Search
Advanced Search
of the following are true

Results

Items (208,190)
ARINC 858 Part 2 provides aviation ground system gateway considerations necessary to transition to the Internet Protocol Suite (IPS). ARINC 858 Part 2 describes the principles of operation for an IPS gateway that enables ACARS application messages to be exchanged between an IPS aircraft and a ground ACARS host. ARINC 858 Part 2 also describes the principles of operation for an IPS gateway that enables OSI-based application messages to be exchanged between an IPS host and an OSI end system. This product was developed in coordination with ICAO WG-I, RTCA SC-223, and EUROCAE WG-108
Airlines Electronic Engineering Committee
This ARP describes recommended sampling conditions, instrumentation, and procedures for the measurement of nonvolatile particle number and mass concentrations from the exhaust of aircraft gas turbine engines. Procedures are included to estimate sampling system loss performance. This ARP is not intended for in-flight testing, nor does it apply to engines operating in the afterburning mode. This ARP is intended as a guide toward standard practice and is subject to change to keep pace with experience and technical advances
E-31P Particulate Matter Committee
This specification covers a silver alloy in the form of wire, rod, sheet, strip, foil, pig, powder, shot, and chips, and a viscous mixture (paste) of powder in a suitable binder
AMS D Nonferrous Alloys Committee
This specification covers aluminum alloy die castings
AMS D Nonferrous Alloys Committee
This specification covers a nylon in the form of webbing with integral locking slots
AMS P Polymeric Materials Committee
The foundation specification (AMS3050) and this category specification (AMS3050/1) cover anti-seize greases conforming to the requirements but using the anti-seize ingredient Copper only
AMS M Aerospace Greases Committee
This document defines an open encoding format for airport databases which are loaded in airborne systems. This format, when designed and implemented, will enable a quick, economic, and efficient use of AMDB. However, since industry does not require applications to be standardized, data interpretation is not addressed in this document
Airlines Electronic Engineering Committee
The foundation specification (AMS3050) and this category specification (AMS3050/5) cover anti-seize greases conforming to the requirements but using the anti-seize ingredient PTFE only. For use only below 600 °F / 315 °C
AMS M Aerospace Greases Committee
This specification covers helical compression and extension springs, made from single wire or rod of either round or special cross-section (see 6.4
E-25 General Standards for Aerospace and Propulsion Systems
This specification covers an aluminum alloy in the form of foil
AMS D Nonferrous Alloys Committee
The intended upper bound of this specification is that the particle size distribution (PSD) of powders supplied shall be <60 mesh (250 µm) and that no powder (0.0 wt.%) greater than 40 mesh (425 µm) is allowed
AMS AM Additive Manufacturing Metals
This specification covers an aluminum alloy in the form of pre-alloyed powder
AMS AM Additive Manufacturing Metals
This specification covers requirements for the acquisition of two types and two classes of material that will remove or loosen carbon from components of internal combustion engines and compressor sections of jet engines
AMS J Aircraft Maintenance Chemicals and Materials Committee
This document defines the requirements for a PTFE lined, aramid reinforced assembly suitable for use up to 135 °C and up to 28 000 kPa aircraft and missile hydraulic and pneumatic systems
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
This procurement specification covers alloy steel and corrosion and heat resistant steel free running metric nuts of the following types, styles and classes
E-25 General Standards for Aerospace and Propulsion Systems
This specification covers one type of continuous multifilament carbon fibers in the form of a tow or yarn (when twisted). The weight per unit length of the tow or yarn is governed by the filament count which is identified by the supplier's grade or material designation
AMS P17 Polymer Matrix Composites Committee
This specification covers one type of tape and sheet for use in the installation of windshields, panels, and windows in cabins and cockpits of aircraft
AMS P Polymeric Materials Committee
This specification covers the requirements for one grade of an ultra-clean instrument grease with characteristics which permit its use from −54°C to 121°C
AMS M Aerospace Greases Committee
This specification covers a low modulus meta-aramid in the form of cloth
AMS P Polymeric Materials Committee
This specification covers a low-modulus aramid in the form of webbing
AMS P Polymeric Materials Committee
This specification covers one type of hot-melt, addition-type, polyimide adhesive in the form of supported film furnished in rolls or cut sheets
AMS P17 Polymer Matrix Composites Committee
The foundation specification (AMS3050) and this category specification (AMS3050/9) cover anti-seize greases conforming to the requirements, but using the anti-seize ingredient Graphite+Calcium Fluoride only
AMS M Aerospace Greases Committee
This specification covers one type of continuous multifilament carbon fibers in the form of a tow or yarn (when twisted). The weight per unit length of the tow or yarn is governed by the filament count which is identified by the supplier's grade or material designation
AMS P17 Polymer Matrix Composites Committee
This specification covers a heat-resistant gamma titanium aluminide alloy in the form of pre-alloyed powder
AMS AM Additive Manufacturing Metals
This specification covers nonfluorescent, magnetic particles in the form of dry powders in the form of single or composite magnetic particle intended to be suspended in oil or conditioned water vehicle for use in the wet method, magnetic particle inspection
AMS K Non Destructive Methods and Processes Committee
This specification covers a filled epoxy resin formulation, supplied as a one-component system, requiring an oven cure for attainment of its properties
AMS P Polymeric Materials Committee
This specification establishes the requirements for a high visibility, durable, exterior fluorescent coating system consisting of a pigmented fluorescent coating with a clear protective overcoat containing a weathering stabilizer. This coating system is capable of being removed without softening the permanent undercoats
AMS G8 Aerospace Organic Coatings Committee
This specification covers steel forgings suitable for use in the construction of aircraft/aerospace equipment, special ordnance, and related accessories
AMS E Carbon and Low Alloy Steels Committee
This SAE Standard defines the general requirements and provides a system for the control of quality for conformal coatings suitable for application to printed circuit assemblies
AMS G8 Aerospace Organic Coatings Committee
This specification covers the requirements for one type of tiedown fitting for installation in the floors of aircraft
AGE-2 Air Cargo
This specification covers a silicone rubber in the form of sheet, strip, tubing, extrusions, and molded shapes
AMS CE Elastomers Committee
This SAE Aerospace Standard (AS) establishes the requirements for self-aligning, self-lubricating plain spherical bearings incorporating polytetrafluoroethylene (PTFE) in a liner between the ball and the outer race for use in a temperature range of -65 to +250 °F (-54 to +121 °C
ACBG Plain Bearing Committee
This model is designed to enhance insight into the application of meaningful metrics. The emphasis is on business processes which may best provide indication of the level of risk to the customer when contemplating or continuing business with the supplier base. (E.g., the RFP/RFQ, proposal, supplier selection, and performance
Systems Management Council
This Standard is applicable to suppliers of electronic components, assemblies, equipment and related materials. This standard establishes the general requirements to achieve a certified process. The use of this standard is intended for any manufacturing or service company whose goal is to achieve customer satisfaction through continuous improvement
Systems Management Council
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Items per page:
1 – 50 of 208190