Criteria

Text:
Content:
Display:

Results

Viewing 91 to 120 of 44393
CURRENT
2017-07-07
Standard
AS85848/2A
SCOPE IS UNAVAILABLE.
CURRENT
2017-07-07
Standard
ARP5483B
This SAE Aerospace Recommended Practice (ARP) establishes methods for testing airframe rolling element bearings. The purpose of ARP5483 and its associated slash sheets is to document test methods commonly used to evaluate airframe bearings. These test methods may be referenced in standards, purchase orders, etc. when the test is deemed appropriate to the intended use of the bearing by the end user of the bearing. These test methods are not intended to encompass every conceivable requirement for an airframe bearing. The end user of the bearing must exercise engineering judgment to determine the most appropriate standard and/or nonstandard tests for the application.
CURRENT
2017-07-07
Standard
AS21905D
Scope unavailable.
CURRENT
2017-07-07
Standard
AS21910E
Scope unavailable.
CURRENT
2017-07-07
Standard
AMS4031J
This specification covers an aluminum alloy in the form of sheet and plate 0.020 to 2.000 inches (0.51 to 50.80 mm), inclusive, in nominal thickness, supplied in the annealed (O) condition (see 8.4). When specified, product shall be supplied in the “as fabricated” (F) temper.
2017-07-06
WIP Standard
SAE1001
The purpose of the "Integrated Project Processes for Engineering a System(IPPES)" Standard is to provide an integrated set of fundamental technical processes to aid a project in the engineering or reengineering of a system over the full life cycle. Covers systems that can be any combination of people (humans); product (hardware or software); or process (service). Applicable to any type of system: commercial or non-commercial; small or large, simple or complex, precedented or unprecedented; new or legacy or any combination of these characteristics.
CURRENT
2017-07-06
Standard
AS85848A
This specification establishes the requirements for various types of identification sleeving that will shrink to a predetermined size upon the application of heat after it has been marked. Continuous operating temperature ratings range from -55° to 175°C (-67° to 347°F). (See 6.1).
CURRENT
2017-07-06
Standard
AIR6297
This document describes a method to calculate noise level adjustments at locations behind an airplane (described by an angular offset or directivity) at the start of takeoff roll (SOTR). This method is derived from empirical data from jet aircraft (circa 2004), most of which are configured with wing-mounted engines with high by-pass ratios (Lau, et al., 2012). Methods are also described which apply to modern turboprop aricraft.
2017-07-06
WIP Standard
AMS7464D
This specification covers premium quality bolts and screws made from a low-alloy, heat-resistant steel and having threads of UNJ (MIL-S-8879) form.
CURRENT
2017-07-06
Standard
AS21911D
SCOPE IS UNAVAILABLE.
2017-07-06
WIP Standard
AMS2376E
This specification covers procedures for approval of premium quality forgings, usually serialized, the stock from which such forgings are produced, and the controls to be exercised in producing the forgings and forging stock.
2017-07-05
WIP Standard
AS85049/151
This AS85049 product will accommodate the user demand for a metal version of the AS85049/103 style accessory.
2017-07-05
WIP Standard
AS85049/152
This AS85049 product will accommodate the user demand for a metal version of the AS85049/104 style accessory.
2017-07-05
WIP Standard
AS85049/153
This AS85049 product will accommodate the user demand for a metal version of the AS85049/105 style accessory.
CURRENT
2017-07-05
Standard
AS4688C
(A) Propose to replace .5625-16 UNJF with .5625-18 UNJF on Table 3 and other editorial changes (ex. replace ARP4296 with AS4296). (B) Propose revision to add conductive high purity aluminum coating per MIL-DTL-83488 for aluminum alloy fittings. The W code aluminum parts with new finish will be distinguished by new finish code V at the end of part number.
CURRENT
2017-07-05
Standard
AS7220A
This procurement specification covers rivets fabricated from an aluminum alloy designated as 1100 H14, strain hardened.
2017-07-05
WIP Standard
J3146
This document has been issued to provide a reference or overview of some current practices which could be utilized for securing the vehicle’s interface with the Data Link Connector (DLC) from cybersecurity risks associated with external test equipment connections (e.g. diagnostics scan tools) or remotely connected applications (e.g. telematics devices). The practices outlined in this report are examples of some secured in-vehicle data access methods which might be used in the automotive industry. Note that In-vehicle network protocol descriptions and data format details are not included in this report.
2017-07-04
WIP Standard
AMS5122K
This specification covers a carbon steel in the form of strip.

This material hs been used typically for washers and other stamped parts requiring a smooth finish and only slight or no forming, but usage is not limited to such applications.

2017-07-04
WIP Standard
AMS7301J
This specification has been declared “NONCURRENT” by the Aerospace Materials Division, SAE, as of August 2009. It is recommended, therefore, that this specification not be specified for new designs. “NONCURRENT” refers to those specifications which have previously been widely used and which may be required for production or processing of existing designs in the future. The Aerospace Materials Division, however, does not recommend these specifications for future use in new designs. “NONCURRENT” specifications are available from SAE upon request.
2017-07-04
WIP Standard
AMS5328E
This specification covers a low alloy steel in the form of investment castings.
2017-07-04
WIP Standard
AMS5315E
This specification covers a ductile (nodular) iron in the form of sand castings.
2017-07-04
WIP Standard
AMS5316E
This specification covers a ductile (nodular) iron in the form of sand castings.
2017-07-04
WIP Standard
AMS7311H
This specification covers a centrifugally-cast, alloyed iron in the form of sleeves for the fabrication of piston rings. Primarily for use as top compression rings in aircraft piston engines. Rings usually require chromium plating for compatibility with the cylinder barrel material.
2017-07-04
WIP Standard
AMS5115J
This specification covers a carbon steel in the form of wire supplied as coils of wire or as finished springs. Primarily for springs, such as valve springs, subject to moderate stresses and requiring good fatigue properties.
2017-07-03
WIP Standard
AMS5061H
This specification has been declared "NONCURRENT "by the Aerospace Materials Division, SAE, as of February 2009. It is recommended, therefore, that this specification not be specified for new designs.
2017-07-03
WIP Standard
AMS5042N
This specification has been declared “NONCURRENT” by the Aerospace Materials Division, SAE, as of August 2009. It is recommended, therefore, that this specification not be specified for new designs. “NONCURRENT” refers to those specifications which have previously been widely used and which may be required for production or processing of existing designs in the future. The Aerospace Materials Division, however, does not recommend these specifications for future use in new designs. “NONCURRENT” specifications are available from SAE upon request.
2017-07-03
WIP Standard
AMS5031G
This specification covers a low-carbon steel in the form of covered welding electrodes.
2017-07-03
WIP Standard
AMS5030K
This specification covers a low-carbon steel in the form of welding wire.
2017-07-03
WIP Standard
AMS5062J
This specification has been declared “NONCURRENT” by the Aerospace Materials Division, SAE, as of August 2009. It is recommended, therefore, that this specification not be specified for new designs. “NONCURRENT” refers to those specifications which have previously been widely used and which may be required for production or processing of existing designs in the future. The Aerospace Materials Division, however, does not recommend these specifications for future use in new designs. “NONCURRENT” specifications are available from SAE upon request.
Viewing 91 to 120 of 44393