HG/T 5877\uff5e5879-2021
MIL MIL-R-81294D Amendment 2
REMOVER, PAINT, EPOXY, POLYSULFIDE, AND POLYURETHANE SYSTEMS (SUPERSEDING MIL-R-81294C)
MIL MIL-R-81294D Notice 1-Inactivation
REMOVER, PAINT, EPOXY, POLYSULFIDE, AND POLYURETHANE SYSTEMS (SUPERSEDING MIL-R-81294C)
MIL MIL-R-81294D Amendment 1
REMOVER, PAINT, EPOXY, POLYSULFIDE, AND POLYURETHANE SYSTEMS (SUPERSEDING MIL-R-81294C)
MIL MIL-R-81294D
REMOVER, PAINT, EPOXY, POLYSULFIDE, AND POLYURETHANE SYSTEMS (SUPERSEDING MIL-R-81294C)
SAE AMS6891/3
Carbon Fiber and Fiberglass Epoxy/Prepreg Products with 350 °F (177 °C) Cure for Aerospace Applications: Type 34, Class 4, Grade 294, Style 7781
SAE AMS6891/4
Carbon Fiber and Fiberglass Epoxy/Prepreg Products with 350 °F (177 °C) Cure for Aerospace Applications: Type 42, Class 4, Grade 48, Style 108
SAE AMS3970/2A
Carbon Fiber Fabric Repair Prepreg, 125°C (250°F) Vacuum Curing Part 2 - Qualification Program for Fiber, Fabric, Resin and Film Adhesive
SAE AMS6891/2
Carbon Fiber and Fiberglass Epoxy/Prepreg Products with 350 °F (177 °C) Cure for Aerospace Applications: Type 40, Class 1, Grade 196, Style 6K-PW
SAE AMS3970/2
Carbon Fiber Fabric Repair Prepreg, 125°C (250°F) Vacuum Curing Part 2 - Qualification Program for Fiber, Fabric, Resin and Film Adhesive
DIN EN 2833-3-DRAFT
Draft Document - Aerospace series - Glass fibre thermosetting preimpregnates; technical specification - Part 3: Glass fabric/epoxy resin preimpregnates curing at up to 180 °C for continous use up to 120 °C