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, NITRIDING .65 Ni 1 Cr 1 Mo
1946-04-01
HISTORICAL
AMS6480
Standard
STEEL TUBING (WELDED) Chromium Molybdenum (.27 - .33 Carbon) (Normalized)
1942-06-01
HISTORICAL
AMS6510
Standard
STEEL Nickel Molybdenum
1939-12-04
HISTORICAL
AMS6315
Standard
STEEL Nickel Molybdenum
1942-03-01
HISTORICAL
AMS6315A
Standard
STEEL 1.8 Ni - .25 Mo (.38 - .43C) Heat Treated (105,000 TS)
1945-07-01
HISTORICAL
AMS6315B
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
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
ELECTRONIC FLIGHT BAG (EFB) APPLICATION CONTROL INTERFACE (ACI) FOR TABLET DEVICES
2019-08-23
CURRENT
ARINC840A
This document specifies how application to application navigation is managed on tablet EFB devices. Topics include: inter-application navigation for users, blending of multiple applications into a single workflow, single data entry with data shared across applications.
Standard
GUIDANCE FOR DISTRIBUTED RADIO ARCHITECTURES
2021-07-15
CURRENT
ARINC678
The purpose of this document is to evaluate Communication, Navigation, and Surveillance (CNS) Distributed Radio architectures and the feasibility of distributing the RF and systems processing sections to ensure the following: Reduce cost of equipment Reduce Size, Weight, and Power (SWaP) Ease of aircraft integration Growth capability built into the design Maintain or improve system availability, reliability, and maintainability It provides a framework to determine whether it is feasible to develop ARINC Standards that support CNS distributed radio architectures.
