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Viewing 91 to 120 of 37693
2014-10-09
WIP Standard
AIR4243A
This document discusses the work done by the U.S. Army Corps of Engineers and the Waterways Experiment Station (WES) in support of SAE A-5 Committee activity on Aerospace Landing Gear Systems. It is an example of how seemingly unrelated disciplines can be combined effectively for the eventual benefit of the overall aircraft systems, where that system includes the total airfield environment in which the aircraft must operate. In summary, this AIR documents the history of aircraft flotation analysis as it involves WES and the SAE.
2014-10-09
Standard
J1609_201410
This SAE Recommended Practice establishes performance guidelines of the air reservoir systems used on trucks, towing trucks, truck-tractors, trailers, and converter dollies, with GVWRs over 10 000 lb, designed to be used on the highway. NOTE: Compliance with this document does not guarantee compliance with the air reservoir requirements of FMVSS 121.
2014-10-09
Standard
ARP4925B
This SAE Aerospace Recommended Practice (ARP) establishes the factors which should be considered in the design and installation of a commercial transport rotorcraft hydraulic system, including the applicable airworthiness regulations that affect the hydraulic system. This ARP also provides information and guidelines on the many factors that arise in the design process to provide cost effectiveness, reliability, maintainability and accepted design and installation practices.
2014-10-09
WIP Standard
J1698/3
This SAE Recommended Practice defines procedures that may be used to validate that relevant EDR output records conform with the reporting requirements specified in Part 563, Table 1 during the course of FMVSS-208, FMVSS-214 and other applicable vehicle level crash testing.
2014-10-09
Standard
ARP4103A
This document recommends design and performance criteria for aircraft lighting systems used to illuminate flight deck controls, luminous visual displays used for transfer of information, and flight deck background and instrument surfaces that form the flight deck visual environment. This document is for commercial transport aircraft except for applications requiring night vision compatibility.
2014-10-08
WIP Standard
ARP6336
This SAE Aerospace Recommended Practice (ARP) provides technical recommendations for the application, design and development of lighting for Unmanned Aircraft (UA). The recommendations set forth in this document are to aid in the design of UA lighting for the type or size of aircraft and the operation in the National Aerospace System for which the aircraft is intended.
2014-10-08
WIP Standard
AMS5629/H1000
This specification covers a corrosion-resistant steel in the form of bars, wire, forgings, flash welded rings, and extrusions in the solution and precipitation heat treated (H1000) condition. These products have been used typically for parts requiring corrosion resistance, stress-corrosion resistance, high strength up to 600 °F (316 °C), and good ductility and strength in the transverse direction in large section sizes, but usage is not limited to such applications.
2014-10-08
WIP Standard
AMS2231K
This specification covers established inch/pound manufacturing tolerances applicable to carbon steel bars ordered to inch/pound dimensions. These tolerances apply to all conditions, unless otherwise noted. The term "excl " is used to apply only to the higher figure of the specified range.
2014-10-08
WIP Standard
AMS2453A
Specification defines the equipment, method, and requirements for the grinding of hard chrome plate when applied to high strength steels in aerospace applications.
2014-10-08
WIP Standard
AMS5035C
This specification covers a loy-alloy steel in the form of welding wire.
2014-10-08
WIP Standard
AMS5034B
This specification covers a low-alloy steel in the form of welding wire.
2014-10-08
WIP Standard
AMS5010L
This specification covers a free-machining carbon steel in the form of bars.
2014-10-08
WIP Standard
AMS5040N
This specification covers a carbon steel in the form of sheet and strip.
2014-10-08
WIP Standard
AMS6374D
This specification covers an aircraft-quality, low-alloy steel in the form of round, non-welded tubing free from OD surface seams.

This product has been used typically for use in airframe tubular parts requiring a minimum tensile strength of 95.0 ksi (655 MPa) as received, or up to 180.0 ksi (1241 MPa) after heat treatment, but usage is not limited to such applications.

2014-10-08
WIP Standard
AMS6373H
This specification covers an aircraft-quality, low-alloy steel in the form of welded tubing.
2014-10-08
WIP Standard
AMS6282K
This specification covers an aircraft-quality, low-alloy steel in the form of mechanical tubing.
2014-10-08
WIP Standard
AMS6281K
This specification covers an aircraft-quality, low-alloy steel in the form of mechanical tubing.
2014-10-08
WIP Standard
GAD14AB
This is a General Agreement for Committee D, and if adopted it will rescind the actions implemented by GA D12AA.
2014-10-08
WIP Standard
AMS6460G
This specification covers a low-alloy steel in the form of welding wire. Primarily for use as filler metal for gas-tungsten-arc and gas-metal-arc welding of low-alloy steels requiring a joint capable of being heat treated to strength levels consistent with the metals joined. Alloy: NAX-9115-AC UNS Number: K11365
2014-10-08
WIP Standard
AMS6375D
This specification covers a low-alloy steel in the form of welding wire.
2014-10-08
WIP Standard
AS1260A
Primarily to provide the aerospace industry with approximate standards for comparing various shaped sections to round bars, in determining the response to hardening characteristics when heat treating low-alloy and marensitic corrosion-resistant steels.
2014-10-08
Standard
ARP5454B
This SAE Aerospace Recommended Practice (ARP) describes the multi-pass method for evaluating the filtration performance of fine lube filter elements, commonly utilized in aerospace power and propulsion lubrication systems: gas turbine engines, auxiliary power units (APUs), helicopter transmissions, constant speed drives (CSDs), and integrated drive generators (IDGs).
2014-10-08
Standard
AIR6226
Most of the Trimmable Horizontal Stabilizer Actuators (THSA) feature a dual structural load path, the primary load path being loaded, the secondary load path being normally unloaded, or both load paths sharing in parallel the Horizontal Stabilizer load. This document describes existing methods for detecting rupture or disconnection of loaded load paths as an overview for those specifying or designing Horizontal Stabilizer Trim Actuators in order to compare existing solutions as reference for implementation in new aircraft programs.
2014-10-08
Standard
ARP6200
This SAE Aerospace Recommended Practice (ARP) describes the recommended tests and their associated test means for commercial aircraft hydraulic systems at the system level that are required to demonstrate compliance with the 14 CFR Part 25 and EASA CS 25 airworthiness regulations, and to show that the required level of maturity at the aircraft entry into service (EIS) has been achieved.
Viewing 91 to 120 of 37693