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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
POLYTETRAFLUOROETHYLENEAMS3651D (Current)12/1/1994
AMS P Polymeric Materials Committee
POTTING COMPOUND, EPOXY, FLEXIBLE Durometer 75 - 85AMS3750 (Current)12/1/1994
AMS P Polymeric Materials Committee
Bolts and Screws, Nickel Alloy, Corrosion and Heat Resistant, Upset Headed, Heat Treated, Roll Threaded, 1950°F Solution Heat Treatment (AMS 5708)AMS7471G (Current)10/1/1993
AMS F Corrosion and Heat Resistant Alloys Committee
Bolts and Screws Nickel Alloy, Corrosion and Heat Resistant, Upset Headed, Roll Threaded, Fatigue ResistantAMS7466B (Current)10/1/1993
AMS F Corrosion and Heat Resistant Alloys Committee
PLASTIC ROD AND BAR, POLYIMIDE Unfilled, MoldedAMS3644/1 (Current)9/1/1994
This specification covers an unfilled polyimide plastic in the form of molded rod and bar.
AMS P Polymeric Materials Committee
Cotter Pins, Steel 18cr 10.5ni 0.40ti, Corrosion and Heat Resistant SteelAMS7211G (Current)10/1/1993
AMS F Corrosion and Heat Resistant Alloys Committee
Fabric-Wire Reinforced Asbestos, Polytetrafluoroethylene Impregnated, SinteredAMS3839E (Current)7/1/1992
No scope available.
AMS P Polymeric Materials Committee
SEALING COMPOUND, LOW ADHESION, CORROSION INHIBITING 9,000 to 14,000 Poises (900 to 1400 Pa·s), 2 Hour Application Time (B-2)AMS3267/4A (Current)4/1/1992
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
POTTING COMPOUND, EPOXY, FILLED 15 – 20 CTE, 180 HDTAMS3738 (Current)12/1/1994
AMS P Polymeric Materials Committee
Tape, Nylon, Nonmelting, Reinforcing 2 (50) Wide, 3000 (13,345 N) Breaking StrengthAMS3777/9B (Current)10/1/1995
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1995.
AMS P Polymeric Materials Committee
Pins, Spring, Tubular-Corrosion and Moderate Heat Resistant Steel (Ams 5506)AMS7207H (Current)10/1/1993
AMS E Carbon and Low Alloy Steels Committee
Cord, Coreless, Para-Aramid Intermediate Modulus 5000 Lb (22,240 N), 58 Ft Per Lb (40 M/Kg)AMS3814/11A (Current)2/1/1996
This specification has been 'CANCELLED' by the Aerospace Materials Division, SAE, as of February 1996.
AMS P Polymeric Materials Committee
Bolts and Screws, Titanium Alloy 6al 4v, Heat Treated, Roll ThreadedAMS7460E (Current)5/1/1995
AMS G Titanium and Refractory Metals Committee
Inserts, Thread Form, Corrosion and Heat Resistant Alloy 72ni 15.5cr 0.95(Cb + Ta) 2.5ti 0.70al 7.0feAMS7246B (Current)10/1/1993
AMS F Corrosion and Heat Resistant Alloys Committee
Plastic Rod and Bar, Polyimide, Graphite/Ptfe Filled, Molded, 15/10AMS3644/2C (Current)9/1/1994
This specification has been declared "SUPERSEDED" by the Aerospace Materials Division, SAE, as of September 1994. The requirements of this specification are embodied in the latest issue of AMS 3644 class/form 4M.
