Search Results

Standard

STEEL, SHEET, STRIP, AND PLATE 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130) Normalized or Otherwise Heat Treated

1996-11-01

HISTORICAL

AMS6345

This specification covers an aircraft-quality, low-alloy steel in the form of sheet, strip, and plate.

Standard

PRESSURE ALTIMETER SYSTEMS

1996-10-29

HISTORICAL

AS8009A

This Aerospace Standard (AS) specifies minimum performance requirements for primary pressure altimeter systems other than air data computers. This AS covers altimeter systems that measure and display altitude as a function of atmospheric pressure. The pressure transducer may be contained within the instrument display case or located remotely. Requirements for air data computers are specified in AS8002. Some requirements for nontransducing servoed altitude indicators are included in AS791. The instrument system specified herein does not include aircraft pressure lines. Unless otherwise specified, whenever the term "instrument" is used, it is to be understood to be the complete system of pressure transducer components, any auxiliary equipment, and display components. The test procedures specified herein apply specifically to analog type instruments. Digital instruments or automatic test instrumentation may require other test procedures.

Technical Paper

Smart Cars: 2000 Or 2020?

1996-10-21

96C026

Emerging commercial and aerospace electronics technologies are significant enablers for a new era of smart cars that might become available at the turn of the century. However, strong inhibitors such as cost, electronics architecture, government regulation, and highway and vehicle manufacturer infrastructure threaten to delay the benefits of smart car functions to the year 2020 or beyond. This paper examines these enablers and inhibitors and discusses steps that the auto industry and government might take to accelerate the deployment of smart car functions.

Standard

OXYGEN SYSTEM AND COMPONENT CLEANING AND PACKAGING

1996-10-18

HISTORICAL

AIR1176A

This Aerospace Information Report (AIR) specifies work area details, cleaning methods, test methods, and specifications for oxygen clean parts and packaging materials.

Standard

FINING END, INTEGRAL CENTERED WELD LIP, DESIGN STANDARD, METRIC

1996-10-01

HISTORICAL

MA2307

Standard

AGS3815 Bearing, Self-Aligning, Plain Outer Ring, P.T.F.E. Lined, Narrow

1996-10-01

CURRENT

AGS3815-3

No scope available.

Standard

AGS3812 Bearing, Self-Aligning, Grooved Outer Ring, P.T.F.E. Lined, Wide

1996-10-01

CURRENT

AGS3812-3

No scope available.

Standard

AGS3813 Bearing, Self-Aligning, Grooved Outer Ring, P.T.F.E. Lined, Narrow

1996-10-01

CURRENT

AGS3813-3

No scope available.

Standard

AGS3814 Bearing, Self-Aligning, Plain Outer Ring, P.T.F.E. Lined, Wide

1996-10-01

CURRENT

AGS3814-3

No scope available.

Standard

Plastic Tubing, Electrical Insulation, Polytetrafluoroethylene, Heat Shrinkable, Overexpanded

1996-10-01

CURRENT

AMS3584D

No scope available.

Standard

Resin, Polyimide, Laminating and Molding High Temperature Resistant, 370°C (700°F) Unfilled, Addition Polymer

1996-10-01

CURRENT

AMS3616C

No scope available.

Standard

Plastic Extrusions, Flexible, Polyvinyl Chloride

1996-10-01

CURRENT

AMS3630F

This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1996.

Standard

Plastic Molding Compound, Novolac Epoxy Resin, Short Glass Fiber Reinforced, Structural

1996-10-01

CURRENT

AMS3671C

This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1996.

Standard

Plastic Moldings, Electrical Insulation, Crosslinked Polyolefin, Pigmented, Flexible, Heat Shrinkable

1996-10-01

CURRENT

AMS3674D

This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1996.

Standard

AIRCRAFT DEICING/ANTI-ICING METHODS WITH FLUIDS

1996-10-01

HISTORICAL

ARP4737A

This document establishes the minimum criteria for ground based aircraft deicing/anti-icing with fluids to ensure the safe operation of aircraft during icing conditions. This document does not specify requirements for particular airplane models.

Standard

Plastic Sheet, Methyl Methacrylate, General Purpose

1996-10-01

CURRENT

AMS3608D

This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1996.

Standard

Plastic Moldings and Extrusions Cellulose Acetate, General Purpose

1996-10-01

CURRENT

AMS3622D

This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1996.

Standard

Polyvinyl Chloride Tubing, Extruded, High Temperature Electrical Insulation

1996-10-01

CURRENT

AMS3629B

This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1996.

Standard

Plastic Moldings, Melamine-Formaldehyde, Mineral Filled

1996-10-01

CURRENT

AMS3640F

This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1996.

Standard

STEEL, INVESTMENT CASTINGS 0.50Cr - 0.55Ni - 0.25Mo (0.11 - 0.17C) (SAE 8615) Normalized

1996-10-01

HISTORICAL

AMS5333D

This specification covers a low-alloy steel in the form of investment castings.