Search
Advanced Search
of the following are true
(
)

Results

Items (219,531)
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
CONNECTOR ACCESSORIES, ELECTRICAL, BACKSHELL, ENVIRONMENTAL, CABLE SEALING, 45°, SHIELD TERMINATION, CATEGORY 1A (FOR AS50151 CRIMP, AS95234, MIL-DTL-26482 SERIES 2, AS81703 SERIES 3, AND MIL-DTL-83723 SERIES III CONNECTORS)AS85049/6D (Current)1/31/2026
AE-8C1 Connectors Committee
CONNECTOR ACCESSORIES, ELECTRICAL, BACKSHELL, 90°, SELF-LOCKING, SHIELD BAND TERMINATION (RFI/EMI), SHRINK SLEEVE ACCOMMODATION, CATEGORY 3B (FOR AS50151 CRIMP, AS95234, MIL-DTL-26482 SERIES 2, AS81703 SERIES 3, AND MIL-DTL-83723 SERIES III CONNECTORS)AS85049/84D (Current)5/20/2021
AE-8C1 Connectors Committee
CONNECTOR ACCESSORIES, ELECTRICAL, ADAPTER, SHRINK BOOT, CATEGORY 5 (FOR AS50151 CRIMP, AS95234, MIL-DTL-26482 SERIES 2, AS81703 SERIES 3, AND MIL-DTL-83723 SERIES III CONNECTORS)AS85049/60D (Current)9/10/2021
AE-8C1 Connectors Committee
CONNECTOR ACCESSORIES, ELECTRICAL BACKSHELL, STRAIGHT, NON-SELF LOCKING AND SELF LOCKING, PRE-ATTACHED SHIELD TERMINATION (RFI/EMI), BOOT ACCOMMODATION, CATEGORY 3B (FOR MIL-DTL-83723 SERIES III, AS50151 CRIMP, AS95234, AS81703 SERIES III, AND MIL-DTL-26482 SERIES II CONNECTORS)AS85049/109D (Current)7/30/2021
AE-8C1 Connectors Committee
Tape and Webbing, Textile, Para-Aramid Intermediate Modulus 1 Inch (25 mm), 0.08 to 1.65 Ounces per Yard (2.5 to 51.2 g/m)AMS3793/4B (Current)9/11/2013
This specification covers twelve classes of para-aramid tape and webbing of a single width and with varying weights.
AMS P Polymeric Materials Committee
CONNECTOR ACCESSORIES, ELECTRICAL, BACKSHELL, STRAIGHT, NON-SELF-LOCKING AND SELF-LOCKING, CATEGORY 3B (FOR MIL-DTL-38999 SERIES III AND IV CONNECTORS)AS85049/14C (Current)4/5/2019
AE-8C1 Connectors Committee
CONNECTOR ACCESSORIES, ELECTRICAL, STRAIN RELIEF, STRAIGHT SELF-LOCKING, AND NON-SELF-LOCKING, CATEGORY 4C (FOR MIL-DTL-38999 SERIES I AND II CONNECTORS)AS85049/121C (Current)2/8/2025
AE-8C1 Connectors Committee
Potting Compound, Epoxy, Filled 10 - 15 Cte, 225 HdtAMS3735C (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
EPOXY RESIN, TETRAGLYCIDYL METHYLENEDIANILINE 14,000 TO 18,000 Centipoise ViscosityAMS3702A (Current)1/1/1993
AMS P Polymeric Materials Committee
POTTING COMPOUND, EPOXY, FILLED 15 – 20 CTE, 180 HDTAMS3738 (Current)12/1/1994
AMS P Polymeric Materials Committee
Webbing, Woven Nylon For Decelerators 1 (25) Wide, 9000 (40,000) Breaking StrengthAMS3718/5B (Current)6/14/2016
This specification covers one width and one strength of nylon 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 FillingAMS3789B (Current)10/1/1995
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1995.
AMS P Polymeric Materials Committee
Potting Compound, Epoxy Flexible, Thermal Shock Resistant, Heat CureAMS3731/9C (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
Interleaf Carrier Material, Composite Tape/Broadgoods Kraft, Differentially Coated Paper, Unperforated 0.0038 inch ± 0.0004 (0.097 mm ± 0.010)AMS3898/8A (Current)4/13/2022
This specification covers a kraft paper, coated on both sides and with different release characteristics on each side (i.e., differentially coated), supplied in the form of rolls of sheeting or reels of unperforated tape of the width specified.
AMS P17 Polymer Matrix Composites Committee
Cloth, Upholstery, Flame Resistant Aramid, Plain WeaveAMS3856/2B (Current)6/24/2016
This specification covers one weight and one weave of aramid cloth.
AMS P Polymeric Materials Committee
Core, Polyurethane Foam (Polyether) 4.0 Pounds Per Cubic Foot (64 kg/m3) DensityAMS3725/2B (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 StrengthAMS3718/3B (Current)6/14/2016
This specification covers one width and one strength of nylon webbing.
