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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
STUD, STEPPED - 2.5 DIA ENGAGEMENT, PD SHANK, UNS S66286 .3750-24 UNJF-3A X .3125-24 UNJF-3AAS3141C (Current)3/23/2026
E-25 General Standards for Aerospace and Propulsion Systems
BOLT, MACHINE - HEXAGON HEAD, DRILLED 6 HOLES, PD SHANK, AMS5731, UNS S66286, .375-24 UNJF-3AAS3117B (Current)3/23/2026
E-25 General Standards for Aerospace and Propulsion Systems
BOLT, MACHINE - HEXAGON HEAD, DRILLED 6 HOLES, PD SHANK, UNS S66286, .5625-18 UNJF-3AAS3120B (Current)3/23/2026
E-25 General Standards for Aerospace and Propulsion Systems
BOLT, MACHINE - HEXAGON HEAD, DRILLED 6 HOLES, PD SHANK, AMS5731, UNS S66286, .4375-20 UNJF-3AAS3118B (Current)3/23/2026
E-25 General Standards for Aerospace and Propulsion Systems
STUD, STEPPED - 2.5 DIA ENGAGEMENT, PD SHANK, UNS S66286 .3125-24 UNJF-3A X .2500-28 UNJF-3AAS3140C (Current)3/23/2026
E-25 General Standards for Aerospace and Propulsion Systems
BOLT, MACHINE - HEXAGON HEAD, DRILLED 6 HOLES, PD SHANK, CRES (UNS S66286), .5000-20 UNJF-3AAS3119B (Current)3/23/2026
E-25 General Standards for Aerospace and Propulsion Systems
STUD, STEPPED - 2.5 DIA ENGAGEMENT, PD SHANK, UNS S66286 .2500-28 UNJF-3A X .1900-32 UNJF-3AAS3139C (Current)3/23/2026
E-25 General Standards for Aerospace and Propulsion Systems
Shaft Nut and Keywasher Installation Dimensions forAS1495B (Current)3/20/2026
The purpose of this Standard is to provide installation dimensions for shaft nuts and their companion keywasher. The Standard type typically shown on MS9951 and MS9952, but is also suitable for parts which are dimensionally equivalent.
E-25 General Standards for Aerospace and Propulsion Systems
STUD - STRAIGHT, DRILLED, .2500-20UNS X .2500-28UNF-3AAS128363B (Current)3/20/2026
E-25 General Standards for Aerospace and Propulsion Systems
NUT, SPANNER, AERONAUTICAL, UNS G41400AS172321B (Current)3/20/2026
E-25 General Standards for Aerospace and Propulsion Systems
STUD, LOCKED IN - RING, STRAIGHT, HOLE PREPARATION FORAS1620A (Current)3/20/2026
E-25 General Standards for Aerospace and Propulsion Systems
STUD - STRAIGHT, NECKED, .3750-16UNS X .3750-24UNF-3AAS126881B (Current)3/20/2026
E-25 General Standards for Aerospace and Propulsion Systems
STUD - STRAIGHT, WAISTED, .4375-14 X .4375-20UNF-3AAS127193B (Current)3/20/2026
E-25 General Standards for Aerospace and Propulsion Systems
STUD - STRAIGHT, DRILLED, STEEL (SAE 8740), CADMIUM PLATED, .3750-16UNS X .3750-24UNF-3AAS129293B (Current)3/20/2026
E-25 General Standards for Aerospace and Propulsion Systems
RING, RETAINING-SPIRAL, EXTERNAL, LIGHT DUTY, CRESAS3218C (Current)3/20/2026
E-25 General Standards for Aerospace and Propulsion Systems
RING, RETAINING-SPIRAL, EXTERNAL, HEAVY DUTY, CRES (UNS S30200)AS3216C (Current)3/20/2026
E-25 General Standards for Aerospace and Propulsion Systems
STUD - STRAIGHT, DRILLED, .3125-18UNS X .3125-24UNF-3AAS128687B (Current)3/20/2026
E-25 General Standards for Aerospace and Propulsion Systems
Cloth, Monofilament, NettingAMS3790B (Current)10/1/1995
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1995.
AMS P Polymeric Materials Committee
Glass Sheet, Barium Aluminum Borosilicate for Electronic ApplicationsAMS3883A (Current)10/1/1995
No scope available.
AMS P Polymeric Materials Committee
Cloth, Type "E" Glass "B" Stage Epoxy Resin Impregnated Style 181 - 75deAMS3822A (Current)6/1/1996
This specification has been 'CANCELLED' by the Aerospace Materials Division, SAE, as of June, 1996.
