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Viewing 121 to 150 of 20352
CURRENT
2017-06-20
Standard
AS85848/1A
SCOPE IS UNAVAILABLE.
CURRENT
2017-06-20
Standard
AMS4315A
This specification covers an aluminum alloy in the form of sheet and plate up to 2.000 inch (54.80 mm) inclusive, in thickness (see 8.5).
CURRENT
2017-06-19
Standard
AS7200/1B
This document has been declared "CANCELLED" as of June 2017 and has been superseded by PRI AC7200/1. By this action, this document will remain listed in the Numerical Section of the Aerospace Standards Index noting that it is superseded by PRI AC7200/1. Cancelled specifications are available from SAE.
CURRENT
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This document has been declared "CANCELLED" as of June 2017 and has been superseded by PRI AC7115.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action, this document will remain listed in the Numerical Section of the Aerospace Standards Index noting that it is superseded by PRI AC7115.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.
CURRENT
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This document has been declared "CANCELLED" as of June 2017 and has been superseded by PRI AC7112/3.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action, this document will remain listed in the Numerical Section of the Aerospace Standards Index noting that it is superseded by PRI AC7112/3.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.
CURRENT
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.
2017-06-19
WIP Standard
J1992
This SAE Recommended Practice provides minimum performance requirements and uniform laboratory procedures for fatigue testing of disc wheels, demountable rims, and bolt-together divided wheels intended for normal highway use on military trucks, buses, truck-trailers, and multipurpose vehicles. For wheels and rims intended for normal highway use on trucks and buses, see SAE J267. For wheels intended for normal highway use on passenger cars, light trucks, and multipurpose vehicles, see SAE J328. For wheels used on trailers drawn by passenger cars, light trucks, or multipurpose vehicles, see SAE J1204. This document does not cover off-highway or other special application wheels and rims.
CURRENT
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.
CURRENT
2017-06-16
Standard
AMS4200C
This specification covers an aluminum alloy in the form of plate.
CURRENT
2017-06-16
Standard
AMS4300D
This specification covers boron filaments and 6061-0 aluminum alloy foil laminated and bonded into a composite sheet.
CURRENT
2017-06-16
Standard
J1525_201706
This SAE Recommended Practice describes a lap shear test method for use in measuring the bonding characteristics of automotive-type adhesives for joining fiber reinforced plastics (FRPs) to themselves and to metals.
CURRENT
2017-06-16
Standard
AMS2380G
This specification covers the procedures for approval of products of premium-quality titanium alloys and the controls to be exercised in producing such products.
CURRENT
2017-06-15
Standard
AMS4084E
This specification covers an aluminum alloy in the form of sheet.
CURRENT
2017-06-15
Standard
AMS4046G
This specification covers an aluminum alloy in the form of sheet and plate clad on one side.
2017-06-15
WIP Standard
AMS6407K
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
2017-06-13
WIP Standard
J2932
This document provides test performance requirements for air disc brake actuators for service and combination service parking brake actuators with respect to function, durability and environmental performance when tested according to SAE J2902.
CURRENT
2017-06-13
Standard
AMS5826E
This specification covers a corrosion and heat-resistant steel in the form of welding wire.
2017-06-13
WIP Standard
B17AD
Specification to cover the technical requirements for a high density ceramic peening media.
CURRENT
2017-06-13
Standard
AMSA21180C
This specification covers the requirements for six alloy compositions, four inspection classes, four radiographic quality grades and six classes of mechanical properties of high strength aluminum-alloy castings.
CURRENT
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).
CURRENT
2017-06-12
Standard
AS7106/2B
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.
CURRENT
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.
CURRENT
2017-06-09
Standard
AMS4352J
This specification covers a magnesium alloy in the form of extruded bars, rods, wire, tubing, and profiles up to 40 in2 (258 cm2) in cross-sectional area (solids) and up to 8.5 inches (216 mm) OD by 1.188 inches (30.18 mm) wall thickness (tubing) (see 8.4).
CURRENT
2017-06-09
Standard
AMS1424N
This foundation specification (AMS1424N) and its associated category specifications (AMS1424/1 and AMS1424/2) cover a deicing/anti-icing material in the form of a fluid.
CURRENT
2017-06-08
Standard
AS7109/7B
This document has been declared "CANCELLED" as of June 2017 and has been superseded by PRI AC7109/7. By this action, this document will remain listed in the Numerical Section of the Aerospace Standards Index noting that it is superseded by PRI AC7109/7. Cancelled specifications are available from SAE.
CURRENT
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.
CURRENT
2017-06-07
Standard
AS7109/4B
This document has been declared "CANCELLED" as of June 2017 and has been superseded by PRI AC7109/4. By this action, this document will remain listed in the Numerical Section of the Aerospace Standards Index noting that it is superseded by PRI AC7109/4. Cancelled specifications are available from SAE.
CURRENT
2017-06-07
Standard
AS7109/5B
This document has been declared "CANCELLED" as of June 2017 and has been superseded by PRI AC7109/5. By this action, this document will remain listed in the Numerical Section of the Aerospace Standards Index noting that it is superseded by PRI AC7109/5. Cancelled specifications are available from SAE.
CURRENT
2017-06-07
Standard
AS7109/3B
This document has been declared "CANCELLED" as of June 2017 and has been superseded by PRI AC7109/3. By this action, this document will remain listed in the Numerical Section of the Aerospace Standards Index noting that it is superseded by PRI AC7109/3. Cancelled specifications are available from SAE.
Viewing 121 to 150 of 20352