Standard
AS882 Pin - Trim Control
1941-06-02
CURRENT
AS882-2
No scope available.
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SAE Aerospace Technical Papers Collection
2016-11-30
The Aerospace Technical Paper Collection is a family of technical papers as either an annual subscription (current papers, archived papers, or both) or a perpetual collection (1906-1997). This collection is perfect for aerospace engineers, managers, or educators who need access to the most current content covering today's most relevent topics. Please contact one of our sales representatives to learn more and start your subscription today! SAE Sales Team customersales@sae.org 1-888-875-3976 (U.S. and Canada) 1-724-772-4086 (Outside the U.S.)
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
Quality Management Systems - Nonconformance Documentation - Word Format
2007-09-26
AS9131AW
AS9131 - This standard defines the common nonconformance data definition and documentation that an internal or external supplier or sub-tier supplier must submit when informing a customer of a nonconformity. The requirements shall be are applicable for reporting a nonconforming product to the owner/operator (i.e., end item user), if specified by contract. Reporting of nonconformance data, either electronically or conventionally on paper, is subject to the terms and conditions of the contract. This also includes, where applicable, data access under export control regulations.
Standard
BITE GLOSSARY
1986-12-18
CURRENT
ARINC612
The purpose of this standard is to provide a source of definitions of terms and acronyms commonly used in the air transport maintenance community for test and evaluation with an emphasis on terms applicable to BITE.
Standard
TIMELY RECOVERY OF FLIGHT DATA (TRFD)
2021-08-06
CURRENT
ARINC681
The difficulty in locating crash sites has prompted international efforts for alternatives to quickly recover flight data. This document describes the technical requirements and architectural options for the Timely Recovery of Flight Data (TRFD) in commercial aircraft. ICAO and individual Civil Aviation Authorities (CAAs) levy these requirements. The ICAO Standards and Recommended Practices (SARPs) and CAA regulations cover both aircraft-level and on-ground systems. This report also documents additional system-level requirements derived from the evaluation of ICAO, CAA, and relevant industry documents and potential TRFD system architectures. It describes two TRFD architectures in the context of a common architectural framework and identifies requirements. This report also discusses implementation recommendations from an airplane-level perspective.
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.
