Search
Advanced Search
of the following are true

Results

Items (207,327)
This document provides background information, rationale, and data (both physical testing and computer simulations) used in defining the component test methods and similarity criteria described in SAE Aerospace Recommended Practice (ARP) 6330. ARP6330 defines multiple test methods used to assess the effect of seat back mounted IFE monitor changes on blunt trauma to the head and post-impact sharp edge generation. The data generated is based on seat and IFE components installed on type A-T (transport airplane) certified aircraft. While not within the scope of ARP6330, generated test data for the possible future development of surrogate target evaluation methods is also included
Aircraft Seat Committee
This SAE Aerospace Recommended Practice (ARP) provides recommendations for: The audit process in general A list of specific areas of attention to be audited Maintaining the test facility in such a manner that it meets audit requirements
EG-1E Gas Turbine Test Facilities and Equipment
No Scope available
Engine and Airframe Technical Standards Committee (TSC)
This drawing specifies parts AS55018, AS55019, AS55020, AS55021, AS55022, AS55023, AS55024, AS55025, AS55026, AS55027, AS55028, AS55029, AS55030, AS55031, AS55032, AS55034, AS55036, AS55038, AS55040, AS55042, AS55044, AS55046, AS55048, AS55050, AS55052, AS55054, AS55056, AS55058, AS55060, AS55062, AS55064, AS55066, AS55068, AS55070, AS55072, AS55074, AS55076, AS55078, AS55080, AS55082, AS55084, AS55086, AS55088, AS55090, AS55092, AS55094, and AS55096. To view suppliers qualified to manufacture this part, visit https://ts200.sae-itc.org
Engine and Airframe Technical Standards Committee (TSC)
This drawing specifies parts AS54712, AS54713, AS54714, AS54715, AS54716, AS54717, AS54718, AS54719, AS54720, AS54721, AS54722, AS54723, AS54724, AS54725, AS54726, AS54727, AS54728, AS54729, AS54730, AS54731, AS54732, AS54734, AS54736, AS54738, AS54740, AS54742, AS54744, AS54746, AS54748, AS54750, AS54752, AS54754, AS54756, AS54758, AS54760, AS54762, AS54764, AS54766, AS54768, AS54770, AS54772, AS54774, AS54776, AS54778, AS54780, AS54782, AS54784, AS54786, AS54788, AS54790, AS54792, AS54794, and AS54796. To view suppliers qualified to manufacture this part, visit https://ts200.sae-itc.org
Engine and Airframe Technical Standards Committee (TSC)
This technical specification document describes tests that certain parts may be required to meet. For example, this tech spec applies to All parts to TS147. To view suppliers qualified against this standard, visit https://ts200.sae-itc.org
Engine and Airframe Technical Standards Committee (TSC)
This specification covers filled, resinous, thermosetting compounds capable of being applied and cured in place between the surfaces of mechanically fastened (joined) structures
AMS P Polymeric Materials Committee
No scope available
Engine and Airframe Technical Standards Committee (TSC)
This specification covers a corrosion- and heat-resistant, work-strengthened, and aged cobalt-nickel-chromium alloy in the form of bars 2 inches (50 mm) and under in nominal diameter
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers an aluminum alloy in the form of plate 4.000 to 10.000 inches (101.6 to 254.0 mm), inclusive, in nominal thickness (see 8.5
AMS D Nonferrous Alloys Committee
This specification covers a corrosion- and heat-resistant cobalt alloy in the form of strip 0.100 inch (2.54 mm) and under in specified thickness and 4.000 inches (101.60 mm) and under in specified width in the solution heat-treated and cold rolled condition
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a corrosion-resistant steel in the form of bars, wire, forgings, extrusions, mechanical tubing, flash-welded rings, and stock for forging, extruding, or flash-welded rings
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock
AMS E Carbon and Low Alloy Steels Committee
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock
AMS E Carbon and Low Alloy Steels Committee
This specification covers powdered metal products consolidated by hot isostatic pressing (HIP) of titanium alloy powder compacts
AMS G Titanium and Refractory Metals Committee
This specification covers a corrosion- and heat-resistant nickel alloy in the form of welding wire
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a corrosion- and heat-resistant steel in the form of bars, wire, forgings, mechanical tubing, flash welded rings, and stock for forging or flash welded rings
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a nickel alloy in the form of wire, rod, strip, foil, and powder and a viscous mixture (paste) of the powder in a suitable binder
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a corrosion- and heat-resistant steel in the form of welded tubing
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers elemental copper in the form of powder (see 8.5
AMS D Nonferrous Alloys Committee
This specification covers an aluminum alloy in the form of die forgings not over 3 inches (76 mm) and hand forgings up to 6 inches (150 mm), inclusive, in nominal thickness at the time of heat treatment, and forging stock of any size (see 8.7
AMS D Nonferrous Alloys Committee
This specification covers a nickel alloy in the form of wire, rod, strip, foil, and powder and a viscous mixture (paste) of the powder in a suitable binder
AMS F Corrosion and Heat Resistant Alloys Committee
