Standard
Steel Nickel Chromium
1941-03-01
CURRENT
AMS6337
No scope available.
Search Results
Standard
Steel Tubing, (Seamless), Round Chromium Molybdenum (.32 - .39 Carbon) (125,000 Tensile Strength)
2002-12-16
CURRENT
AMS6366
Standard
Steel Tubing, (Seamless), Round Chromium Molybdenum (.32 - .39 Carbon) (150,000 Tensile Strength)
2002-12-16
CURRENT
AMS6367
Standard
Steel Tubing, (Seamless), Round Chromium Molybdenum (.32 - .39 Carbon) (200,000 Tensile Strength)
2002-12-16
CURRENT
AMS6368
Standard
Steel Tubing, (Seamless), Round Chromium Molybdenum (.32 - .39 Carbon) (200,000 T.S.)
2002-12-16
CURRENT
AMS6369
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
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, 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
Nuts, Self-Locking, Steel High Strength, All Metal, 450°F Use, Unified "J" (MIL-S-8879) Thread Form
1990-10-01
CURRENT
AMS7252C
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.
Video
Vertical Picture-Frame Wing Jig Structure Design with an Eye to Foundation Loading
2012-03-14
The foundation of many production aircraft assembly facilities is a more dynamic and unpredictable quantity than we would sometimes care to admit. Any tooling structures constructed on these floors, no matter how thoroughly analyzed or well understood, are at the mercy of settling and shifting concrete, which can cause very lengthy and costly periodic re-certification and adjustment procedures. It is with this in mind, then, that we explore the design possibilities for one such structure to be built in Belfast, North Ireland for the assembly of the Shorts C-Series aircraft wings. We evaluate the peak floor pressure, weight, gravity deflection, drilling deflection, and thermal deflection of four promising structures and discover that carefully designed pivot points and tension members can offer significant benefits in some areas.
Collection
Auto Fastening/Assembly & Tooling, AeroTech 2015
2015-09-16
This collection of technical papers covers advanced portable semi-automated drilling and fastening systems and portable crawler/flex track systems; assembly methodologies and advanced assembly fixtures and tooling; composites assembly and fastening; composte/heavy metal drilling and assembly; large component assembly, sub-assembly, major section join and final assembly; robotic applications in drilling, fastening and assembly; and advancements in drill bit, temporary and permanent fastening technology.
Standard
COTTER PINS, METRIC Corrosion and Heat Resistant Steel 18Cr - 10.5Ni - 0.40Ti
1993-10-01
MAM7211C
Standard
COTTER PINS, METRIC, STEEL, CORROSION AND HEAT RESISTANT 18Cr - 10.5Ni - 0.40Ti
1983-04-01
MAM7211A
This specification covers cotter pins made to metric dimensions from a corrosion and heat resistant steel.
