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Viewing 1 to 30 of 14820
CURRENT
2017-10-23
Standard
AMS3218D
This specification covers a fluorocarbon (FKM) elastomer that can be used to manufacture product in the form of sheet, strip, tubing, extrusions, and molded shapes. For molded rings, compression seals, O-ring cord, and molded-in-place gaskets for aeronautical and aerospace applications, use the AMS7259 specification.
2017-10-23
WIP Standard
J246
This SAE Standard covers complete general and dimensional specifications for tube fittings of the spherical and flanged sleeve compression types for use in the piping of air brake systems on automotive vehicles. The spherical sleeve compression type Figures 1A to 5 and Tables 1 to 3 is intended for use with annealed copper alloy tubing per SAE J1149, Type 1. The flanged sleeve compression type Figures 6A to 11 and Tables 4 to 6 is intended for use with nylon tubing per SAE J844. It is not intended to restrict or preclude other designs of a tube fitting for use with SAE J844, air brake tubing. Performance requirements for SAE J844 are covered in SAE J1131. See SAE J1131 for the Performance Requirements of Reusable (Push to Connect) Fittings Intended for Use in Automotive Air Brake Systems.
2017-10-20
WIP Standard
AIR5128B
This SAE Aerospace Information Report (AIR) is limited to the subject of aircraft fuel systems and the questions concerning the requirements for electrical bonding of the various components of the system as related to Static Electric Charges, Fault Current, Electromagnetic Interference (EMI) and Lightning Strikes (Direct and Indirect Effects). This AIR contains engineering guidelines for the design, installation, testing (measurement) and inspection of electrical bonds.
2017-10-20
WIP Standard
AS1895E
This SAE Aerospace Standard establishes the requirements for a V-retainer coupling, flanges, and seal suitable for joining high pressure and high temperature ducting in aircraft bleed air systems. The rigid coupling joint assembly, hereafter referred to as “the joint”, shall operate within the temperature range of -65 to +1200 °F.
2017-10-20
WIP Standard
AS4108C
This specification defines the requirements for A286 cres T-bolts and eye bolts, with room temperature tensile strength of a minimum of 160000 psi, for use with clamps and V-band couplings at 1000 °F maximum ambient temperature.
2017-10-19
WIP Standard
AMS3304J
This specification covers a silicone rubber in the form of sheet, strip, tubing, extrusions, and molded shapes.
2017-10-19
WIP Standard
AMS3305K
This specification covers a silicone rubber in the form of sheet, strip, tubing, extrusions, and molded shapes. Primarily for parts required to operate or seal from -65 to +205 degrees C (-85 to +401 degrees F). Silicone elastomer is resistant to deterioration by weathering and petroleum-base lubricating oil and remains flexible over the temperature range noted. These products are not normally suitable for use in contact with gasoline or aromtic fuels and low-aniline-point petroleum-base fluids due to excessive swelling of the elastomer.
2017-10-19
WIP Standard
AMS3325G
This specification covers a fluorosilicone (FVMQ) rubber in the form of sheet, strip, tubing, extrusions, and molded shapes. These products have been used typically for parts requiring resistance to jet fuel and lubricating oils, but usage is not limited to such applications. Generally, products are usable over a temperature range of -76 to +302 degrees F (-60 to +150 degrees C); each application, however, has to be considered individually.
2017-10-19
WIP Standard
AMS3741
This specification covers an 80 durometer fluorosilicone (FVMQ) rubber in the form of sheet, strip, tubing, extrusions, and molded shapes.
2017-10-19
WIP Standard
TS145AR-5
No Scope available.
CURRENT
2017-10-18
Standard
MS1002_201710
The SAE International Industrial Lubricants Committee has developed a number of industrial, non-production lubricant performance specifications. a. Define minimum performance requirements for industrial lubricants. b. Provide lubricant suppliers with performance targets for a minimum number of key industrial lubricants. c. Improve the availability of these lubricants to member companies. d. Provide a plant oriented, user friendly, classification system using common test standards and properties.
CURRENT
2017-10-18
Standard
AS4877G
This procurement specification covers bolts and screws made from a corrosion and heat resistant, age hardenable nickel base alloy of the type identified under the Unified Numbering System as UNS N07718.
CURRENT
2017-10-18
Standard
AS103C
NO SCOPE AVAILABLE.
CURRENT
2017-10-18
Standard
AMS3217/8A
This specification covers a fluorocarbon (FKM) rubber stock in the form of molded test slabs.
CURRENT
2017-10-18
Standard
AS1001J
SCOPE IS UNAVAILABLE.
2017-10-18
WIP Standard
AMS3238J
This specification covers a butyl (IIR) rubber in the form of sheet, strip, tubing, extrusions, and molded shapes.
2017-10-16
WIP Standard
ARP6448A
This document provides an industry-recommended framework for establishing agreements to ensure that seats with integrated electronic components (e.g., actuation system, reading light, inflatable restraint, IFE, etc.) meet the seat TSO Minimum Performance Standard. These agreements will allow Seat Suppliers to build and ship completed, integrated and approved seat assemblies under TSOA with electronics included. The document presents the roles, responsibilities and accontibilities of the Electronics Manufacturer, the Seat Supplier, and the Seat Installer/Electronics Activator in the context of AC 21-49 Section 7.b ‘ Type Certification using TSO-approved seat with electronic components defined in TSO design’. This document applies to all FAA seat TSOs (C39(), C127()…etc).
CURRENT
2017-10-13
Standard
AS4200B
SCOPE IS UNAVAILABLE.
2017-10-13
WIP Standard
AS7516A
SCOPE IS UNAVAILABLE.
2017-10-13
WIP Standard
AS7510A
This SAE Aerospace Standard (AS) defines the requirements for a threadless, flexible, high conductive self-bonding coupling assembly which, when installed on defined ferrules, provides a flexible connection for joining ducting and components in pressurized fluid systems. The assembled coupling is designed to provide interchangeability of parts and components between qualified manufacturers for use from -65 to +265 °F at 130 psi nominal operating pressures and for the service life of the aircraft system.
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