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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

Numerical Modeling Techniques for Jet Engine Test Cell Aerodynamics

AIR6355 (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-3A

AS9727A (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-3A

AS9918C (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-3A

AS9676C (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. 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 S32100

AS9581D (Current)

6/3/2026

E-25 General Standards for Aerospace and Propulsion Systems

Seals--Testing of Radial Lip

J110_200210 (Current)10/25/2002

SAE IC Powertrain Steering Committee

Latex-Dipped Goods and Coatings for Automotive Applications

J19_200508 (Current)8/22/2005

These specifications cover dipped goods and coatings made from compounded latex. Products manufactured from this material include boots, coated clips, coated sponge parts, and coated fabrics for automotive applications. The compounds listed in Tables 1 and 2 are grouped into classifications based primarily on physical properties which are prescribed in the tables. These values, together with any additional requirements, indicated by suffix letters in the grade designations as described in Section 3, define the properties of the compounds after vulcanization. These values apply to test specimens obtained from standard laboratory dipped films prepared in accordance with procedures described in the applicable ASTM test methods. Test results from finished products may not duplicate the values obtained from standard test films. When differences due to the difficulty in obtaining suitable test specimens from the finished part arise, the purchaser and the supplier may agree on acceptable

Committee on Automotive Rubber Specs

Information Report on Its Terms and Definitions

J1761_200304 (Current)5/5/2003

This SAE Information Report defines consistent terminology for Intelligent Transportation Systems (ITS). The list of defined terms is followed by a list of acronyms. Certain criteria were used in selecting terms for this document. Terms in widespread use in the ITS community covering significant services, technologies and applications were chosen. This document focuses on terms used in the United States, although it covers aspects of worldwide ITS deployment. This document focuses on automotive applications, which include interfaces to and from the automobile. Later version may include a wider scope. ITS includes a wide array of services, applications, and technologies. The Department of Transportation ITS National program Plan divides ITS into 29 User Services, which are included in this glossary. The User Services range from pre-Trip Travel Planning to Fully Automated Highway Systems. Other organizations and experts have divided ITS into a smaller set of more general application

Motor Vehicle Council

Engine Flywheel Housing and Mating Transmission Housing Flanges

J617_202009 (Current)

9/29/2020

This SAE Standard specifies the major dimensions and tolerances for Engine Flywheel Housings and the Mating Transmission Housing Flanges. It also locates the crankshaft flange face or the transmission pilot bore (or pilot bearing bore) stop face in relation to housing SAE flange face. This document is not intended to cover the design of the flywheel housing face mating with the engine crankcase rear face or the design of housing walls and ribs. Housing strength analysis and the selection of housing materials are also excluded. This document applies to any internal combustion engine which can utilize SAE No. 6 through SAE No. 00 size flywheel housing for mounting a transmission.

Automatic Transmission and Transaxle Committee

Specification Definitions-Skidder-Grapple

J1112_200310 (Current)11/3/2003

This SAE Standard establishes definitions of specifications most commonly associated with grapple skidders. Specifications common to all articulated, rubber-tired log skidders are included in SAE J1110. The dimensions included in this document are basic and may be supplemented by the individual machine manufacturer. Dimensions shall be stated in SI units. Illustrations used herein are not intended to include all existing commercial machines or to be exactly descriptive of any particular machine. They have been included to facilitate application of this document.

MTC4, Forestry and Logging Equipment

J1930 Electrical/Electronic Systems Diagnostic Terms, Definitions, Abbreviations, and Acronyms Web Tool Spreadsheet

J1930DA_202301 (Current)1/17/2023

Continuation of the digital annex of terms and definitions for use by scantools and maintain alignment of terms with other committees such as J2012, J1979, J1939 etc. and with regulatory bodies.

Vehicle E E System Diagnostic Standards Committee

A Conceptual Its Architecture: An Atis Perspective

J1763_200304 (Current)5/5/2003

This SAE Information Report represents an information report on a conceptual ITS architecture and its accompanying protocols from the perspective of Advanced Traveller Information Systems providers and users. While a specific logical and physical architecture for ITS is still in the development stages, this conceptual architecture provides a robust general view of ITS functions and interfaces.

Motor Vehicle Council

Displacement of Pneumatic Service Brake Actuators

J1155_198801 (Current)3/1/1988

MTC4, Forestry and Logging Equipment

Cobalt Alloy, Corrosion- and Heat-Resistant, Strip 20Cr - 15Ni - 40Co - 7.0Mo - 16Fe Solution Heat Treated, Cold Rolled, and Aged Vacuum Induction Plus Vacuum Consumable Electrode Melted

AMS5875E (Current)

1/22/2025

This specification covers a corrosion- and heat-resistant cobalt alloy in the form of strip up to 0.100-inch (2.54-mm) thick.

