Search Results

Standard

Structural Weldbonding of Aluminum Structures

2014-08-14

CURRENT

ARP1675

This SAE Aerospace Recommended Practice describes the aluminum weldbonding process for fabrication of secondary aircraft structural assemblies possessing excellent strength, fatigue life, and environmental durability.

Standard

Silica Cloth, "B" Stage Phenolic Resin Impregnated High Pressure Molding

1990-01-01

CURRENT

AMS3830A

This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of January 1990.

Standard

Sandwich Structures, Glass Fabric-Resin Low Pressure Molded, Heat Resistant

2022-12-29

CURRENT

AMS3710C

This specification covers a resin-impregnated glass fabric honeycomb core in the form of flat or contoured sandwich structures.

Standard

Sandwich Constructions and Core Materials: General Test Methods

2023-04-21

CURRENT

AMSSTD401

This standard covers the general requirements and methods for testing sandwich core materials and for testing sandwich construction of the types used primarily in aircraft structures. This standard does not include test methods applicable only to a specific product; such test methods are included in the detailed specifications for the product.

Standard

Roving, Type "S-2" Glass Epoxy Resin Impregnated

2016-12-16

CURRENT

AMS3832D

This specification covers continuous, multiple-strand, roving of Type "S-2" glass impregnated with a heat-curable epoxy resin matrix and processed to a "B" stage condition.

Standard

Roving, Organic Fiber (Para-Aramid), High Modulus 8520 Denier, (9500 d tex), 0.6% Finish

2014-07-31

CURRENT

AMS3901/16B

This specification covers one type of organic fiber in the form of roving. The product shall be formed as three ends of 2840 (3160 d tex) denier yarn (AMS3901/14) collected into an approximately parallel arrangement without twist.

Standard

Roving, Organic Fiber (Para-Aramid), High Modulus 7350 Denier, (8200 d tex), 0.6% Finish

2014-07-31

CURRENT

AMS3901/15B

This specification covers one type of organic fiber in the form of roving. The product shall be formed as three ends of 2450 denier yarn (AMS3901/13) collected into an approximately parallel arrangement without twist.

Standard

Roving, Organic Fiber (Para-Aramid), High Modulus 7100 Denier, (7900 d tex), 0.6% Finish

2014-07-30

CURRENT

AMS3901/5D

This specification covers one type of organic fiber in the form of roving. The product shall be formed as five ends of 1420 denier (1580 d tex) yarn (AMS3901/4) collected into an approximately parallel arrangement without twist.

Standard

Roving, Organic Fiber (Para-Aramid), High Modulus 4560 Denier, (5070 d tex), 0.6% Finish

2014-07-30

CURRENT

AMS3901/6D

This specification covers one type of organic fiber in the form of roving. The product shall be formed as four ends of 1140 denier (1270 d tex) yarn (AMS3901/3) collected into an approximately parallel arrangement without twist.

Standard

Resin, Polyimide, Laminating High Temperature Resistant, 315 °C (599 °F)

1998-09-01

HISTORICAL

AMS3619C

This specification covers a single-component, heat-reactive, thermosetting aromatic system which thermally cures to form a polyimide polymer structure.

Standard

Resin System, Epoxy, Carbon Microballoon Filled, 135 °C (275 °F) Cure

2022-12-29

CURRENT

AMS3699A

This specification covers a two-part epoxy resin system in the form of a bisphenol "A" epoxy resin filled with fumed silica and carbon microspheres and a separate curing agent.

Standard

ROVING, TYPE "S-2" GLASS Epoxy Resin Impregnated

1994-05-01

HISTORICAL

AMS3832C

This specification covers continuous, multiple-strand, roving of Type "S-2" glass impregnated with a heat-curable epoxy resin matrix and processed to a "B" stage condition.

Standard

RESIN, EPOXY, MATRIX, THERMOSETTING Moderate Temperature Resistant, Unfilled

1988-07-01

HISTORICAL

AMS3727

This specification covers a heat-reactive, thermosetting, epoxy resin matrix in the form of a semi-solid. The resin matrix thermally cures to an epoxy polymer.

Standard

Quality Inspection Procedure, Composites Tracer Fluoroscopy and Radiography

2022-06-05

CURRENT

ARP1611A

This document describes an inspection procedure for detecting, by use of a radiographic opaque tracer and fluoroscopy or radiography methods, flaws which have been produced as the result of cutting, machining, or drilling operations in composite or laminate structures.

Standard

Primer, Adhesive, Electrodeposited -55 to +82 °C (-67 to +180 °F)

2022-08-10

CURRENT

AMS3109

This specification covers a corrosion-inhibiting, water soluble, modified epoxy primer in liquid form.

Standard

Primer, Adhesive, Corrosion-Inhibiting for High Durability Structural Adhesive Bonding

2022-08-10

CURRENT

AMS3107A

This specification and its supplementary detail specifications cover corrosion-inhibiting, modified epoxy primers in the form of ready-to-use sprayable liquids.

Standard

Polyimide Printed Circuit Boards Fabrication of

2022-06-05

CURRENT

ARP1612A

This document describes the materials, equipment, and processing techniques utilized in the fabrication of polyimide printed wiring boards. Included are recommendations for both double-sided and multilayer boards.

Standard

Physical-Chemical Characterization Techniques, Epoxy Adhesive and Prepreg Resin Systems

2022-06-05

CURRENT

ARP1610A

This recommended practice describes the physical and chemical characterization techniques for identification of epoxy adhesive and prepreg resin systems in order to verify the chemical formulation, resin B-staging (See 8.1), cure reaction rates, adhesive moisture content, and resin component mix ratios, as necessary to achieve manufacturing and quality producibility and engineering performance.

Standard

Paper Honeycomb 60 lb (25 kg) Paper

2016-11-10

CURRENT

AMS3720C

This specification covers paper base honeycomb material having a cell size of 0.330 or 0.440 in. (8.38 or 11.18 mm). Unless otherwise ordered, size 0.440 in. (11.18 mm) be supplied.

Standard

PAPER HONEYCOMB 125 lb (55 kg) Paper

1994-04-01

HISTORICAL

AMS3722A

This specification covers paper base honeycomb material having a cell size of 0.440 in. (11.18 mm). Unless otherwise ordered, size 0.440 in. (11.18 mm) will be supplied.