Polymeric Materials Committee

Epoxy Resin, Tetraglycidyl Methylenedianiline (TGMDA), 10,000 to 14,000 Centipoise Viscosity

AMS3701C (Current)4/1/1995

This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1995.

AMS P17 Polymer Matrix Composites Committee

SYNTHETIC RUBBER Buna S Type (35-45)

AMS3245 (Current)

5/1/1954

AMS CE Elastomers Committee

GASKET, OIL RESISTING

AMS3230 (Current)

12/16/2002

AMS CE Elastomers Committee

Adhesion Promoter for Polysulfide Sealing Compounds Nonhalogenated Solvent

AMS3100/1B (Current)12/15/2008

This specification has been declared "CANCELLED " by the Aerospace Materials Division, SAE, as of December 2008 and has been superseded by AMS3100B. The requirements of the latest issue of AMS3100B shall be fulfilled whenever reference is made to the cancelled AMS3100/1A. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications, noting that it has been superseded by AMS3100B.

AMS G9 Aerospace Sealing Committee

SEALING COMPOUND, LOW ADHESION, CORROSION INHIBITING 200 to 600 Poises (20 to 60 Pa·s), 1/2 Hour Application Time (A-1/2)

AMS3267/1A (Current)

4/24/2003

This specification covers accelerated curing synthetic rubber compounds with corrosion inhibitors and low adhesive strength supplied as a two-component system.

AMS G9 Aerospace Sealing Committee

Core, Polyurethane Foam (Polyether) 4.0 Pounds Per Cubic Foot (64 kg/m3) Density

AMS3725/2B (Current)

11/10/2016

This specification covers a rigid cellular polyurethane or polyisocyanurate (polyether only) foam in the form of board or block.

AMS P17 Polymer Matrix Composites Committee

Webbing, Woven Nylon For Decelerators 1 (25) Wide, 6000 (26,700) Breaking Strength

AMS3718/3B (Current)

6/14/2016

This specification covers one width and one strength of nylon webbing.

AMS P Polymeric Materials Committee

Alloy, Corrosion- and Heat-Resistant, Bars and Forgings 53Ni - 15Cr - 18.5Co - 5.0Mo - 3.2Ti - 4.2Al - 0.03B Double Vacuum Melted Solution, Stabilization, and Precipitation Heat Treated

AMS5846D (Current)

2/7/2022

This specification covers a corrosion and heat-resistant nickel alloy in the form of bars, forgings, and forging stock.

AMS F Corrosion and Heat Resistant Alloys Committee

Titanium Alloy, Bars and Rods 3Al - 8V - 6Cr - 4Mo - 4Zr Consumable Electrode Melted Solution Heat Treated and Centerless Ground or Peeled and Polished

AMS4958F (Current)

11/2/2022

This specification covers a titanium alloy in the form of bars and rods 1.00 inch (25.4 mm) and under in nominal diameter.

AMS G Titanium and Refractory Metals Committee

CONNECTOR ACCESSORIES, ELECTRICAL, BACKSHELL, NONENVIRONMENTAL, STRAIGHT, RFI/EMI, CATEGORY 3B (FOR MIL-DTL-38999 SERIES III AND IV CONNECTORS)

AS85049/19C (Current)

4/26/2021

AE-8C1 Connectors Committee

WIRE, ELECTRICAL, POLYTETRAFLUOROETHYLENE/POLYIMIDE INSULATED, SMOOTH SURFACE, LIGHT WEIGHT, TIN-COATED COPPER CONDUCTOR, 150 °C, 600 VOLTS ROHS

AS22759/180A (Current)

12/18/2019

AE-8D Wire and Cable Committee

Cloth, Upholstery, Flame Resistant Aramid, Plain Weave

AMS3856/2B (Current)

6/24/2016

This specification covers one weight and one weave of aramid cloth.

AMS P Polymeric Materials Committee

Cord, Aromatic Polyamide, Nonmelting 375 Pounds (1670 N), 230 Foot/Pound (155 M/Kg)

AMS3853/2B (Current)10/1/1995

No scope available.

AMS P Polymeric Materials Committee

Webbing, Nylon, Aircraft Arresting 105,000 Pounds (467 kN)

AMS3796/1B (Current)

6/14/2016

This specification covers one type of nylon in the form of webbing.

AMS P Polymeric Materials Committee

Tape and Webbing, Textile, Para-Aramid Intermediate Modulus 2.00 Inches (50 mm), 0.12 to 1.10 Ounces per Yard (3.7 to 34.1 g/m)

AMS3793/9B (Current)

9/11/2013

This specifications covers thirteen classes of para-aramid tape and webbing of a single width and with varying weights.

AMS P Polymeric Materials Committee

Cloth, Twill Nylon, Warp, Rayon Filling

AMS3789B (Current)10/1/1995

This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1995.

AMS P Polymeric Materials Committee

Sealing Compound, Low Adhesion, Corrosion Inhibiting, 200 to 600 Poises (20 to 60 Pa⋅s), 2 Hour Application Time (A-2)

AMS3267/3B (Current)2/18/2011

This specification covers accelerated curing synthetic rubber compounds with corrosion inhibitors and low adhesive strength supplied as a two-component system. This product has been used typically for sealing aircraft access doors and accessories where gaskets are required, but usage is not limited to such applications. Compound is classified as an A-2 sealing compound; the compound being suitable for brush application with a minimum of two hours application time after mixing.

AMS G9 Aerospace Sealing Committee

Titanium Alloy Welding Wire, 5Al - 2.5Sn

AMS4953J (Current)

4/25/2024

This specification covers a titanium alloy in the form of welding wire (see 8.5).

AMS G Titanium and Refractory Metals Committee

Titanium Alloy Bars, Wire, and Forgings 7Al - 4Mo Solution and Precipitation Heat Treated

AMS4970M (Current)

8/19/2025

This specification covers a titanium alloy in the form of bars, wire, forgings up to 4.000 inches (101.60 mm), inclusive, and forging stock.

AMS G Titanium and Refractory Metals Committee

Steel, Maraging, Investment Castings 18.5Ni - 9.0Co - 5.0Mo - 0.70Ti - 0.12Al Vacuum Melted Homogenized, Overaged, and Solution Heat Treated

AMS5337E (Current)

6/5/2022

This specification covers an alloy steel in the form of investment castings.

AMS E Carbon and Low Alloy Steels Committee

Tow or Yarn, Carbon Fibers For Structural Composites GF (0X) 400 (2758) Tensile Strength, 40 (276) Tensile Modulus

AMS3892/8B (Current)

12/15/2016

This specification covers one type of continuous multifilament carbon fibers in the form of a tow or yarn (when twisted). The weight per unit length of the tow or yarn is governed by the filament count which is identified by the supplier's grade or material designation.

AMS P17 Polymer Matrix Composites Committee