AMS P17 Polymer Matrix Composites Committee
Night Vision Goggles (NVG) Compatible Lighting for Civil AircraftAS5452C (Current)3/13/2026
This SAE Aerospace Standard (AS) will specify what type of NVGs are required and minimum requirements for compatible crew station lighting, aircraft exterior lighting such as anti-collision lights, and position/navigation lights that are “NVG compatible.” Also, this document is intended to set standards for NVG utilization for aircraft so that special use aircraft such as the Coast Guard, Border Patrol, Air Rescue, Police Department, Medivacs, etc., will be better equipped to chase drug smugglers and catch illegal immigrants, rescue people in distress, reduce high-speed chases through city streets by police, etc. Test programs and pilot operator programs are required. For those people designing or modifying civil aircraft to be NVG compatible, the documents listed in 2.1.3 are essential.
A-20A Crew Station Lighting
Cord, Coreless, Para-Aramid, Intermediate ModulusAMS3814A (Current)2/1/1996
This specification has been 'CANCELLED' by the Aerospace Materials Division, SAE, as of February 1996.
AMS P Polymeric Materials Committee
Aluminum Alloy, Castings, High Strength, 4.5cu 0.70ag 0.30mn 0.25mg 0.25ti, Solution and Precipitation Heat TreatedAMS4228B (Current)4/1/1996
This specification has been 'CANCELLED' by the Aerospace Materials Division, SAE, as of April 1996. Alloy: A201.0-T6 UNS Number: A12010
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Castings, Sand, 4.5cu, Solution TreatedAMS4230D (Current)11/1/1995
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of November 1995.
AMS D Nonferrous Alloys Committee
Asbestos Felting, "B" Stage Phenolic Resin Impregnated, Low Pressure MoldingAMS3858E (Current)10/1/1995
No scope available.
AMS P Polymeric Materials Committee
Cloth, Chloroprene (Cr) Coated NylonAMS3850B (Current)10/1/1995
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1995.
AMS CE Elastomers Committee
Steel, Corrosion and Heat Resistant, Covered Welding Electrodes 25cr 20niAMS5695G (Current)6/1/2000
This specification covers a corrosion and heat resistant steel in the form of covered welding electrodes.
AMS F Corrosion and Heat Resistant Alloys Committee
Aluminum Alloy, Castings, Sand, 4cu 2ni 1.5mg 0.2cr, Solution Treated and OveragedAMS4220E (Current)11/1/1995
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of November 1995.
AMS D Nonferrous Alloys Committee
Magnesium Wire, Welding 14li 1.25alAMS4397A (Current)9/1/1996
This specification has been 'CANCELLED' by the Aerospace Materials Division, SAE, as of September 1996. Alloy: LA141A UNS Number: M14141
AMS D Nonferrous Alloys Committee
Aluminum Wire, 99.0Al Minimum (1100-H18)AMS4180G (Current)7/13/2007
This specification covers an aluminum alloy in the form of wire.
AMS D Nonferrous Alloys Committee
ALUMINUM ALLOY WELDING WIRE 4.5Cu - 0.70Ag - 0.30Mn - 0.25Mg - 0.25Ti (A201.0)AMS4188/1 (Current)12/16/2002
This specification covers an aluminum alloy in the form of extruded or drawn welding wire.
AMS D Nonferrous Alloys Committee
Cotter Pins, Medium Carbon Steel Zinc PlatedAMS7213 (Current)12/16/2002
AMS F Corrosion and Heat Resistant Alloys Committee
Bars and Forgings, 14cr 4.0mo (1.00-1.10c)AMS5619A (Current)7/1/2000
Primarily for parts requiring resistance to both corrosion and wear with hardness retained during exposure to temperatures up to 600 F (316 C).
AMS F Corrosion and Heat Resistant Alloys Committee
Coating, Interior Aircraft Cabin Low Heat and Smoke ReleaseAMS3146 (Current)9/1/2000
This specification covers interior aircraft cabin coatings, which when tested under specified conditions exhibit low heat release and smoke release properties.
AMS G8 Aerospace Organic Coatings 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
Sealing, Fluorocarbon Rubber High Temperature Fluid Resistant 85-95AMS7279G (Current)5/1/1995
This specification has been declared "SUPERSEDED" by the Aerospace Materials Division, SAE, as of 10/17/90.
AMS CE Elastomers Committee
Bar, Sheet, Strip, and Plate, Iron, Commercially Pure, Hot Rolled, AnnealedAMS7706B (Current)2/1/1995
This specification has been Cancelled by the Aerospace Materials Division, as of January 1995.
