Search Results

Referee Material

AMS-STD-595A/10032

2016-05-01

AMS-STD-595A Color Chips Precise Color Matching, Individual Color Chips: A 3 x 5 inch color chip supplied in a 3 x 5 inch protective envelope for each AMS-STD-595 color, suitable for matching quality control inspection purposes. SAE Product Code: EA-10032 AMS-STD-595 – Colors Used in Government Procurement. This standard presents the colors used by Government Activities in a format suitable for color selection matching and for quality control inspection for paints and coatings. Standard is used with DoD and other Federal Agencies as a primary source of color reference.

Book

Honda R&D Technical Review April 2021

2021-04-01

Honda R&D Technical Review is a periodical containing research papers related to Honda R&D Center activities worldwide that cover automobile, motorcycle, power products, aircraft engine, and other fundamental technologies. Honda Motor offers a book for the April 2021 issue with 104 pages containing 12 papers focusing on the following latest topics: Technology for Prediction of Contactor Noise for Electric-powered Vehicle Batteries Reduction of Internal Resistance in High Capacity Lithium-ion Batteries with 3D Lattice-structured Electrode Predictive Technique for Seat Belt Submarining Injury by Triaxial Iliac Load Cell

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

AMS6310

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

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

Vehicle Electronic Identification

2002-07-23

CURRENT

J1724_200207

Standard

Hydraulic Backhoe Basic Operating Control Arrangements

2002-07-23

CURRENT

J1358_200207

Standard

Fuel Fired Engine Preheaters and Their Application

2002-12-16

CURRENT

J1327_200212

Standard

Definitions and Glossary of Terms for Tower Cranes

2002-07-23

CURRENT

J1408_200207

Standard

Remote and Automatic Control Systems for Construction and Industrial Machinery

2002-12-16

CURRENT

J956_200212

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

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

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.).