AMS F Corrosion and Heat Resistant Alloys Committee

Face Seal Gland Design, Static, O-Ring and Other Seals for Aerospace Hydraulic and Pneumatic Applications

AS6235C (Current)5/27/2026

This SAE Aerospace Standard (AS) specifies standardized gland design criteria and dimensions for static face seals for internal pressure and external pressure applications for aerospace hydraulic and pneumatic applications using the same dash size range as AS4716 and AS5857 where applicable. NOTE: Some small diameter sizes are excluded because they are not practical.

A-6C2 Seals Committee

Alloy, Corrosion- and Heat-Resistant, Sheet, Strip, and Plate 29Fe - 22Cr - 21Ni - 18.5Co - 3.2Mo - 2.8W - 0.78Ta - 0.30Al - 0.05Zr - 0.05La - 0.20N (HS-556) Solution Heat Treated

AMS5874D (Current)

10/16/2023

This specification covers a corrosion- and heat-resistant alloy in the form of sheet, strip, and plate.

AMS F Corrosion and Heat Resistant Alloys Committee

Steel, Bars, Forgings and Forging Stock, 0.18 - 0.23C (SAE 1022)

AMS5070L (Current)

8/22/2025

This specification covers a carbon steel in the form of bars up through 3.000 inches (76.20 mm) and forgings and forging stock of any size.

AMS E Carbon and Low Alloy Steels Committee

COUPLING, V-RETAINER, DOUBLE LATCH, TYPE I STANDARD PROFILE

AS1895/22G (Current)

8/19/2024

G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies

CONNECTOR ACCESSORIES, ELECTRICAL, STRAIN RELIEF, STRAIGHT, SELF-LOCKING AND NON-SELF-LOCKING, CATEGORY 4C (MIL-DTL-38999 SERIES I AND II CONNECTORS)

AS85049/49D (Current)

1/11/2021

AE-8C1 Connectors Committee

Minimum Performance Standard General Aviation Flight Recorder

AS8039A (Current)

2/16/2008

This standard covers three (3) basic types of flight recorders as defined below: All requirements specified in Sections 3, 4, 5, 6 and 7 of this standard shall be applicable to all recorder types unless otherwise noted.

A-4 Aircraft Instruments Committee

CONNECTOR ACCESSORIES, COMPOSITE, ELECTRICAL, STRAIN RELIEF, 90°, SELF-LOCKING, CATEGORY 4C (FOR MIL-DTL-38999 SERIES III AND IV CONNECTORS)

AS85049/92D (Current)

12/1/2025

AE-8C1 Connectors Committee

HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, CRES REINFORCED, 400 °F, 3000 PSI, LIGHTWEIGHT, BEAM SEAL, 90 TO 90°

AS1914E (Current)

7/22/2025

G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies

Nickel-Iron Alloy Wire, Copper Clad, Round, 42Ni - 56.5Fe, Annealed Dumet

AMS7734D (Current)5/15/2006

This specification covers a nickel-iron alloy in the form of round wire clad with electrolytic copper.

AMS F Corrosion and Heat Resistant Alloys Committee

Passenger Car and Light Truck Tire Dynamic Driving Traction in Snow

J1466_200102 (Current)4/12/2001

Highway Tire Committee

Steel, Corrosion and Heat Resistant, Welding Wire 15Cr - 7.1Ni - 2.4Mo - 1.0Al Vacuum Induction Melted

AMS5812G (Current)

5/4/2021

This specification covers a corrosion and heat resistant steel in the form of welding wire.

AMS F Corrosion and Heat Resistant Alloys Committee

Air Cargo Pallet Extensions

AS1988B (Current)

10/6/2023

This SAE Aerospace Standard (AS) establishes the dimensional and operational requirements for pallet extension devices. It provides support for items of cargo beyond either the short or the long sides of a pallet, allowing increased volume to be achieved in conjunction with pallets meeting the requirements of AS1491 plus additional pallet sizes usable with extensions.

AGE-2 Air Cargo

CONNECTOR ACCESSORIES, ELECTRICAL, STRAIN RELIEF, STRAIGHT, SELF-LOCKING AND NON-SELF-LOCKING, CATEGORY 4C (FOR MIL-DTL-38999 SERIES III AND IV CONNECTORS)

AS85049/38C (Current)

9/23/2014

AE-8C1 Connectors Committee

CONNECTOR ACCESSORIES, ELECTRICAL, STRAIN RELIEF, NON-ENVIRONMENTAL, SELF-LOCKING AND NON-SELF-LOCKING, 45°, CATEGORY 4B (FOR MIL-DTL-5015 CRIMP, MIL-DTL-26482 SERIES 2, AS81703 SERIES 3, AND MIL-DTL-83723 SERIES III CONNECTORS)

