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Viewing 451 to 480 of 35602
CURRENT
2017-09-22
Standard
AS150F
This SAE Aerospace Standard (AS) establishes Type classification for those hose assemblies commonly used in aerospace fuel, lubricating oil, and hydraulic fluid systems.
2017-09-22
WIP Standard
AMS4918P
This specification covers a titanium alloy in the form of sheet, strip, and plate up through 4.000 inches (101.60 mm), inclusive.
2017-09-22
WIP Standard
AMS4967M
This specification covers a titanium alloy in the form of bars, wire, forgings, flash welded rings up through 4.000 inches (101.60 mm) in diameter or least distance between parallel sides and stock of any size for forging, heading, or flash welded rings (See 8.6).
2017-09-22
WIP Standard
AMS4919J
This specification covers a titanium alloy in the form of sheet, strip, and plate 0.025 to 3.000 inches (0.64 to 76.20 mm), inclusive, in nominal thickness.
2017-09-22
WIP Standard
AMSH81200E
This specification covers the heat treatment of titanium and titanium alloy mill products (raw material), including wrought and cast products, by material producers. This specification also covers furnace equipment requirements, test procedures, and general information for heat treating procedures, heat treating temperatures, and material test procedures for the heat treatment of titanium and titanium alloys. It also describes procedures that, when followed, have produced the desired properties within the limitations of the respective alloys.
CURRENT
2017-09-22
Standard
AMSM7866B
This specification covers the requirements for procurement of one grade of powdered molybendum disulfide to be used in lubricants and greases for surfaces where boundary conditions exist.
2017-09-22
WIP Standard
AMS4914G
This specification covers a titanium alloy in the form of sheet and strip up to and including 0.125 inches in thickness. These products have been used typically in applications requiring high strength-to-weight ratio and stability up to 550 °F (288 °C), but usage is not limited to such applications. Parts are typically formed in the solution heat treated condition and subsequently precipitation heat treated to final condition.
CURRENT
2017-09-22
Standard
AMS6327L
This specification covers an aircraft-quality, low-alloy steel in the form of bars and forgings.
CURRENT
2017-09-22
Standard
AMS2685F
This specification defines the requirements for joining metals and alloys using the gas-tungsten-arc welding (GTAW) methods.
2017-09-21
WIP Standard
AIR8012
The purpose of the document is to provide the guidelines of the technological approach for developing a PHM system for EMAs with particular reference to their possible use as primary flight control actuators. It provides a basic description of the physics of the most common degradation processes,a reliability assessment and a discussion on the signals, with the associated data processing, required to build up an effective health monitoring system.
2017-09-21
WIP Standard
SAE9990/1
This eLoran transmitted signal standard provides technical descriptions of a data channel based on the tri-state pulse position modulation technique.
2017-09-21
WIP Standard
SAE9990/2
This eLoran transmitted signal standard provides technical descriptions of the data channel using 9th pulse modulation technique.
2017-09-21
WIP Standard
AMSQQP416F
This specification covers the requirements for electrodeposited cadmium plating.
2017-09-20
WIP Standard
F17AA
These castings have been used typically for structural parts requiring strength up to 1350 °F (732 °C) and oxidation resistance up to 1800 °F (982 °C), but usage is not limited to such applications.
2017-09-20
WIP Standard
AS5148A
This SAE Aerospace Standard (AS) describes the assembly, installation and torque values for flareless and straight thread fluid fittings and tube assemblies.
2017-09-20
WIP Standard
AMS2628B
This specification covers procedures for ultrasonic immersion inspection of premium grade wrought titanium and titanium alloy round billet 5.0 inches (127 mm) and over in nominal diameter. This inspection procedure has been used typically for locating internal defects such as cracks, voids, inclusions, and other structural discontinuities which may or may not be exposed to the surface in billets, but usage is not limited to such applications. Testing normally will be by longitudinal procedure, but shear wave procedure may be added when agreed upon by purchaser and vendor. This specification includes zoned inspection and digital data acquisition.
2017-09-20
WIP Standard
AS6062A
This document defines a set of standard application layer interfaces called JAUS Mission Spooling Services. JAUS Services provide the means for software entities in an unmanned system or system of unmanned systems to communicate and coordinate their activities. The Mission Spooling Services represent the platform-independent capabilities commonly found across all domains and types of unmanned systems. At present, 1 service is defined in this document (more services are planned for future versions of this document): • Mission Spooler: Stores mission plans, coordinates mission plans, and parcels out elements of the mission plan for execution The Mission Spooler service is described by a JAUS Service Definition (JSD) which specifies the message set and protocol required for compliance. The JSD is fully compliant with the JAUS Service Interface Definition Language [JSIDL].
CURRENT
2017-09-20
Standard
AMS2510F
This specification covers the engineering requirements for finishing aircraft parts and assemblies with an engine gray enamel.
CURRENT
2017-09-20
Standard
AMS2550F
This specification covers the engineering requirements for a treatment to provide enhanced corrosion resistance to sheet metal parts, such as brackets, spacers, and washers, fabricated from martensitic Corrosion-resistant steels, usually AMS 5504 or AMS 5508 and having hardness not higher than 40 HRC, or ferritic corrosion-resistant steels, usually AMS 5506. The treatment is not recommended for use on parts subject to impact in service.
Viewing 451 to 480 of 35602