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Alloys AMS P17 Polymer Matrix Composites Committee Steel Wrought alloys Materials identification Forming Magnesium alloys

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Standard

350 °F Autoclave Cure, Low Flow Toughened Epoxy Prepregs
2015-12-02
CURRENT
AMS3961
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 this 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 All material qualification and equivalency data has been archived and is available for review upon request.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
2019-03-12
WIP
AMS3961A
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 this 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 All material qualification and equivalency data has been archived and is available for review upon request.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

Acceptance Criteria Adhesive-Bonded Metal-Faced Sandwich Structures
2022-08-10
CURRENT
AMS3920A
This specification establishes the acceptance criteria and inspection requirements for adhesive-bonded sandwich structures including the metal-to-metal bonding found in these structures, but usage is not limited to such applications and each application should be considered individually.
Standard

Adhesive, Film Form Metallic Structural Sandwich Construction
2022-10-04
CURRENT
AMSA25463
This specification covers the requirements for adhesives in film form for bonding metal facings to metal cores and to metal components of sandwich panels which are intended for use in primary and secondary structural airframe parts that may be exposed to temperatures up to 500°F (260°C).
Standard

CLOTH, TYPE "E" GLASS, "B" STAGE POLYIMIDE-RESIN-IMPREGNATED 181 Style Fabric, Low-Flow Addition-Cure Resin For Press Cure at 40 - 100 psi (275 - 690 kPa) or Vacuum/Autoclave Processing
1985-04-01
HISTORICAL
AMS3845/1A
This specification covers one type of glass cloth impregnated with a heat-reactive, addition-cure, thermosetting, polyimide-resin system, the resin to be supplied in a "B" stage condition for low flow and press cure at 40 - 100 psi (275 - 690 kPa) or vacuum/autoclave processing.
Standard

Carbon Fiber and Fiberglass Epoxy Prepreg Products with 350 °F (177 °C) Cure for Aerospace Applications
2020-12-30
CURRENT
AMS6891
The intent of this specification is for the procurement of carbon fiber and fiberglass epoxy prepreg products with 350 °F (177 °C) cure for aerospace applications; therefore, no qualification or equivalency threshold values are provided. Users that intend to conduct a new material qualification or equivalency program must refer to the production quality assurance section (4.3) of this base specification, AMS6891.
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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