AS85049/43C (Current)

12/1/2025

AE-8C1 Connectors Committee

Alloy Rivets, Corrosion and Heat Resistant, 74ni 15.5cr 8.0fe

AMS7232H (Current)10/1/1990

AMS F Corrosion and Heat Resistant Alloys Committee

Rubber: Acrylonitrile-Butadiene (NBR) Engine Oil Resistance, 65 to 75 Hardness, for Seals in Aircraft Engine Oil Systems

AMS7274K (Current)

7/8/2020

This specification covers an acrylonitrile-butadiene (NBR) rubber in the form of molded rings, compression seals, O-ring cord, and molded-in-place gaskets for aeronautical and aerospace applications. For sheet, strip, tubing, extrusions, and molded shapes, use the AMS3XXX specification which is intended for that use.

AMS CE Elastomers Committee

Compound, Corrosion Preventive Aircraft Engine

AMS3072E (Current)4/5/2007

This specification covers a blend of corrosion-preventive compound concentrate and petroleum-base aircraft-engine lubricating oil in the form of a ready-to-use liquid.

AMS B Finishes Processes and Fluids Committee

Internal Combustion Engines--Piston Rings--Expander/Segment Oil Control Rings

J2004_200806 (Current)6/30/2008

This SAE Standard is equivalent to ISO Standard 6627 TR. Differences, where they exist, are shown in Appendix A with associated rationale. This SAE Standard specifies the dimensional features of commonly used oil control rings having two steel segments (rails) separated and expanded by one steel expander/spacer. The segments vary in width from 0.4 to 0.6 mm. The assembly width ranges from 2.5 to 4.75 mm. The 4.75 mm width is equivalent to existing 3/16 in applications. Expander design will vary considerably with piston ring manufacturer. The total circumferential deflection and the piston groove depth should be considered when designing these oil rings to optimize the fit of the ring assembly into the piston groove. This document applies to oil control rings up through 125 mm for reciprocating internal combustion engines. It may also be used for piston rings of compressors working under similar conditions.

Piston and Ring Standards Committee

Aluminum Alloy Sheet and Plate, Alclad 4.4Cu - 1.5Mg - 0.60Mn (Alclad 2024 and 1-1/2% Alclad 2024-T861 Flat Sheet; 1-1/2% Alclad 2024-T861 Plate) Solution Heat Treated, Cold Worked, and Precipitation Heat Treated

AMS4195D (Current)

3/28/2016

This specification covers an aluminum alloy in the form of flat sheet and plate 0.500 inch (12.70 mm) and under in nominal thickness.

AMS D Nonferrous Alloys Committee

Gas Nitriding of Steel Parts

AMS2756B (Current)6/3/2008

This specification covers a process for surface-hardening parts, made from appropriate low-alloy steels (See 8.4), by the introduction of nitrogen from ammonia.

AMS B Finishes Processes and Fluids Committee

Coating, Vapor Deposited Poly-Monochloro-Para-Xylylene for Microcircuits

AMS2535B (Current)

10/22/2015

This specification covers requirements for poly-monochloro-para-xylylene coatings.

AMS B Finishes Processes and Fluids Committee

Safe Carriage of Impaired and Disabled Passengers

AIR1815A (Current)4/4/2013

This AIR defines the major groups of impairments and disabilities among passengers who use aircraft as a transportation mode, and the types of safety problems which might be associated with each impairment. These impairments, and their safety-related problems, should be considered when referring to ARP's related to the design of cabin furnishings and equipment.

S-9B Cabin Interiors and Furnishings Committee

ADAPTER 8” TO 5” BOLT CIRCLE

AS517A (Current)

1/1/2001

AE-1 Engine Accessory Installations Committee

HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, CRES REINFORCED, 400 °F, 3000 PSI, LIGHTWEIGHT, BEAM SEAL, 45 TO 90°

AS1913E (Current)

8/22/2025

G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies

Pressure Testing, 55 Psi

AMS2605E (Current)2/10/2004

This specification provides requirements and procedures for air-pressure leak testing of parts.

AMS B Finishes Processes and Fluids Committee

Radiographic Inspection

AMS2635D (Current)

5/1/1999

This specification covers the procedures for radiographic inspection.

AMS K Non Destructive Methods and Processes Committee

Aircraft Humidification

AIR1609B (Current)

1/14/2021

This SAE Aerospace Information Report (AIR) covers the design parameters for various methods of humidification applicable to aircraft, the physiological aspects of low humidities, the possible benefits of controlling cabin humidity, the penalties associated with humidification, and the problems which must be solved for practical aircraft humidification systems. The design information is applicable to commercial and military aircraft. The physiological aspects cover all aircraft environmental control applications.

AC-9 Aircraft Environmental Systems Committee