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Operator's Seat Dimensions for Off-Road Self-Propelled Work Machines

  • Ground Vehicle Standard
  • J899_202102
  • Current
Published 2021-02-23 by SAE International in United States
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Annotation ability available
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TERMINALS, LUG AND SPLICES, CONDUCTOR, CRIMP STYLE, SPLICE, ELECTRIC, TIN WHISKER RESISTANT (PERMANENT, TYPE II, CLASS 1) FOR 105 °C TOTAL CONDUCTOR TEMPERATURE

  • Aerospace Standard
  • AS7928/10B
  • Current
Published 2021-02-23 by SAE International in United States
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Unidirectional Carbon Fiber Tape Epoxy Repair Prepreg, Vacuum Curing Part 1 - General Requirements

  • Aerospace Material Specification
  • AMS6885/1
  • Current
Published 2021-02-23 by SAE International in United States
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Unidirectional Carbon Fiber Tape Epoxy Repair Prepreg, Vacuum Curing Part 4 - Purchasing Specification for Film Adhesive

  • Aerospace Material Specification
  • AMS6885/4
  • Current
Published 2021-02-22 by SAE International in United States
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Unidirectional Carbon Fiber Tape Epoxy Repair Prepreg, Vacuum Curing Part 3 - Purchasing Specification for Unidirectional Carbon Fiber Tape Epoxy Repair Prepreg

  • Aerospace Material Specification
  • AMS6885/3
  • Current
Published 2021-02-22 by SAE International in United States
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Unidirectional Carbon Fiber Tape Epoxy Repair Prepreg, Vacuum Curing Part 0 - Introduction

  • Aerospace Material Specification
  • AMS6885
  • Current
Published 2021-02-23 by SAE International in United States
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Unidirectional Carbon Fiber Tape Epoxy Repair Prepreg, Vacuum Curing Part 2 - Qualification Program for Fiber, Carbon Fiber Tape Prepreg, and Film Adhesive

  • Aerospace Material Specification
  • AMS6885/2
  • Current
Published 2021-02-23 by SAE International in United States
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Unidirectional Carbon Fiber Tape Epoxy Repair Prepreg, Vacuum Curing Part 5 - Material Specification for Unidirectional Carbon Fiber Tape Epoxy Prepreg for Repair and Film Adhesive for Repair, 120 to 145 °C (250 to 290 °F) Curing

  • Aerospace Material Specification
  • AMS6885/5
  • Current
Published 2021-02-22 by SAE International in United States
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Plating, Nickel Low-Stressed Deposit

  • Aerospace Material Specification
  • AMS2424G
  • Current
Published 2021-02-26 by SAE International in United States
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Processes for Engineering a System

  • Aerospace Standard
  • EIA632A
  • Current
Published 2021-02-23 by SAE International in United States
This content contains downloadable datasets
Annotation ability available