Standard
Alloy Sheet and Strip, Corrosion and Heat Resistant Cobalt Base 25.5cr 20ni 4mo 2w 2(Cb+Ta)
2002-12-16
CURRENT
AMS5535
Search Results
Standard
Magnesium Alloy Sheet Aluminum Zinc (Hard)
2002-12-16
CURRENT
AMS4381
Standard
STEEL Nickel Molybdenum
1939-12-04
HISTORICAL
AMS6310
Standard
STEEL Nickel Molybdenum
1939-12-04
HISTORICAL
AMS6315
Standard
STEEL Nickel Molybdenum
1942-03-01
HISTORICAL
AMS6315A
Standard
Alloy, Corrosion and Heat Resistant 37ni 20co 18cr 3mo 2.9ti
1949-01-01
CURRENT
AMS5760
Parts, such as bolts, turbine wheels, discs, buckets, and blades, for high strength and oxidation resistance up to 1500 F when suitably heat treated.
Standard
STEEL COTTER PINS, GALVANIZED Low Carbon
1942-12-01
CURRENT
AMS7212
Standard
NUTS, SELF-LOCKING, STEEL High Strength, Prevailing-Torque, All Metal 450 F (232 C) Use, Unified "J" (MIL-S-8879) Thread Form
1969-11-01
HISTORICAL
AMS7252
Standard
NUTS, SELF-LOCKING, STEEL High Strength, All Metal 450° F (230° C) Use, Unified "J" (MIL-S-8879) Thread Form
1980-01-15
HISTORICAL
AMS7252B
This specification covers all-metal, self-locking nuts, plate nuts, and gang channel nuts made of a carbon or low-alloy steel.
Standard
NUTS, SELF-LOCKING, STEEL High Strength, Prevailing Torque, All Metal 450° F (232° C) Use, Unified "J" (MIL-S-8879) Thread Form
1973-05-15
HISTORICAL
AMS7252A
This specification covers all-metal, self-locking, prevailing-torque nuts, plate nuts, and gang channel nuts made of a carbon or low-alloy steel.
Standard
BOLTS AND SCREWS, TITANIUM ALLOY 6Al - 4V Upset Headed, Heat Treated, Roll Threaded
1973-05-15
HISTORICAL
AMS7461B
This specification covers premium quality bolts and screws made of 6Al - 4V titanium alloy.
Standard
BOLTS AND SCREWS, TITANIUM ALLOY 6Al - 4V Upset Headed, Heat Treated, Roll Threaded
1970-11-01
HISTORICAL
AMS7461A
Standard
BOLTS AND SCREWS, TITANIUM ALLOY 6Al - 4V Upset Headed, Heat Treated, Roll Threaded
1964-06-30
HISTORICAL
AMS7461
Standard
TOLERANCES, METRIC Aluminum Alloy Drawn Tubing
1994-09-01
MAM2203B
Standard
TOLERANCES, METRIC Aluminum Alloy Drawn Tubing
1994-04-01
MAM2203A
This specification covers established metric manufacturing tolerances applicable to aluminum alloy drawn tubing ordered to metric dimensions. These tolerances apply to all conditions, unless otherwise noted. The term "excl" applies only to the higher figure of the specified range.
Standard
TOLERANCES, METRIC Aluminum Alloy Drawn Tubing
2002-07-23
MAM2203
This specification covers established metric manufacturing tolerances applicable to aluminum alloy drawn tubing ordered to metric dimensions. These tolerances apply to all conditions, unless otherwise noted. The term "excl" applies only to the higher figure of the specified range.
Standard
Nickel Alloy, Corrosion and Heat Resistant, Sheet, Strip, and Plate 72Ni - 15.5Cr - 0.95 (Cb + Ta) - 2.5Ti - 0.70Al - 7.0Fe Consumable Electrode or Vacuum Induction Melted Solution Heat Treated, Precipitation Hardenable
2000-05-01
HISTORICAL
MAM5598B
This specification covers a corrosion and heat resistant nickel alloy in the form of sheet, strip, and plate procured in SI (metric) units.
Standard
NICKEL ALLOY, CORROSION AND HEAT RESISTANT, SHEET, STRIP, AND PLATE 72Ni - 15.5Cr - 0.95(Cb + Ta) - 2.5Ti - 0.70Al - 7.0Fe Consumable Electrode or Vacuum Induction Melted Solution Heat Treated, Precipitation Hardenable
1993-07-01
HISTORICAL
MAM5598A
This specification covers a corrosion and heat resistant nickel alloy in the form of sheet, strip, and plate procured in SI (metric) units.
Standard
ALLOY SHEET, STRIP, AND PLATE, CORROSION AND HEAT RESISTANT 72Ni - 15.5Cr - 0.95(Cb + Ta) - 2.5Ti - 0.70Al - 7.0Fe Consumable Electrode or Vacuum Induction Melted Solution Heat Treated, Precipitation Hardenable
1991-10-01
HISTORICAL
MAM5598
This specification covers a corrosion and heat resistant nickel alloy in the form of sheet, strip, and plate procured in SI (metric) units. AMS 5598 is the equivalent, specified in inch/pound units, of this MAM.
Standard
AIRCRAFT AUTONOMOUS DISTRESS TRACKING (ADT)
2019-08-26
CURRENT
ARINC680
This document describes the technical requirements, architectural options, and recommended interface standards to support an Autonomous Distress Tracking (ADT) System intended to meet global regulatory requirements for locating aircraft in distress situations and after an accident. This document is prepared in response to International Civil Aviation Organization (ICAO) and individual Civil Aviation Authorities (CAAs) initiatives.
