Search
Advanced Search
of the following are true
(
)

Results

Items (219,528)
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
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, CLOSE TOLERANCE SHANK, UNS N07001, 165 KSI, .4375-20 UNJF-3AAS9727A (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.
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-3AAS9676C (Current)6/3/2026
SCOPE IS UNAVAILABLE.
E-25 General Standards for Aerospace and Propulsion Systems
WASHER, KEY - 90°, LOCKING, CRES, UNS S32100AS9581D (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 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
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
Low Speed Thorax Impact Test Procedure for the HIII 50th Male DummyJ2779_202206 (Current)6/29/2022
Dummy Testing and Equipment Committee
Automatic Transmissions - Schematic DiagramsJ647_202512 (Current)12/1/2025
The following schematic diagrams reflect various methods of illustrating automotive transmission arrangements. These have been developed to facilitate a clear understanding of the functional interrelations of the gearing, clutches, hydrodynamic drive unit, and other transmission components. Two variations of transmission diagrams are used: in neutral (clutches not applied) and in gear. For illustrative purposes, some typical transmissions are shown.
Automatic Transmission and Transaxle Committee
AIRCRAFT NOISE RESEARCH NEEDSAIR1079 (Current)12/16/2002
A-21 Aircraft Noise Measurement Aviation Emission Modeling
HOSE ASSEMBLIES, POLYTETRAFLUOROETHYLENE, ARAMID REINFORCED, 28 000 kPa, HYDRAULIC AND PNEUMATICMA2140 (Current)4/1/1994
This specification defines the requirements for a PTFE lined, non-metallic, aramid reinforced assembly suitable for use to 135°C and 28 000 kPa aircraft and missile hydraulic and pneumatic systems.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
FITTING, UNION, STANDARD AND REDUCER, BULKHEAD, FLARELESSAS1007M (Current)12/20/2022
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
FITTING, ELBOW, 90°, STANDARD AND REDUCER, BULKHEAD, FLARELESSAS1008K (Current)5/9/2022
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Quality Assurance Sampling and Testing, Corrosion- and Heat-Resistant Steels and Alloys, Wrought Products and Forging StockAMS2371M (Current)11/12/2025
This specification covers quality assurance sampling and testing procedures used to determine conformance to applicable material specification requirements of wrought corrosion- and heat-resistant steel and alloy products and of forging stock.
AMS F Corrosion and Heat Resistant Alloys Committee
FITTING, CROSS, STANDARD AND REDUCER, FLARELESSAS1006G (Current)8/18/2017
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Aircraft Turbine Fuel Contamination History and Endurance Test RequirementsAIR4023C (Current)11/1/2021
This document discusses the history and development of endurance requirements, provides an analysis of test contaminant material and includes a discussion of future requirements.
AE-5B Aircraft and Engine Fuel and Lubricant Sys Components
FITTING, TEE, STANDARD AND REDUCER, BULKHEAD ON RUN, FLAREDAS1033G (Current)4/1/2020
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Turbine Engine Starting System Design RequirementsARP949B (Current)3/1/1999
This SAE Aerospace Recommended Practice (ARP) defines and establishes a standard presentation of data for gas turbine propulsion engine starter characteristics in graphs and curves. The data presentation applies to both pneumatic and hydraulic energy source starting systems.
AE-6 Starting Systems and Auxiliary Power Committee
Bubble-Point Test MethodARP901B (Current)9/30/2022
This test method describes a procedure for measuring the largest pore or hole in a filter or similar fluid-permeable porous structure. A standard referee test method for precise determination or resolution of disputes is specified. A simpler inspection test procedure for quality assurance “go-no-go” measurement is also given. Bubble-point testing physics, analysis of bubble-point test data, and correlation with other methods of pore size determination are separately discussed in the appendix.
A-6C1 Fluids and Contamination Control Committee
Reusable Lock for Spanner NutsARP688B (Current)4/28/2018
This aerospace recommended practice is applicable to the design of a reusable locking device for cylindrical nuts which are generally tightened with a spanner wrench. Nuts of this type are commonly used to pre-load, and/or position, anti-friction bearings.
E-25 General Standards for Aerospace and Propulsion Systems
Impact Protective Design of Occupant Environment Transport AircraftARP767C (Current)8/14/2006
This ARP provides design guidelines based on currently available information for the impact safety design of the cabin occupant environment.
S-9B Cabin Interiors and Furnishings Committee
Human Engineering Considerations in the Application of Color to Electronic Aircraft DisplaysARP4032B (Current)3/25/2013
This document is intended for the application of color to cathode-ray-tube (CRT) displays, liquid crystal displays (LCD) and other types of display technologies such as projection displays. Emerging color display technologies other than those noted above, may not be adequately covered by these recommendations. Color recommendations will not address Night Vision Devices (NVD), Head-Up Displays (HUD) or Head or Helmet Mounted Displays (HMD). This document is applicable to aircraft as understood in 14 CFR Parts 23, Part 25, Part 27 and Part 29, and EASA CS-23, CS-25. CS-27 and CS-29 certification standards.
G-10D Color Display Committee
Airstream Deviation Instrument (ADI)ARP794A (Current)2/16/2008
This recommended practice covers an instrument which measures and displays angle of deviation of the airstream dependent on mounting location on the aircraft.
