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 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
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
CABIN CONNECTORS AND CABLES, PART 4, STANDARD TEST METHODOLOGY
2020-07-13
CURRENT
ARINC800P4-1
ARINC 800 is the first industry standard intended for characterization of aviation-grade high-speed (Gbps) Ethernet links. The test methods are based on realistic representation of cabin networks. The notional cabling architecture is based on IFE seat distribution using multiple intermediate disconnects. Sequential testing is supported by building up number of connectors in the link. Test guidelines for mixed intermediate cable lengths are provided.
Standard
AS4751 Lid Assembly - Flush Filler Cap MK.II
1958-07-17
CURRENT
AS4751-1
No scope available.
Standard
Design and Operation of Hydraulic Brake Systems With Skid Control
1980-12-01
CURRENT
ARP812
Standard
AS6369 Seal
1956-04-06
CURRENT
AS6369-3
No scope available.
Video
Ice Phobic Coatings for Control and Covered Surfaces
2012-03-14
Silicones have been utilized in multiple industries in the last 50 years and their applications are still expanding as technology grows. Ice phobic coatings, as an example, have been utilized on lock walls, navigation channels, wind turbines, hydropower intakes, and aircraft. Without protection these applications have a high risk of failure in the functions they perform. For example, ice build up on an aircraft?s aerodynamic surfaces increases drag which reduces lift during flight operations. Utilizing a silicone ice phobic coating significantly reduces the adhesion of ice to aerodynamic surfaces. Compared to other polymeric materials, silicones are known for their broad operating temperature range and lend themselves to excellent performance in a variety of harsh environments. Especially in low temperatures where ice adhesion is a concern, silicones retain their elastomeric physical properties and low modulus.