AMS P Polymeric Materials Committee
Studs Steel, Low-Alloy Heat Resistant, Normalized and Tempered, Roll Threaded, 135,000 Psi (931 Mpa) Tensile StrengthAMS7458G (Current)10/1/1993
UNS Number: K14675
AMS E Carbon and Low Alloy Steels Committee
Studs, Low-Alloy Steel Heat Treated, Rolled Threaded (Uns G87400)AMS7456K (Current)10/1/1993
AMS E Carbon and Low Alloy Steels Committee
SEALING COMPOUND, LOW ADHESION, CORROSION INHIBITING 9,000 to 14,000 Poises (900 to 1400 Pas 1/2 Hour Application Time (B-1/2)AMS3267/2A (Current)4/1/1992
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
Cord, Aromatic Polyamide, Nonmelting 550 Pounds (2445 N), 165 Foot/Pound (110 M/Kg)AMS3853/3B (Current)10/1/1995
No scope available.
AMS P Polymeric Materials Committee
Bolts and Screws Steel, Low-Alloy, Heat Treated, Roll ThreadedAMS7452M (Current)10/1/1993
AMS E Carbon and Low Alloy Steels Committee
Cotter Pins, Steel, Corrosion-Resistant 18cr 9.5niAMS7210H (Current)10/1/1993
AMS F Corrosion and Heat Resistant Alloys Committee
Rivets, Steel, Corrosion and Heat Resistant 18cr 10.5ni (Cb + Ta) Solution Heat TreatedAMS7229H (Current)10/1/1993
AMS F Corrosion and Heat Resistant Alloys Committee
Rivets-Carbon SteelAMS7225G (Current)10/1/1993
AMS E Carbon and Low Alloy Steels Committee
STUDS, CORROSION AND HEAT RESISTANT STEEL Heat Treated, Roll ThreadedAMS7481B (Current)5/1/1995
AMS F Corrosion and Heat Resistant Alloys Committee
Cord, Coreless, Para-Aramid Intermediate Modulus 1500 Lb (6670 N), 200 Ft Per Lb (135 M/Kg)AMS3814/8A (Current)2/1/1996
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of February 1996.
AMS P Polymeric Materials Committee
BOLTS AND SCREWS, WORK-STRENGTHENED ALLOY, CORROSION RESISTANT Forged Head, Roll Threaded After AgingAMS7468 (Current)5/1/1995
This specification covers aircraft-quality bolts and screws having UNJ (MIL-S-8879) thread form, made from a corrosion-resistant, work-strengthened cobalt-chromium-nickel alloy and aged to develop the specified properties.
AMS F Corrosion and Heat Resistant Alloys Committee
Tolerances, Metric, Aluminum Alloy and Magnesium Alloy Sheet and PlateMAM2202C (Current)8/1/1996
This specification covers established manufacturing tolerances applicable to aluminum alloy and magnesium alloy sheet and plate ordered to metric dimensions. These tolerances apply to all conditions, unless otherwise noted. These tables are based on logical metric values and preferred metric sizes. Throughout this specification, the term 'metric' is intended to refer to the SI system.
AMS D Nonferrous Alloys Committee
Brazing Silver, for Flexible Metal Hose 800°F (425°C) Max Operating TemperatureAMS2669D (Current)4/1/1992
This specification has been declared "SUPERSEDED" by the Aerospace Materials Division, SAE, as of October, 1991.
AMS B Finishes Processes and Fluids Committee
TITANIUM ALLOY BARS 11.5Mo - 6.0Zr - 4.5Sn 1375°F (745°C) Solution Heat TreatedAMS4980B (Current)4/1/1992
AMS G Titanium and Refractory Metals Committee
Sheet, Strip and Plate Molybdenum, Arc Cast, Stress RelievedAMS7801B (Current)4/1/1992
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of December, 1991.
AMS G Titanium and Refractory Metals Committee
Cloth, Nylon, Metallized, UntreatedAMS3848/1B (Current)10/1/1995
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1995.
AMS P Polymeric Materials Committee
Tolerances, Aluminum Alloy Standard Structural ShapesAMS2204H (Current)8/1/1996
This specification has been declared 'NONCURRENT' by the Aerospace Materials Division, SAE, as of September 1994. It is recommended, therefore, that this specification not be specified for new designs.
AMS D Nonferrous Alloys Committee
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