Standard
Cloth, Aramid Intermediate Modulus
2022-10-04
CURRENT
AMS3909B
This specification and its supplementary detail specifications cover an intermediate modulus aramid yarn in the form of cloth.
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Standard
Mold Release Agent
2022-10-04
CURRENT
AMS3091C
This specification covers a mold release agent in the form of a liquid.
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
Primer, Adhesive, Corrosion-Inhibiting High Durability Epoxy, -55 to +215 °C (-67 to +419 °F)
2022-08-10
CURRENT
AMS3107/4A
This specification covers a corrosion-inhibiting, modified epoxy resin primer in the form of a ready-to-use, sprayable liquid.
Standard
Primer, Adhesive, Corrosion-Inhibiting High Durability Epoxy, -55 to +175 °C (-67 to +347 °F)
2022-08-10
CURRENT
AMS3107/3A
This specification covers a corrosion-inhibiting, modified epoxy resin primer in the form of a ready-to-use, sprayable liquid.
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
350 °F Autoclave Cure, Low Flow Toughened Epoxy Prepregs, Type 38, Class 2, Grade 193, Style 3K-70-PW, Fiber 1
2019-03-12
WIP
AMS3961/1A
The intent of this specification is for the procurement of the material listed on the QPL and, therefore, no qualification or equivalency threshold values are provided. Users that intend to conduct a new material qualification or equivalency program shall refer to the Quality Assurance section of the base specification, AMS3961. All material qualification and equivalency data has been archived and is available for review upon request. Contact the CMH-17 Secretariat (www.cmh17.org) for additional information.
Standard
350 °F Autoclave Cure, Low Flow Toughened Epoxy Prepregs, Type 35, Class 1, Grade 190, Fiber 2
2019-03-12
WIP
AMS3961/2A
The intent of this specification is for the procurement of the material listed on the QPL and, therefore, no qualification or equivalency threshold values are provided. Users that intend to conduct a new material qualification or equivalency program shall refer to the Quality Assurance section of the base specification, AMS3961. All material qualification and equivalency data has been archived and is available for review upon request. Contact the CMH-17 Secretariat (www.cmh17.org) for additional information.
