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Viewing 91 to 120 of 14712
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.
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.
2017-06-13
Standard
AMS5707N
This specification covers a corrosion and heat-resistant nickel alloy in the form of bars, forgings, flash welded rings, 3.25 inches (82.6 mm) and under and stock of any size for forging and for flash welded rings. (see 8.5).
2017-06-12
WIP Standard
AS6171A

This SAE Aerospace Standard (AS) standardizes inspection and test procedures, workmanship criteria, and minimum training and certification requirements to detect Suspect/Counterfeit (SC) Electrical, Electronic, and Electromechanical (EEE) parts. The requirements of this document apply once a decision is made to use parts with unknown chain of custody that do not have pedigree back to the original component manufacturer, or have been acquired from a broker or independent distributor, or when there are other known risk elements that result in the User/Requester to have concerns about potential SC EEE parts. The tests specified by this standard may also detect occurrences of malicious tampering, although the current version of this standard is not designed specifically for this purpose.

2017-06-09
Standard
ARP4912C
This SAE Aerospace Recommended Practice (ARP) provides recommendations on cavity design, the installation of elastomer type spare seals in these cavities, and information surrounding elastomer material properties after contact with typical shock absorber hydraulic fluid(s) or grease. This ARP is primarily concerned with the use of spare seals on shock absorbers where only a single dynamic seal is fitted and in contact with the slider/shock absorber piston at any one time. These shock absorbers typically have a spare (dynamic) seal gland located on the outer diameter of the lower seal carrier. This spare seal gland is intended to house a spare elastomer contact seal. Split Polytetrafluoroethylene (PTFE) backup rings can also be installed in the spare seal cavity. During operation, if the fitted dynamic shock absorber standard seal begins to fail/leak, then the aircraft can be jacked up, allowing the lower gland nut of the shock absorber to be dropped down.
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
Standard
AS7109/6B
This document has been declared "CANCELLED" as of June 2017 and has been superseded by PRI AC7109/6. By this action, this document will remain listed in the Numerical Section of the Aerospace Standards Index noting that it is superseded by PRI AC7109/6. Cancelled specifications are available from SAE.
2017-06-08
WIP Standard
AS5461C
SCOPE IS UNAVAILABLE.
2017-06-08
WIP Standard
AS5460C
SCOPE IS UNAVAILABLE.
2017-06-08
WIP Standard
AS5463C
SCOPE IS UNAVAILABLE.
2017-06-08
WIP Standard
AS5462C
SCOPE IS UNAVAILABLE.
2017-06-08
WIP Standard
AS5459C
SCOPE IS UNAVAILABLE.
2017-06-08
WIP Standard
AS5458C
SCOPE IS UNAVAILABLE.
2017-06-07
Standard
J2494/2_201706
This SAE Standard covers general dimensional specifications for non-metallic body reusable push to connect tube fittings for use in the piping of air brake systems on automotive vehicles. This type of fitting is intended for use with nylon tubing per SAE J844. It is not intended to restrict or preclude other designs of a tube fitting for use with SAE J844. Performance requirements for SAE J844 are covered in SAE J1131. See SAE J2494-3 for the performance requirements of Reusable (push-to-connect) fittings intended for use in Automotive Air Brake Systems and U.S. Department of Transportation FMVSS 571.106.
2017-06-07
Standard
AS81659B
This specification covers two series of electrical, rectangular connectors with crimp type removable contacts. These connectors are provided with single, dual, triple, and quadruple insert shell configurations.
2017-06-07
Standard
J820_201706
This document applies primarily to mobile cranes that lift loads by means of a drum and hoist line mechanism. It can be used to determine the hoist line speed and power of other hoist line mechanisms, if the load can be held constant and hoist line travel distance is sufficient for the accuracy of the line speed measurements prescribed. This recommended practice applies to all mechanical, hydraulic, and electric powered hoist mechanisms.
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.
2017-06-05
Standard
AMS7445E
This specification covers balls made of high-carbon corrosion-resistant steel of three carbon ranges.

These products have been used typically for bearing balls, but usage is not limited to such applications.

2017-06-05
Standard
AS14227D
SCOPE IS UNAVAILABLE.
2017-06-04
WIP Standard
AS5242C
Scope is unavailable.
2017-06-02
WIP Standard
AS85421/10D
SCOPE IS UNAVAILABLE.
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.
2017-06-01
Standard
AS20218B
SCOPE IS UNAVAILABLE.
2017-06-01
Standard
AS81714/5A
SCOPE IS UNAVAILABLE.
2017-06-01
Standard
AS1005H
SCOPE IS UNAVAILABLE.
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
AS81306A
This specification covers tools used to install tiedown straps on wire bundles and for installing connector accessory shield termination bands.
Viewing 91 to 120 of 14712

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