Standard
Syntactic Foam Tiles
2016-11-10
CURRENT
AMS3709D
This specification covers dielectrically-loaded syntactic foam tiles having a polyimide resin matrix.
Search Results
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, 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
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.
Standard
Organic Fiber (Para-Aramid), Yarn and Roving, High Modulus
1998-09-01
CURRENT
AMS3901C
This specification and its supplementary detail specifications covers organic fibers in the form of continuous, multifilament yarn and roving.
Standard
Organic Fiber (Para-Aramid), Yarn and Roving Intermediate Modulus For Cables, Cordage, and Woven Goods
1999-03-01
HISTORICAL
AMS3904B
This specification and its supplementary detail specifications cover intermediate modulus para-aramid organic fibers in the form of continuous, multifilament yarn and roving.
Standard
Organic Fiber (Para-Aramid), Yarn and Roving Intermediate Modulus For Cables, Cordage, and Woven Goods
2016-08-01
CURRENT
AMS3904C
This specification and its supplementary detail specifications cover intermediate modulus para-aramid organic fibers in the form of continuous, multifilament yarn and roving.
Standard
Nadcap REQUIREMENTS FOR COMPOSITES
2004-05-26
HISTORICAL
AS7118
This Aerospace Standard (AS) establishes the requirements for suppliers of Composites to be accredited by Nadcap. Nadcap accreditation is granted in accordance with SAE AS7003 after demonstration of compliance with the requirements herein. The requirements may be supplemented by additional requirements specified by the Nadcap Composites Task Group. Using the corresponding Audit Criteria (PRI AC7118) will ensure that accredited Composites suppliers meet all of the requirements in this standard and all applicable supplementary standards and applicable AS7118 slash sheets. The purpose of this audit program is to assess a supplier’s ability to consistently provide a product or service that conforms to the technical specifications and customer requirements. The corresponding audit criteria is also structured to obtain information relevant to management practices and processes that directly or indirectly affect the product or service.
Standard
Glass Roving, Epoxy Resin Preimpregnated Type E Glass
2016-11-10
CURRENT
AMS3828D
This specification covers glass roving impregnated with epoxy resin, the resin being partially processed to a "B" stage condition.
Standard
Glass Roving, Epoxy Resin Preimpregnated Type E Glass
1998-09-01
HISTORICAL
AMS3828C
This specification covers glass roving impregnated with epoxy resin, the resin being partially processed to a "B" stage condition.
Standard
GRAPHITE FIBER TAPE AND SHEET Polysulfone Resin Impregnated
1980-04-15
HISTORICAL
AMS3899
This specification and its supplementary detail specifications cover graphite fibers in the form of tape and sheet impregnated with heat-activated, formable, thermoplastic polysulfone resin.
Standard
FIBERS, GRAPHITE TOW AND YARN For Structural Composites
1972-11-15
HISTORICAL
AMS3892
This specification and its supplementary detail specifications cover graphite fibers in the form of continuous multifilament tow and yarn.
Standard
FIBERS, CARBON (GRAPHITE), TOW AND YARN, For Structural Composites
1984-07-01
HISTORICAL
AMS3892A
This specification and its supplementary detail specifications cover carbon (graphite) fibers in the form of continuous multifilament tow and yarn.
Standard
Core, Overexpanded Honeycomb, Polyamide Paper Base, Phenolic Coated
2022-08-10
CURRENT
AMS3714D
This specification covers honeycomb core made of polyamide paper sheets and supplied in the form of blocks, slices, and ordered shapes, the cells of the core being in an overexpanded, rectangular configuration.
Standard
Core, Honeycomb, Glass/Polyimide
2022-08-10
CURRENT
AMS3712C
This specification covers expanded honeycomb core made of glass cloth impregnated with polyimide resin and supplied in the form of blocks, slices, and ordered shapes.
Standard
Core, Honeycomb, Glass/Phenolic
2022-08-10
CURRENT
AMS3715D
This specification covers honeycomb core made of glass fabric impregnated with phenolic resin and supplied in the form of blocks, slices, and ordered shapes.
Standard
Core, Flexible Honeycomb, Polyamide Paper Base, Phenolic Coated
2013-07-16
CURRENT
AMS3713D
This specification covers honeycomb core made of polyamide paper sheets in a non-hexagonal, flexible cell configuration and supplied in the form of blocks, slices, and ordered shapes.
Standard
Core Material, Plastic Honeycomb, Nylon Paper Base for Aircraft Structural Applications
2022-08-10
CURRENT
AMSC81986
This specification covers the requirements for nonperforated nylon paper base plastic honeycomb core material for aircraft structural applications, including exterior parts such as radio and radar antenna housings.
Standard
Core Material, Plastic Honeycomb, Laminated Glass Fabric Base for Aircraft Structural and Electronic Applications
2022-08-10
CURRENT
AMSC8073
This specification covers the requirements for glass fabric base plastic honeycomb core materials for aircraft structural applications, including aircraft exterior parts, such as radio and radar antenna housings, and other parts.
