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Life cycle analysis AMS P17 Polymer Matrix Composites Committee Electrical, Electronics, and Avionics Assembling

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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 All material qualification and equivalency data has been archived and is available for review upon request.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 All material qualification and equivalency data has been archived and is available for review upon request.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

Cure Monitor, Electrical Methods
2022-06-07
CURRENT
ARP1926
This document describes a standard method to collect and report dielectric data for the purpose of monitoring or studying the cure of composites.
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

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

Surface Preparation and Priming of Aluminum Alloy Parts for High Durability Structural Adhesive Bonding
2018-11-15
WIP
ARP1524B
This Aerospace Recommended Practice (ARP) describes the processing system and techniques for the surface preparation and priming of aluminum alloy parts for structural adhesive bonding to achieve optimum bondline durability, corrosion resistance, and manufacturing producibility. While this surface preparation has been developed and validated for two high strength aluminum alloys, 2024 and 7075, in the hardened condition it is expected to be applicable to other alloys and tempers. This surface preparation system has been validated for use with 180 degrees F (82 degrees C) and with 250 degrees F (121 degrees C) curing elastomer-modified epoxy adhesive and corrosion-inhibiting primer. The processes described herein are the result of laboratory evaluation of structural and durability performance.
Standard

Syntactic Foam Tiles
2016-11-10
CURRENT
AMS3709D
This specification covers dielectrically-loaded syntactic foam tiles having a polyimide resin matrix.
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