A-4 Aircraft Instruments 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
Lighting, Integral, For Aircraft Instruments: Criteria for Design of Red Incandescent Lighted InstrumentsARP582D (Current)4/4/2012
This SAE Aerospace Recommended Practice (ARP) covers the general requirements and test procedures for illuminating systems for integrally lighted aircraft instruments in order to provide (a) uniformity of illumination within each instrument, (b) legibility of instrument presentation under daylight or integral light, and (c) uniformity of illumination between instrument displays.
A-20A Crew Station Lighting
Directional Indicating System (Turbine Powered Subsonic Aircraft)ARP416B (Current)4/14/2020
This recommended practice covers the requirements for gyroscopically stabilized Directional Indicating Systems, which will operate as a 1°/hour latitude corrected, free directional gyro or as a slaved gyro, magnetic compass with 1/2° accuracy.
A-4 Aircraft Instruments Committee
Plastic Sheet and Strip, Modified Vinyl, Foamed Closed CellAMS3635E (Current)1/16/2012
This specification covers a modified vinyl plastic foam in the form of sheet and strip up to 1-1/2 inches (38.1 mm) in nominal thickness.
AMS P Polymeric Materials Committee
Steel, Bars Aircraft Quality 0.95Cr - 0.20Mo (0.28 to 0.33C) (4130) NormalizedAMS6348F (Current)10/20/2023
This specification covers an aircraft-quality, low-alloy steel in the form of bars.
AMS E Carbon and Low Alloy Steels Committee
Aluminum Alloy, Alclad, Sheet 5.7Zn - 2.2Mg - 1.6Cu - 0.22Cr (Alclad 7475-T761) Solution and Precipitation Heat TreatedAMS4100G (Current)1/16/2024
This specification covers an aluminum alloy in the form of alclad sheet 0.040 to 0.249 inch (1.02 to 6.32 mm), inclusive, in nominal thickness (see 8.5).
AMS D Nonferrous Alloys Committee
Alloy Castings, Corrosion- and Heat-Resistant 66Ni - 29Cu - 4.0Si Solution TreatedAMS4893D (Current)8/1/2022
This specification covers a nickel-copper alloy in the form of castings.
AMS F Corrosion and Heat Resistant Alloys Committee
Bar, Rod, and Shapes Produced from 30% Glass Fiber Filled Polyamide-Imide (PAI) MaterialAMS3670/4D (Current)5/19/2021
This specification covers molded or extruded bar, rod, and shapes produced from a polyamide-imide (PAI) polymer filled with 30% glass fiber. This is designated as Grade 4 material per AMS3670.
AMS P Polymeric Materials Committee
TUBING, PLASTIC, FLEXIBLE, CONVOLUTED, ANNULAR POLYVINYLIDENE FLUORIDE (PVDF), THERMALLY STABILIZED, STANDARD CONVOLUTIONSAS81914/8C (Current)6/30/2025
AE-8C1 Connectors Committee
Standard Test Procedure and Limit Value for Shutoff Surge Pressure of Pressure Fuel Dispensing SystemsAS1284B (Current)7/17/2015
The test procedure and related limit value are intended to apply to fixed and mobile ground pressure fuel dispensing systems and to aerial refueling tankers.
AE-5C Aviation Ground Fueling Systems Committee
HOSE, AIR DUCT, FLEXIBLE, HELICAL, METALLIC WIRE, SUPPORTED (COVERED), SELF-EXTINGUISHINGAS1503B (Current)9/9/2025
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
WRENCH - PROPELLER SHAFT (SHAFT SIZES NO. 40-50-60)AS351B (Current)12/5/2012
AGE-2 Air Cargo
Hose Assemblies, Metal, Medium Pressure, High TemperatureAS1424H (Current)4/7/2020
This SAE Aerospace Standard (AS) covers medium-pressure, high-temperature, flexible, metal-hose assemblies suitable for operation in pneumatic systems up to 800 °F with excursion to 1200 °F for Class “B” and “N” and primarily for use on jet aircraft power plants. See 1.2.1 for recommended usage.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
FITTING END, BULKHEAD FLARED TUBE, FOR SEAL RING, STANDARD DIMENSIONS FOR, DESIGN STANDARDAS1099D (Current)12/13/2021
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Aluminum Alloy, Sheet and Plate Copper Manganese Magnesium (17 S-T)AMS4032C (Current)4/1/1946
AMS D Nonferrous Alloys 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
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
Powder, Chromium Carbide Plus Nickel-Chromium Alloy 75Cr3C2 + 25 (80Ni - 20Cr Alloy)AMS7875F (Current)5/12/2022
This specification covers a blend of chromium carbide and a nickel-chromium alloy in the form of powder.
AMS F Corrosion and Heat Resistant Alloys Committee
Cabin Emergency Exits Design and Operation - Transport Category AircraftARP488G (Current)12/4/2024
This ARP provides design and performance recommendations for emergency exits in the passenger cabin. This ARP does not apply to Crew Emergency Exits.
S-9B Cabin Interiors and Furnishings Committee
FITTING, TEE, STANDARD AND REDUCER, BULKHEAD ON RUN, FLARELESSAS1003K (Current)5/4/2022
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Steel Bars, Forgings, Mechanical Tubing, Rings and Stock for Forgings and Rings 0.78Cr - 1.8Ni - 0.35Mo - 0.20V (0.33 - 0.38C) (4335 Mod) Premium Aircraft Quality Consumable Electrode Vacuum RemeltedAMS6429K (Current)9/22/2023
This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, flash-welded rings, and stock for forging or flash-welded rings.
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
Items per page:
1 – 50 of 219528