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Viewing 61 to 90 of 14712
2017-06-22
Standard
AMS6512H
This specification covers a premium aircraft-quality, maraging alloy steel in the form of bars, forgings, mechanical tubing, flash welded rings up through 10.000 inches (254.00 mm) inclusive in diameter or least distance between parallel sides and stock for forging or flash welded rings.
2017-06-22
Standard
AS893E
To Stabilize AS893D - issued 1-15-76 per MIL-F-18280 for O2 and GSE only; revised 4 times (12-1-83 to add O2 cleaning requirement and part id note, 1995-12 to reformat to SAE template and revised title, 2008-03 to add cad note, change proc spec to AS4842/2 and associated QML requirements, update matl inactive/can'd specs to active ones, revised wrench flat tolerances, and inactivated 'D' matl for new design, 2009-11 to update to current SAE template along with Table updates and add 'D' inactive effectivity date; reaffirmed twice; April 1983 & 2007-08. No other significant changes to the standard.
2017-06-21
Standard
AS4665C
SCOPE IS UNAVAILABLE.
2017-06-21
Standard
AMS2249H
This specification defines limits of variation for determining acceptability of the composition of cast or wrought titanium and titanium alloy parts and material acquired from a producer.
2017-06-21
Standard
AS43021-3
No Scope available.
2017-06-21
Standard
AS43021AR-3
No Scope available.
2017-06-21
Standard
AS4664D
SCOPE IS UNAVAILABLE.
2017-06-21
WIP Standard
AS5188C
SCOPE IS UNAVAILABLE.
2017-06-21
Standard
AS5230D
SCOPE IS UNAVAILABLE.
2017-06-21
Standard
AS1004G
SCOPE IS UNAVAILABLE.
2017-06-21
Standard
AS1008J
SCOPE IS UNAVAILABLE.
2017-06-21
Standard
AS1007K
SCOPE IS UNAVAILABLE.
2017-06-20
Standard
AS5235C
SCOPE IS UNAVAILABLE.
2017-06-20
Standard
AS85848/1A
SCOPE IS UNAVAILABLE.
2017-06-19
Standard
AS7202A
This document has been declared "CANCELLED" as of June 2017 and has been superseded by PRI AC7202. By this action, this document will remain listed in the Numerical Section of the Aerospace Standards Index noting that it is superseded by PRI AC7202. Cancelled specifications are available from SAE.
2017-06-19
Standard
AS7201A
This document has been declared "CANCELLED" as of June 2017. By this action, this document will remain listed in the Numerical Section of the Aerospace Standards Index. Cancelled specifications are available from SAE.
2017-06-19
Standard
AS7115A
This document has been declared "CANCELLED" as of June 2017 and has been superseded by PRI AC7115. By this action, this document will remain listed in the Numerical Section of the Aerospace Standards Index noting that it is superseded by PRI AC7115. Cancelled specifications are available from SAE.
2017-06-19
Standard
AS7112/2A
This document has been declared "CANCELLED" as of June 2017 and has been superseded by PRI AC7112/2. By this action, this document will remain listed in the Numerical Section of the Aerospace Standards Index noting that it is superseded by PRI AC7112/2. Cancelled specifications are available from SAE.
2017-06-19
Standard
AS7112/3A
This document has been declared "CANCELLED" as of June 2017 and has been superseded by PRI AC7112/3. By this action, this document will remain listed in the Numerical Section of the Aerospace Standards Index noting that it is superseded by PRI AC7112/3. Cancelled specifications are available from SAE.
2017-06-19
Standard
AS7113A
This document has been declared "CANCELLED" as of June 2017. By this action, this document will remain listed in the Numerical Section of the Aerospace Standards Index. Cancelled specifications are available from SAE.
2017-06-19
Standard
AMS6514J
This specification covers a premium aircraft-quality steel in the form of bars, forgings, mechanical tubing, flash welded rings up through 10.000 inches (254.00 mm) inclusive in diameter or least distance between parallel sides, and stock for forging or flash welded rings.
2017-06-16
Standard
ARP584D
This SAE Aerospace Recommended Practice (ARP) addresses the design, installation, and testing of coiled tube assemblies ranging from 1/4 inch (6.3 mm) to 1.0 inch (25 mm) diameter using CRES tubing per AMS-T-6845, unless otherwise approved by the Procuring Activity. This ARP specifically details three different configurations of coiled tubing. These configurations should be compatible with pressure levels up to 3000 psi (20.7 MPa) upon the completion of the analysis for the actual stress and life requirement of the intended application. However, formal qualification tests are recommended to verify the satisfactory installation, clamping, and the life of each unique design. NOTE: Refer to ARP4146 for information on design of coiled tube assemblies using Titanium tubing.
2017-06-15
WIP Standard
AIR5919B
This SAE Aerospace Information Report (AIR) is intended to document and provide access to information obtained by an industry survey. It summarizes and documents data regarding possible alternatives to the use of cadmium plating on general connectors and connector accessories typically used in aerospace and military defense electrical interconnect systems.
Viewing 61 to 90 of 14712

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