Standard
Mold Release Agent
2022-10-04
CURRENT
AMS3091C
This specification covers a mold release agent in the form of a liquid.
Search Results
Standard
Cloth, Aramid (Para) Plain Weave, Thermally Stable
2022-10-04
CURRENT
AMS3908A
This specification covers a thermally stable aramid fabric in the form of cloth.
Standard
Cloth, Aramid 5 oz per sq yd (170 g/m2) Basket Weave
2022-10-04
CURRENT
AMS3907/1
This specification covers one weight and type of weave of aramid cloth.
Standard
Cloth, Aramid 4.3 oz per sq yd (145 g/m2) Plain Weave
2022-10-04
CURRENT
AMS3907/2
This specification covers one weight and type of weave of aramid cloth.
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.
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
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
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
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
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
Interleaf Carrier Material, Composite Tape or Broadgoods Paper, 0.004 inch (0.10 mm), Perforated
2022-04-13
CURRENT
AMS3898B
This specification and its supplementary detail specifications cover interleaf carrier materials in the form of polyethylene film or coated paper tape or sheeting.
Standard
Advanced Composites Prepreg - Nominal 250 °F Cure - Carbon Fiber and Epoxy Resin, Unidirectional Tape
2021-03-25
WIP
AMS3960B
This specification establishes the requirements for a nominal 250 °F cure epoxy preimpregnated carbon fiber unidirectional tape product. This material is intended for use in laminate applications with a service temperature of -65 to 180 °F. The composite may be used for the manufacture of primary and secondary aircraft structure.
Standard
Advanced Composites Prepreg – Nominal 250 °F Cure –Glass Fiber and Epoxy Resin, 7781 Weave Fabric
2021-03-25
WIP
AMS3915B
This specification establishes the requirements for a nominal 250 °F cure epoxy preimpregnated 7781 glass fabric. The prepreg has a nominal fiber areal weight of 294 gsm, and nominal resin content of 38%.
Standard
Advanced Composites Prepreg - Nominal 250 °F Cure – 12K Tow Carbon Fiber and Epoxy Resin, Plain Weave Fabric
2021-03-25
WIP
AMS3914B
This specification establishes the requirements for a nominal 250 °F cure epoxy preimpregnated carbon fiber plain weave fabric product. The prepreg is a plain weave fabric with 12K tows, a nominal fiber areal weight of 193 gsm, and nominal resin content of 42%.
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
Cloth, Type "S" Glass 181 Style Fabric, Finish No. HTS-904
2016-12-15
CURRENT
AMS3837E
This specification covers "S" glass in one style of woven fabric with an HTS-904 finish.
Standard
Graphite Yarn, Non-Structural 5 Ply Yarn, 720 Filaments
2016-12-15
CURRENT
AMS3890B
The product shall consist of 5-ply yarn having 720 continuous filaments per ply and a maximum of 4 turns per inch (25.4 mm).
Standard
Cloth, Quartz, "B" Stage Polyimide Resin Impregnated Style 581 Fabric, 315 °C (599 °F)
2016-12-15
CURRENT
AMS3847D
This specification covers one type of quartz cloth impregnated with a heat-reactive, thermosetting, polyimide resin system, the resin being processed to a "B" stage condition, and furnished in continuous rolls of full width material.
Standard
Cloth, Type “E” Glass, “B” Stage Polyester-Resin-Impregnated 7781 Style Fabric, Flame Resistant, Improved Strength
2016-12-15
CURRENT
AMS3834B
This specification covers a style 7781 glass cloth impregnated with a heat-curable polyester resin system, the resin being processed to a “B” stage condition, and furnished in the form of continuous rolls.