AMS E Carbon and Low Alloy Steels Committee
Cord, Coreless, Para-Aramid Intermediate Modulus 300 Lb (1335 N), 1500 Ft Per Lb (1005 M/Kg)AMS3814/15A (Current)2/1/1996
This specification has been 'CANCELLED' by the Aerospace Materials Division, SAE, as of February 1996.
AMS P Polymeric Materials Committee
Castings, Alloy-Investment, 61ni 16cr 8.5co 1.8mo 2.6w 0.8cb 3.4ti 1.8ta 3.4al 0.010b 0.06zr (0.03-0.08c), Vacuum Melted, Vacuum Cast, as CastAMS5409A (Current)8/21/2002
This specification covers a corrosion and heat resistant nickel alloy in the form of investment castings.
AMS F Corrosion and Heat Resistant Alloys Committee
Steel Tubing, (Seamless), Round Chromium Molybdenum (.32 - .39 Carbon) (200,000 Tensile Strength)AMS6368 (Current)12/16/2002
AMS E Carbon and Low Alloy Steels Committee
ALUMINUM ALLOY WELDING WIRE 4.6Cu - 0.35Mn - 0.25Mg - 0.22Ti (A206.0)AMS4188/2 (Current)12/16/2002
This specification covers an aluminum alloy in the form of extruded or drawn welding wire.
AMS D Nonferrous Alloys Committee
Selective (Brush) Nickel Plating Low-Stressed, Low Hardness DepositAMS2441A (Current)10/1/2000
This specification covers the engineering requirements for selective (brush) electrodeposition of nickel and the properties of the deposit. This process has been used typically to provide moderate corrosion and oxidation resistance and dimensional build-up and restoration of parts which may operate in service up to 700 degrees F (371 degrees C), where low tensile stress in the deposit is required to avoid marked reduction of fatigue strength, but usage is not limited to such applications.
AMS B Finishes Processes and Fluids Committee
Evaluation of Coking Propensity of Aviation Lubricants in an Air-Oil Mist Environment Using the Vapor Phase CokerARP5921A (Current)3/13/2026
This method is designed to evaluate the coking propensity of synthetic ester-based aviation lubricants under two phase air-oil mist conditions as found in certain parts of a gas turbine engine, for instance, bearing chamber vent lines. Based on the results from round robin data in 2008 to 2009 from four laboratories, this method is currently intended to provide a comparison between lubricants as a research tool; it is not currently a satisfactory pass/fail test.
E-34 Propulsion Lubricants Committee
Counterfeit Materiel; Assuring Acquisition of Authentic and Conforming MaterielAS6174B (Current)2/17/2026
This SAE Standard provides requirements and guidance to: Develop a Materiel authenticity plan. Procure Materiel from reliable sources. Assure authenticity and conformance of procured Materiel, including methods such as certification, traceability, testing, and inspection appropriate to the Commodity/item in question. Control Materiel identified as counterfeit. Report Suspect or Counterfeit Materiel to other potential users and Authorities Having Jurisdiction.
G-21 Counterfeit Materiel Committee
Cloth, Aramid, 2.25 oz per sq yd (76.3 g/m2), 250 Pounds Force per Inch (43782 N/m)AMS3909/2A (Current)10/4/2022
This specification covers one weight and one strength of intermediate modulus aramid cloth.
AMS P17 Polymer Matrix Composites Committee
Cloth, Aramid 2.0 oz per sq yd (68 g/m2), 230 Pounds Force per Inch (40279 N/m) (Warp) and 220 Pounds Force per Inch (38528 N/m) (Filling)AMS3909/3A (Current)10/4/2022
This specification covers one weight and one strength of intermediate modulus aramid cloth.
AMS P17 Polymer Matrix Composites Committee
Cloth, Aramid 3.0 oz per sq yd (102 g/m2), 350 Pounds Force per Inch (61294 N/m)AMS3909/1A (Current)10/4/2022
This specification covers one weight and one strength of intermediate modulus aramid cloth.
AMS P17 Polymer Matrix Composites Committee
Glazed Ceramic Sheet 95% AluminaAMS3871C (Current)10/1/1995
This specification has been declared "NONCURRENT" by the Aerospace Materials Division, SAE, as of July, 1992.
AMS P Polymeric Materials Committee
FLUORESCENT PENETRANT INSPECTIONAMS2645K (Current)2/1/1995
AMS K Non Destructive Methods and Processes Committee
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