This specification establishes the critical controls and requirements for the production of reliable, repeatable, reproducible aerospace parts by the Stratasys Fortus 900mc Plus with Type 1, Class 1, Form 1, Grade 0, Natural Color Material for fused filament fabrication system, but is not limited to such application. This procedure will establish the configuration of the machine and build parameters, the testing methodology, and mechanical specification minimum guidelines required to create aerospace part
AMS AM Additive Manufacturing Non-Metallic
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles 5.000 inches (127.00 mm) and under in nominal diameter or thickness and 32 square inches (206 cm2) and under in cross-sectional area, and tubing 3.000 inches (76.20 mm) and under in wall thickness and 20 square inches (129 cm2) and under in cross-sectional area (see 8.5
AMS D Nonferrous Alloys Committee
This specification covers a titanium alloy in the form of pre-alloyed powder
AMS AM Additive Manufacturing Metals
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock
AMS E Carbon and Low Alloy Steels Committee
This specification covers a corrosion- and heat-resistant nickel alloy in the form of welding wire
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a corrosion and heat-resistant steel in the form of thin-wall seamless tubing
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers an aluminum alloy in the form of two types of welding wire
AMS D Nonferrous Alloys Committee
This specification covers an aluminum alloy in the form of sheet and plate from 0.006 to 6.000 inches (0.15 to 152.40 mm), inclusive, in nominal thickness (see 8.6
AMS D Nonferrous Alloys Committee
This specification covers flash welded rings made of titanium and titanium alloys
AMS G Titanium and Refractory Metals Committee
This specification covers a copper-beryllium alloy in the form of mechanical tubing 2 inches (50.8 mm) and under in wall thickness (see 8.8
AMS D Nonferrous Alloys Committee
This specification covers a titanium alloy in the form of wire for welding filler metal
AMS G Titanium and Refractory Metals 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 8.8
AMS G Titanium and Refractory Metals Committee
This specification covers a fluorosilicone (FVMQ) rubber in the form of sheet, strip, tubing, extrusions, and molded shapes. This specification is not to be used for the manufacture of O-rings, molded O-ring cord, or molded in place seals or gaskets for aerospace applications
AMS CE Elastomers Committee
This specification covers a titanium alloy in the form of prealloyed powder
AMS G Titanium and Refractory Metals Committee
This specification covers a titanium alloy in the form of prealloyed powder
AMS G Titanium and Refractory Metals 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 diameter, or least distance between parallel sides and stock of any size for forging or flash welded rings (see 8.8
AMS G Titanium and Refractory Metals Committee
This specification covers a titanium alloy in the form of sheet 0.020 to 0.1874 inch (0.51 to 4.760 mm), inclusive, in nominal thickness. (see 8.7
AMS G Titanium and Refractory Metals Committee
This specification is to prescribe process requirements for production (from raw materials through preparation for shipment, see 8.6) of metal powder feedstock for use in additive manufacturing of aerospace parts. This specification covers requirements for the production of metal powder for use as feedstock in additive manufacturing. Such powders may be pre-alloyed or commercially pure. This specification is not limited to a specific powder production method. It is intended to define those procedures and requirements necessary to achieve required cleanliness and performance of metal powder feedstock to be used in the manufacture of aerospace parts. This specification is intended to be used in conjunction with AMS powder specifications for additive manufacturing
AMS AM Additive Manufacturing Metals
This specification covers a corrosion and heat-resistant nickel alloy in the form of parts produced by laser-powder bed fusion (L-PBF) that are subjected to post-deposition stress relief (SR), hot isostatic press (HIP) and solution anneal operations. Parts may require subsequent machining or surface finishing to meet specific application requirements
AMS AM Additive Manufacturing Metals
This specification covers an aluminum alloy in the form of rolled or forged rings up to 8.000 inches (203 mm), inclusive (see 8.6
AMS D Nonferrous Alloys Committee
This specification covers polythioether rubber fuel resistant sealing compounds, supplied as a two-component system, which cure rapidly when exposed to a cure on demand (CoD) light source used to initiate a reaction that generates crosslinking of sealant polymers. Type 2 compounds also cure at ambient conditions, without light exposure
AMS G9 Aerospace Sealing Committee
This specification covers a corrosion-resistant steel in the form of bars, wire, forgings 10 inches (254 mm) and under in nominal diameter or maximum cross-sectional dimension, and forging stock
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers the requirements for removers used on amine-cured epoxy coating systems (see 6.1
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification establishes requirements for a temporary protective coating (TPC) intended to protect aluminum surfaces from damage and corrosion. This specification also establishes requirements for an alkaline remover used to strip the specified TPCs
AMS G8 Aerospace Organic Coatings Committee
This specification covers a corrosion- and heat-resistant steel in the form of seamless tubing
AMS F Corrosion and Heat Resistant Alloys Committee
Items per page:
1 – 50 of 207327