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Viewing 31 to 60 of 8772
CURRENT
2017-06-16
Standard
CPYM1_17MX825V
This product includes information on the manufacturer, engine, application, testing location, certified maximum horsepower, certified maximum torque along with the certified curves of horsepower and torque over a wide range of engine RPM speeds.
CURRENT
2017-06-16
Standard
CPYM1_17MX800V
This product includes information on the manufacturer, engine, application, testing location, certified maximum horsepower, certified maximum torque along with the certified curves of horsepower and torque over a wide range of engine RPM speeds.
2017-06-15
WIP Standard
AS6034
Create an AS standard for a high temperature loop type support clamp in 625 nickel alloy in sizes shown on AS9025 and oversized for use with .028" wearsleeves.
CURRENT
2017-06-14
Standard
AS18280F
This SAE Aerospace Standard (AS) establishes the requirements for 24° cone flareless fluid connection fittings and nuts, internally or externally swaged, preset, or welded sleeves for use in aircraft fluid systems at nominal operating pressures up to and including 3000 psi.
CURRENT
2017-06-08
Standard
AS7112/1A
This document has been declared "CANCELLED" as of June 2017 and has been superseded by PRI AC7112/1. By this action, this document will remain listed in the Numerical Section of the Aerospace Standards Index noting that it is superseded by PRI AC7112/1. Cancelled specifications are available from SAE.
CURRENT
2017-06-08
Standard
AS7112A
This document has been declared "CANCELLED" as of June 2017 and has been superseded by PRI AC7112. By this action, this document will remain listed in the Numerical Section of the Aerospace Standards Index noting that it is superseded by PRI AC7112. Cancelled specifications are available from SAE.
2017-06-08
WIP Standard
AS598A
This SAE Aerospace Standard (AS) defines the materials, apparatus and procedure for microscopic sizing and counting of particulate contamination of fluid power systems by membrane filtration using microscopic counting.
2017-06-08
WIP Standard
AS5463C
SCOPE IS UNAVAILABLE.
2017-06-08
WIP Standard
AS5460C
SCOPE IS UNAVAILABLE.
2017-06-08
WIP Standard
AS5462C
SCOPE IS UNAVAILABLE.
2017-06-08
WIP Standard
AS5461C
SCOPE IS UNAVAILABLE.
2017-06-08
WIP Standard
AS5459C
SCOPE IS UNAVAILABLE.
2017-06-08
WIP Standard
AS5458C
SCOPE IS UNAVAILABLE.
CURRENT
2017-06-05
Standard
AS14227D
SCOPE IS UNAVAILABLE.
CURRENT
2017-06-05
Standard
J1536_201706
This SAE Recommended Practice is intended for use by engine manufacturers in determining the Fluidity/Miscibility Grades to be recommended for use in their engines, and by oil marketers in formulating and labeling their products.
CURRENT
2017-06-05
Standard
AS5620B
This SAE Aerospace Standard (AS) shall be used in conjunction with AMS 4946 to provide requirements for qualification testing and for Qualified Products Listing (QPL) and Qualified Manufacturer Listing (QML) for Ti-3Al-2.5V cold worked and stress relieved hydraulic system tubing. The basic tubing shall comply with the requirements of AMS 4946.
2017-06-01
WIP Standard
AIR4250C
This report lists documents that aid and govern the design, development, and utilization of aerospace electronic engine control systems. The report lists the military and industry specifications and standards that are commonly used in electronic engine control system design. However, this list is not necessarily complete. The specifications and standards section has been divided into two parts; a master list arranged numerically and a categorized list that provides a functional breakdown and cross reference of these documents. For specifications and standards, the issue available during the latest revision to this document is listed. Details of current revisions for many documents are available in the Department of Defense Index of Specifications and Standards (DODISS).
CURRENT
2017-06-01
Standard
AMS1548B
This specification covers a solvent-emulsion cleaner in the form of a solvent-base liquid concentrate.
2017-06-01
WIP Standard
AS1424H
This SAE Aerospace Standard (AS) covers medium-pressure, high-temperature, flexible, metal-hose assemblies suitable for operation in pneumatic systems up to 800 °F with excursion to 1200 °F for Class “B” and “N” and primarily for use on jet aircraft power plants. Refer to 1.2.1 for recommended usage. 1.1 Types a. Type 1: Convoluted helical inner tube, seamless or welded and redrawn tube material. b. Type 2: Convoluted annular inner tube, seamless or welded and redrawn tube material. c. Type 3: Convoluted helical inner tube, as-welded tube material. d. Type 4: Convoluted annular inner tube, as-welded tube material. NOTE: Unless otherwise specified on a design activity controlled drawing, or contract, Type 1, Type 2, Type 3, or Type 4 inner tube construction may be supplied. 1.2 Classes Hose assemblies furnished under this document may be of the following classes. If no class is defined the class “S” shall be utilized. a.
CURRENT
2017-06-01
Standard
J1390_201706
Three levels of fan structural analysis are included in this practice: a. Initial Structural Integrity b. In-vehicle Testing c. Durability (Laboratory) Test Methods The Initial Structural Integrity section describes analytical and test methods used to predict potential resonance and, therefore, possible fatigue accumulation. The In-vehicle (or machine) section enumerates the general procedure used to conduct a fan strain gage test. Various considerations that may affect the outcome of strain gage data have been described for the user of this procedure to adapt/discard depending on the particular application. The Durability Test Methods section describes the detailed test procedures for a laboratory environment that may be used depending on type of fan, equipment availability, and end objective. The second and third levels build upon information derived from the previous level.
2017-05-31
WIP Standard
ARP594F
The requirements presented in this document cover the design factors which might cause any part of an electrically motor driven fuel pump assembly to act as an ignition source for explosive fuel vapors within the airplane tank.
2017-05-31
WIP Standard
ARP5794A
This specification covers the general requirements for aircraft tank mounted, centrifugal type, fuel booster pumps, used for engine fuel feed and/or fuel transfer.
2017-05-31
WIP Standard
MS1005
ISO 7745 shall be used for providing detailing, operational characteristics, advantages, disadvantages, and factors affecting the choice to be made among fire-resistant fluids.
CURRENT
2017-05-30
Standard
J512_201705
This SAE Standard covers complete general and dimensional specifications for the various types of tube fittings intended for general application in the automotive, appliance, and allied fields. See SAE J1131 for the performance requirements of reusable (push to connect) fittings intended for use in automotive air brake systems.
Viewing 31 to 60 of 8772

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