Search
Advanced Search
of the following are true
(
)

Results

Items (215,951)
This AIR provides information about the specific requirements for missile hydraulic pumps and their associated power sources.
A-6C4 Power Sources Committee
E-25 General Standards for Aerospace and Propulsion Systems
E-25 General Standards for Aerospace and Propulsion Systems
The purpose of this Standard is to provide installation dimensions for shaft nuts and their companion keywasher. The Standard type typically shown on MS9951 and MS9952, but is also suitable for parts which are dimensionally equivalent.
E-25 General Standards for Aerospace and Propulsion Systems
E-25 General Standards for Aerospace and Propulsion Systems
E-25 General Standards for Aerospace and Propulsion Systems
E-25 General Standards for Aerospace and Propulsion Systems
E-25 General Standards for Aerospace and Propulsion Systems
E-25 General Standards for Aerospace and Propulsion Systems
E-25 General Standards for Aerospace and Propulsion Systems
This specification covers a titanium alloy in the form of bars 6.000 inches (152.40 mm) and under in nominal diameter or least distance between parallel sides, forgings, flash-welded rings 6.000 inches (152.40 mm) and under in thickness, and stock for forging and stock for flash-welded rings of any size (see 8.6).
AMS G Titanium and Refractory Metals Committee
SAE J1939-75 defines the set of data parameters (SPs) and messages (PGs) for information predominantly associated with monitoring and control generators and driven equipment in electric power generation and industrial applications. The data parameters (SPs) and messages (PGs) previously published within this document are published in SAE J1939DA. Applications using the SAE J1939-75 document must refer to SAE J1939DA for the SAE J1939 parameters and messages for monitoring and controlling the power units, e.g., engines and turbines, that power the generators and driven industrial equipment.
Truck and Bus Control and Communications Network Committee
This specification covers a titanium alloy in the form of bars, wire, forgings, flash-welded rings 4.000 inches (101.60 mm) and under in nominal diameter or least distance between parallel sides, and stock of any size for forging or flash-welded rings (see 8.6).
AMS G Titanium and Refractory Metals Committee
This SAE Information Report establishes the Use Cases for communications and customer-focused Key Performance Indicators (KPI) between plug-in electric vehicles (PEVs) and their customers. The Use Case Scenarios define the information to be communicated related to customer convenience features for charge on/off control, charge power curtailment, customer preference settings, charging status, electric vehicle supply equipment (EVSE) availability/access, and electricity usage, plus customer information resulting from conflicts to charging preferences. It also addresses the KPI that can provide a uniform set of metrics to quantitively assess the charging experience. This document only provides the Use Cases that define the communications requirements to enable customers to interact with the PEV and the KPI to optimize their experience with charging a PEV. Specifications such as protocols and physical transfer methods for communicating information are not within the scope of this document.
Hybrid - EV Committee
This specification covers an aluminum alloy in the form of sand, permanent mold, and composite mold castings with nominal wall thicknesses of up to 1.0 inch (25.4 mm), inclusive (see 8.8).
AMS D Nonferrous Alloys Committee
This specification covers an aluminum alloy in the form of sand, permanent mold, composite mold, and investment castings (see 8.6).
AMS D Nonferrous Alloys Committee
This specification covers a corrosion- and heat-resistant nickel alloy in the form of seamless tubing 0.125 inch (3.18 mm) and over in nominal OD with nominal wall thickness 0.015 inch (0.38 mm) and over.
AMS F Corrosion and Heat Resistant Alloys Committee
AMS D Nonferrous Alloys Committee
This specification establishes the requirements for cleaning compounds, used in parts washers and spray cabinets for cleaning aircraft components.
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers a hydrocarbon fluid mixture for use as a reference fuel test fluid to evaluate the ability of polymeric compounds to conform to designated requirements after immersion in the fluid at a specific temperature for a specified time, as required by an applicable specification.
AMS CE Elastomers Committee
This specification covers a two-component air-curing, aluminum-powder-filled, epoxy-resin-base material in the form of a paste or putty, suitable for application by spatula or putty-knife.
AMS G9 Aerospace Sealing Committee
This specification covers a pneumatic system grease. This grease is identified by NATO Code Number G 392 (see 6.5).
AMS M Aerospace Greases Committee
AMS D Nonferrous Alloys Committee
This specification covers an extreme-low-temperature-resistant silicone rubber in the form of sheet, strip, tubing, extrustions, and molded shapes.
AMS CE Elastomers Committee
This specification covers tungsten carbide-cobalt in the form of powder.
AMS B Finishes Processes and Fluids Committee
This specification and its supplementary detail specifications cover polyether-type urethane (EU) resins and hardeners which, when mixed and cured, produce elastomeric polyurethane products.
AMS P Polymeric Materials Committee
This specification covers a colored but unpigmented varnish based on a phenolic resin.
AMS G8 Aerospace Organic Coatings Committee
This specification covers a woven nylon cloth coated with polyether (EU) urethane.
AMS P Polymeric Materials Committee
This specification covers two types of fire extinguishing foam concentrate in the form of a liquid.
AMS J Aircraft Maintenance Chemicals and Materials Committee
Items per page:
1 – 50 of 215951