Standard
AS882 Pin - Trim Control
1941-06-02
CURRENT
AS882-2
No scope available.
Search Results
Standard
Steel Tubing (Seamless for Machined Parts) 1.8ni 0.80cr 0.25mo (0.38 - 0.43c) Heat Treated (200,000 Tensile Strength)
2002-12-16
CURRENT
AMS6420
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 Tubing (Seamless for Machined Parts) .55ni .25mo (.33 - .38c) Normalized Or Heat-Treated (90,000 Tensile Strength)
2002-12-16
CURRENT
AMS6283
Standard
Steel Tubing (Seamless for Machined Parts) .55ni .50cr .25mo (.35 - .38c) Heat-Treated (125,000 Tensile Strength)
2002-12-16
CURRENT
AMS6284
Standard
Steel Tubing (Seamless for Machined Parts) .55ni .50cr .25mo (.38 - .43c) Heat-Treated (180,000 Tensile Strength)
2002-12-16
CURRENT
AMS6285
Standard
Steel Tubing (Seamless for Machined Parts) .55ni .50cr .25mo (.38-.43c) Heat-Treated (180,000 T.S.)
2002-12-16
CURRENT
AMS6286
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
CABIN CONNECTORS AND CABLES PART 2 SPECIFICATION OF CONNECTORS, CONTACTS, AND BACKSHELLS
2018-11-28
CURRENT
ARINC800P2-1
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
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
AS29600-699 Bolt, Externally Relieved Body - Dee Head DTD5077, 10(.190)-32UNJF - 3A BS4084
1972-01-12
CURRENT
AS29600-2
No scope available.
Standard
AIRCRAFT DATA NETWORK, PART 1, SYSTEMS CONCEPTS AND OVERVIEW
2019-06-20
CURRENT
ARINC664P1-2
The purpose of this document is to provide an overview of data networking standards recommended for use in commercial aircraft installations. These standards provide a means to adapt commercially defined networking standards to an aircraft environment. It refers to devices such as bridges, switches, routers and hubs and their use in an aircraft environment. This equipment, when installed in a network topology, can optimize data transfer and overall avionics performance.
Standard
OBSOLESCENCE MANAGEMENT STRATEGIES FOR COMMERCIAL AIRCRAFT
2019-05-14
CURRENT
ARINC662-1
The purpose of this document is to establish guidelines that should be observed during initial design, production, and maintenance of aircraft components, and to present short-term and long-term strategies to minimize the costs and impacts associated with decreasing availability of components.
