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Viewing 1 to 30 of 5223
Standard
2014-09-16
This SAE Aerospace Recommended Practice (ARP) defines a method of numbering aricraft engine cylinders.
WIP Standard
2014-09-12
This document covers the performance requirements for solid dry film lubricants, air dried, or heat cured for use in aerospace applications. These lubricants are intended to prevent galling, and may be capable of remaining effective for extended periods of time after exposure to extreme environmental conditions.
WIP Standard
2014-08-22
Scope is unavailable.
WIP Standard
2014-08-22
This standard covers all-metal, self-locking, prevailing torque nuts made of corrosion resistant steel.
WIP Standard
2014-08-22
This Aerospace Recommended Practice (ARP) establishes a method of testing, and criteria for comparative evaluation of the abrasion resistance of chafe guard, and also establishes standard test equipment to be used in conducting these tests. This ARP establishes a standard test criteria for the evaluation of chafe guards intended to afford protection from abrasion and chafing of hose assemblies and adjacent components. For test purposes, a stainless steel wire braided hose assembly, such as MIL-H-25579, shall be used. The information obtained from testing will be applicable to any hose assembly because testing ceases when the chafe guard has worn through to the test assembly.
Standard
2014-08-20
Scope is unavailable.
Standard
2014-08-20
This AIR describes the current scientific and engineering principles of gas turbine lubricant performance testing per AS5780 and identifies gaps in our understanding of the technology to help the continuous improvement of this specification.
WIP Standard
2014-08-15
Scope unavailable.
WIP Standard
2014-08-15
No Scope Available
WIP Standard
2014-08-15
No scope available.
Standard
2014-08-12
Scope is unavailable.
Standard
2014-08-12
This specification covers helical compression and extension springs, made from single wire or rod of either round or special cross-section (see 6.4).
Standard
2014-08-12
Scope is unavailable.
Standard
2014-08-12
This Aerospace Standard (AS) covers the requirements for polytetrafluoroethylene (PTFE) hose assemblies for use in aerospace hydraulic fuel, and lubricating oil systems at temperatures between -67 degrees F and 450 degrees F for Class I assemblies, -67 degrees F and 275 degrees F for Class II assemblies, and at nominal pressures up to 1500 psi. The hose assemblies are also suitable for use within the same temperature and pressure limitations in aerospace pneumatic systems where some gaseous diffusion through the wall of the PTFE liner can be tolerated. The use of these hose assemblies in pneumatic storage systems is not recommended. In addition, installations in which the limits specified herein are exceeded, or in which the application is not covered specifically by this standard, for example oxygen, shall be subject to the approval of the purchaser.
Viewing 1 to 30 of 5223

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