Standard
Steel Tubing, (Seamless), Round Chromium Molybdenum (.32 - .39 Carbon) (200,000 T.S.)
2002-12-16
CURRENT
AMS6369
Search Results
Standard
Steel Tubing (Seamless), Round Chromium Molybdenum (0.27 - 0.33 Carbon) (180,000 Tensile Strength - 0.156 Maximum Wall Thickness)
2002-12-16
CURRENT
AMS6363
Standard
Steel Corrosion and Heat Resistant 19cr 12ni 3.2w 1cb 0.15n
2002-12-16
CURRENT
AMS5730
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
Cotter Pins, Medium Carbon Steel Zinc Plated
2002-12-16
CURRENT
AMS7213
Standard
Nuts, Self-Locking, Steel High Strength, All Metal, 450°F Use, Unified "J" (MIL-S-8879) Thread Form
1990-10-01
CURRENT
AMS7252C
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
Method for Evaluating the Cleavage Strength of Structurally Bonded Fiberglass Reinforced Plastic (Wedge Test)
1987-10-01
CURRENT
J1882_198708
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
CABIN CONNECTORS AND CABLES PART 2 SPECIFICATION OF CONNECTORS, CONTACTS, AND BACKSHELLS
2021-09-09
CURRENT
ARINC800P2-2
This specification describes the general connectors, contacts, and backshells in their shape and characteristic for cabin systems for commercial aircrafts. ARINC 600, ARINC 404, and ARINC 801 connector specifications are published as independent standards.
Standard
Manufacturing Message Specification – Service Definition and Protocol
2016-06-28
CURRENT
EIA511
The Manufacturing Message Specification is an application layer Standard designed to support messaging communications to and from programmable devices in a Computer Integrated Manufacturing (CIM) environment. This environment is referred to in this Standard as the manufacturing environment. This Standard does not specify a complete set of services for remote programming of devices, although provision of such a set of services may be the subject of future standardization efforts.
Standard
AIRCRAFT SOFTWARE COMMON CONFIGURATION REPORTING
2019-08-13
CURRENT
ARINC843-1
This standard defines a common configuration report format that can be retrieved from an aircraft for use by ground tools and maintenance personnel. Reports will be generated in Extensible Markup Language (XML) format and structured as defined by this document. Several optional elements and attributes are defined to allow flexibility for a given report. This standard provides aircraft manufacturers, regulatory agencies, and airlines a format standard for aircraft configuration reporting, and facilitates automated comparison of configuration data reports (e.g., authorized versus as flying, etc.).
