Standard
BOLT, TEE HEAD - NICKEL ALLOY (UNS N07718), CHAMFERED, .3125-24 UNJF-3A (STRESS RUPTURE RESISTANT)
2024-04-24
CURRENT
AS3411E
Search Results
Standard
Rivets, Solid, UNS N04400, Corrosion Resistant 67Ni - 31Cu Procurement Specification for
2024-04-23
CURRENT
AS7233A
This procurement specification covers aircraft-quality solid rivets made from a corrosion resistant nickel-copper alloy of the type identified under the Unified Numbering System as UNS N04400 and of 46 ksi minimum shear strength.
Standard
Rivets, Blind, Corrosion Resistant Alloy 67Ni - 31Cu Procurement Specification For
2024-04-23
CURRENT
AS7234A
This procurement specification covers tubular, blind rivets fabricated from a corrosion resistant nickel-copper alloy of the type identified under the Unified Numbering System as UNS N04405, and of 52 ksi minimum shear strength for self-plugging style rivets.
Standard
NUT, PLAIN, HEXAGON, CADMIUM PLATED, UNS G87400, 125 KSI MIN
2024-04-23
CURRENT
AS9881C
Standard
PIN, STRAIGHT, HEADED, .0937 DIAMETER, UNS S41800
2024-04-23
CURRENT
AS9842B
Standard
Rivets, UNS S66286, Steel, Corrosion and Heat Resistant, 80 ksi Shear Strength, Procurement Specification for
2024-04-23
CURRENT
AS7235A
This procurement specification covers solid rivets and hollow end rivets made from a corrosion and heat resistant steel of the type identified under the Unified Numbering System as UNS S66286 and of 80 ksi single shear strength at room temperature.
Standard
Lubricant, Solid Film, Heat Cured, Corrosion Inhibiting, Procurement Specification
2024-04-09
WIP
AS5272G
This SAE Aerospace Standard (AS) establishes the requirements for heat cured solid film lubricants. For other general or high temperature applications, refer to AS1701. This document requires qualified products.
Standard
Development of Procurement Specification for Helical Thread Inserts using UNS S21800 (Nitronic 60) Material
2024-04-08
WIP
AS8637
This document aims to define the procurement requirements for helical coil threaded inserts manufactured from corrosion-resistant steel formed wire, with the chemical composition aligning with UNS S21800. It will enable insert manufacturers to adhere to specific standards to meet the criteria outlined in this procurement specification.
Standard
Guidelines for Characterization of Gas Turbine Engine Total-Pressure, Planar-Wave, and Total-Temperature Inlet-Flow Distortion
2024-04-02
WIP
ARP6420A
The turbine-engine-inlet flow distortion descriptors summarized in this document apply to the effects of inlet total-pressure, planar-wave, and total-temperature distortions. Guidelines on stability margin, destabilizing influences, types and purposes of inlet data, AIP definition, and data acquisition and handling are summarized from AIR5866, AIR5867, ARP1420, and AIR1419. The degree to which these recommendations are applied to a specific program should be consistent with the complexity of the inlet/engine integration. Total-pressure distortion is often the predominant destabilizing element that is encountered and is often the only type of distortion to be considered, i.e, not all types of distortion need to be considered for all vehicles.
Standard
Pins, Cotter, Steel, Corrosion Resistant UNS S30200 Procurement Specification for
2024-04-01
CURRENT
AS7210B
This procurement specification covers split cotter pins with optional ends (see Figure 1), made from a corrosion resistant steel of the type identified under the Unified Numbering System as UNS S30200.
Standard
Pins, Cotter, Steel, Corrosion and Heat Resistant UNS S32100 Procurement Specification
2024-04-01
CURRENT
AS7211B
This procurement specification covers split cotter pins with optional ends (see Figure 1), made from a corrosion and heat resistant steel of the type identified under the Unified Numbering System as UNS S32100.
Standard
Spring Pins, Tubular, Carbon Steel, Procurement Specification for
2024-04-01
CURRENT
AS7205A
This specification covers tubular-shaped pins, fabricated from carbon steel, having a full-length longitudinal slot to permit flexure when inserted into a hole.
Standard
Screw Threads - MJ Profile, Metric
2024-04-01
CURRENT
MA1370A
This standard specifies the characteristics of the MJ profile metric series of screw threads, altered from ISO 68 M Profile, to include a mandatory controlled radius of 0.18042P to 0.15011P at the root of the external thread and with the minor diameter of both external and internal threads increased to provide a basic thread height of 0.5625H in order to accommodate the external thread maximum root radius.
Standard
ROD END - THREADED, AIRCRAFT
2024-03-22
CURRENT
AS49011C
Standard
BOLT, MACHINE - HEXAGON HEAD, PD SHANK, CORROSION AND HEAT RESISTANT STEEL, UNS S66286, .4375-20 UNJF-3A
2024-03-12
CURRENT
AS3103B
Standard
Identification of Standard Utility Parts – Bolts and Nuts
2024-03-04
CURRENT
AIR3260A
This information report presents recommendations on part number marking which provides for the maximum identification on bolts and nuts while ensuring adequate readability.
Standard
SPACER, SLEEVE – FOR .190 INCH BOLT, AMS4901 OR AMS4921
2024-03-04
CURRENT
AS3435A
Standard
BOLT, MACHINE - HEXAGON HEAD, PD, SHANK, CORROSION AND HEAT RESISTANT STEEL, UNS S66286, .3750-24 UNFJ-3A
2024-03-04
CURRENT
AS3102B
Standard
Storage, Handling, and Shipping of Aircraft Wheel and Tire Assemblies
2024-03-01
CURRENT
ARP6951
This SAE Aerospace Recommended Practice (ARP) identifies the best practices to reduce damage and promote safety during the storage, handling, and shipping of W/T assemblies.
Standard
Stud, Locked In, Key Locked, UNS S66286, Classification: 140 ksi, Procurement Specification For
2024-02-29
WIP
AS4891A
This procurement specification covers studs made from A286 alloy of the type identified under the Unified Numbering System as UNS S66286 which have integrated locking keys to prevent rotation of the stud when installed in the prepared hole.