AMS P Polymeric Materials Committee
Epoxy Resin, Tetraglycidyl Methylenedianiline (TGMDA), 10,000 to 14,000 Centipoise ViscosityAMS3701C (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
CONNECTOR ACCESSORIES, ELECTRICAL BACKSHELL, 90 DEGREE, SELF LOCKING AND NON-SELF LOCKING, PRE-ATTACHED SHIELD TERMINATION (RFI/EMI), BOOT ACCOMMODATION, CATEGORY 3B (FOR MIL-DTL-83723 SERIES III, AS50151 CRIMP, AS95234, AS81703 SERIES III, AND MIL-DTL-26482 SERIES II CONNECTORS)AS85049/111D (Current)6/22/2021
AE-8C1 Connectors Committee
CONNECTOR ACCESSORIES, ELECTRICAL, BACKSHELL, ENVIRONMENTAL, CABLE SEALING, 45°, CATEGORY 1A (FOR AS50151 CRIMP, AS95234, MIL-DTL-26482 SERIES 2, AS81703 SERIES 3, AND MIL-DTL-83723 SERIES III CONNECTORS)AS85049/7D (Current)1/29/2026
AE-8C1 Connectors Committee
Webbing, Woven Nylon For Decelerators 1 3/4 (44) Wide, 10,000 (44,500) Breaking StrengthAMS3718/6B (Current)6/14/2016
This specification covers one width and one strength of nylon webbing.
AMS P Polymeric Materials Committee
Adhesive, Epoxy Paste, For Structural Weldbond, For 80°C (180°F) ServiceAMS3708B (Current)10/1/1995
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1995.
AMS P17 Polymer Matrix Composites Committee
Forgings, Hardenable Steels and Corrosion-Resistant Steels Heat-Treated, Finished-Part Properties Short-Transverse Tensile Strength and Fracture ToughnessAMS6474B (Current)2/24/2018
This specification establishes requirements for steel forgings of any shape or form that finished parts are to be made (See 8.4, 8.5, 8.8.4 and 8.10).
AMS E Carbon and Low Alloy Steels 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
Tow or Yarn, Carbon Fibers For Structural Composites GF (0X) 400 (2758) Tensile Strength, 40 (276) Tensile ModulusAMS3892/8B (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
Light Source Retention SystemJ567_201502 (Current)2/1/2015
This SAE Standard references the performance and functional requirements of the International Electrotechnical Commission (IEC) and its U.S. member, the American National Standards Institute (ANSI). By referring to IEC/ANSI and its standards concerning light source (bulb) sockets, light source (lamp) holders, and gages, this document recognizes the need for harmonized standards world-wide for what are typically commodity items. Additional requirements are noted.
Lighting Standard Practices Committee
Motorcycle and Motor Driven Cycle Electrical System Maintenance of Design VoltageJ392_202005 (Current)5/25/2020
This SAE Recommended Practice pertains to electrical systems of motorcycles both with and without batteries.
Motorcycle Technical Steering Committee
Steel Bars, Forgings, Rings and Stock for Forging and Flash-Welded Rings 0.95Cr - 0.20Mo (0.28 - 0.33C), (SAE 4130) Aircraft QualityAMS6370S (Current)5/3/2025
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, flash-welded rings, and stock for forging or flash-welded rings.
AMS E Carbon and Low Alloy Steels Committee
Potting Compound, Epoxy, Unfilled General Purpose Room Temperature CureAMS3734B (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 MachiningAMS3740 (Current)12/1/1994
AMS P Polymeric Materials Committee
Tape, Nylon, Nonmelting, Reinforcing 2 (50) Wide, 1500 (6670 N) Breaking StrengthAMS3777/7B (Current)10/1/1995
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1995.
AMS P Polymeric Materials Committee
Steel, Spring Wire 0.95Cr - 0.22V (0.48 - 0.53C) (SAE 6150) Annealed and Cold DrawnAMS6450L (Current)11/2/2022
This specification covers a low-alloy steel in the form of wire supplied as coils, spools, and straight lengths.
AMS E Carbon and Low Alloy Steels Committee
Steel, Welding Wire, 0.50Cr - 0.55Ni - 0.20Mo (0.33 0.38C) (SAE 8735) Vacuum Melted, Environment Controlled PackagingAMS6331B (Current)5/15/2003
This specification covers a low-alloy steel in the form of welding wire.
AMS E Carbon and Low Alloy Steels Committee
Adhesion Promoter for Polysulfide Sealing Compounds Nonrestricted SolventAMS3100/2B (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 AMS3100/2A. 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
Interleaf Carrier Material, Composite Tape Differentially Coated Paper, Unperforated 0.0042 inch (0.107 mm)AMS3898/7A (Current)4/13/2022
This specification covers a paper, coated on both sides and with different release characteristics on each side (i.e., differentially coated), supplied in the form of rolls of sheeting or reels of unperforated tape of the width specified.
AMS P17 Polymer Matrix Composites Committee
Bolts and Screws, Steel, UNS S66286 1650 °F Solution Heat Treated Precipitation Heat Treated Before Roll ThreadedAS7479E (Current)8/27/2021
This specification 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, and of 130000 psi tensile strength at room temperature, with maximum test temperature of parts at 1200 °F.
E-25 General Standards for Aerospace and Propulsion Systems
Washer, Thermal Compensating, Metric SeriesAIR1754B (Current)2/18/2019
The purpose of this document is to define: - compensation washer application requirements - recommended materials - washer thickness determination - dimensioning
E-25 General Standards for Aerospace and Propulsion Systems
HOSE ASSEMBLY, 3000 PSI, PTFE, FLARED, STRAIGHT TO 45°, HEAVYWEIGHTAS628D (Current)11/27/2018
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
HOSE ASSEMBLY, 3000 PSI, PTFE, FLARED, 90° TO 90°, HEAVYWEIGHTAS632D (Current)11/27/2018
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Items per page:
1 – 50 of 219531