Search Results

Standard

Aircraft Sealant Removal Techniques

2024-05-03

WIP

AIR3270B

This SAE Aerospace Information Report (AIR) provides information on the possible methods of sealant removal. The discussion will focus on the methods of sealant removal and give the strengths and weaknesses of each method.

Standard

Combination Pelvic and Upper Torso Operator and Occupant Restraint Systems for Off-Road Work Machines

2024-05-02

WIP

J2292

This SAE Recommended Practice establishes minimum performance and test requirements for combination pelvic and upper torso occupant restraint systems provided for off-road self-propelled work machines.

Standard

Magnesium Alloy, Extrusions, 5.5Zn - 0.45Zr (ZK60A-T5), Precipitation Heat Treated

2024-05-01

CURRENT

AMS4352K

This specification covers a magnesium alloy in the form of extruded bars, rods, wire, tubing, and profiles up to 40 square inches (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 8.5).

Standard

Primer, Anodic Electrodeposition for Aircraft Applications

2024-05-01

WIP

AMS3144B

This specification establishes the requirements for a waterborne, corrosion inhibiting, chemical and solvent resistant, anodic electrodeposition epoxy primer capable of curing at 200 to 210 °F (93 to 99 °C).

Standard

Application of AMS3144 Anodic Electrodeposition Primer

2024-05-01

WIP

G824AB

This standard establishes the recommended requirements for application of AMS3144 anodic electrodeposition primer to aerospace components. Adherence to these requirements will help facilitate satisfactory performance of the applied primer.

Standard

May 2024 Reaffirmation Ballot

2024-04-30

WIP

RefirmAE8C25-24

Reaffirm

Standard

Coating System, Advanced Performance, for Exterior Aerospace Applications

2024-04-30

WIP

G824AA

This specification establishes the requirements for coating systems having high durability for use as aircraft exterior surface finishes. These coating systems normally are comprised of a surface treatment, a primer, and a topcoat and include a chemical stripper and a cleaning compound for topcoat washing.

Standard

TERMINAL, LUG, CRIMP STYLE, COPPER, UNINSULATED, FLAG TONGUE, SIZES 8-0000, TYPE I, CLASS I, FOR 150 °C TOTAL CONDUCTOR TEMPERATURE

2024-04-29

WIP

AS25189D

Scope is unavailable.

Standard

TERMINAL, LUG, CRIMP STYLE, COPPER, UNINSULATED, FLAG TONGUE, SIZES 22-10, TYPE I, CLASS I, FOR 150 ºC TOTAL CONDUCTOR TEMPERATURE

2024-04-29

WIP

AS7928/15C

Scope is unavailable.

Standard

TERMINALS, LUG AND SPLICES, CONDUCTOR, CRIMP STYLE, SPLICE, ELECTRIC, TIN WHISKER RESISTANT (PERMANENT, TYPE II, CLASS 1) FOR 105 °C TOTAL CONDUCTOR TEMPERATURE

2024-04-29

WIP

AS7928/10F

Scope is unavailable.

Standard

Passenger Vehicle Windshield Demisting and Defrosting Systems

2024-04-29

WIP

J902

This SAE Recommend Practice establishes for passenger cars, light trucks, and multipurpose vehicles with GVW of 4500 kg (10000 pounds) or less, as defined by EPA, and M1 category vehicles as defined by the European Commission:Minimum performance standards for defrosting and demisting systems.Test procedures that can be conducted on uniform test equipment by commercially available laboratory facilities.This procedure may be used to develop or to validate a defrosting and defogging system.

Standard

Laser Powder Bed Fusion Produced Parts, Aluminum Alloy 7A50.60L (A7050-RAM2, composition similar to UNS A97050), Hot Isostatic Pressed and T74 Aged

2024-04-26

WIP

AMS7071

Material specification for parts produced using 7A50.60L (A7050-RAM2) using the laser powder bed fusion process

Standard

Steel, Corrosion Resistant Bars and Forgings, 12.5Cr - 1.0Ni - 15.5Co - 2.0Mo, Vacuum Induction Plus, Vacuum Consumable Electrode Remelted

2024-04-26

WIP

AMS5933B

This specification covers a premium aircraft-quality corrosion-resistant steel in the form of bars, forgings, and forging stock.

Standard

F23AB/AMS5971 Steel, Corrosion-Resistant, Bars, Wire, Forgings and Forging Stock 12.25Cr– 2.5Ni – 0.6Mo -- 0.45Ti (<0.13C), Carburizing Aircraft Premium Quality, VIM-VAR or VAR, 190ksi (Composition similar to UNS S41429)

2024-04-26

WIP

F23AB/AMS5971

This specification covers a premium aircraft-quality, corrosion-resistant steel in the form of bars, wire, forgings, and forging stock.

Standard

F23AA/AMS5970 Steel, Corrosion-Resistant, Bars, Wire, Forgings and Forging Stock 12.25Cr– 2.5Ni – 0.6Mo -- 0.45Ti (<0.13C), Carburizing Aircraft Premium Quality, VIM-VAR or VAR, 170ksi (Composition similar to UNS S41429)

2024-04-26

WIP

F23AA/AMS5970

This specification covers a premium aircraft-quality, corrosion-resistant steel in the form of bars, wire, forgings, and forging stock

Standard

Terminals: Lug and Splice, Crimp Style, Aluminum, for Aluminum Aircraft Wire

2024-04-25

WIP

AS70991D

This specification covers crimp-style aluminum lug terminals and conductor splices for aluminum aircraft wire. Lug terminals and conductor splices are hereafter called “terminals.”

Standard

SHIELD TERMINATION, SOLDER STYLE, INSULATED, HEAT-SHRINKABLE, ENVIRONMENT RESISTANT WITH PRE INSTALLED LEADS FOR CABLES HAVING TIN OR SILVER PLATED SHIELDS (CLASS I)

2024-04-25

WIP

AS83519/2B

SCOPE IS UNAVAILABLE.

Standard

SHIELD TERMINATION, SOLDER STYLE, INSULATED, HEAT-SHRINKABLE, ENVIRONMENT RESISTANT FOR CABLES HAVING TIN OR SILVER PLATED SHIELDS (CLASS I)

2024-04-25

WIP

AS83519/1C

SCOPE IS UNAVAILABLE.

Standard

Splice, Electric, Crimp, Copper, Environment Resistant

2024-04-25

WIP

AS81824F

The AS81824 specification covers environment resistant, permanent crimp type, splices having heat shrinkable insulating sleeve and meltable environmental seals or heatless sealing sleeves. The splices may be used with tin, nickel, and silver-plated conductors in applications where the total temperature of the splice application does not exceed 200 °C or as specified in the detail specification.

Standard

Low Voltage Primary Cable

2024-04-25

WIP

J1128

This SAE Standard covers low voltage primary cable intended for use at a nominal system voltage of 60 VDC (25 VAC) or less in surface vehicle electrical systems. The tests are intended to qualify cables for normal applications with limited exposure to fluids and physical abuse.