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Organization / Document #
SAE
Search Result: About 7445 results.

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  • 【Organization】SAE
  • 【Document #】SAE AIR5875

  • Methodology for Investigation of Flight Control System Anomalies

  • 【Date】2005/6/1
  • 【Reaffirmed Date】(R 2011)
  • 【Language】English
  • 【Status】Active
  • 【Organization】SAE
  • 【Document #】SAE AS5878

  • Nut, Self-Locking, Nickel Alloy, UNS N07001, 1400 °F, 180,000 psi, UNJ Thread Procurement Specification

  • 【Date】2005/6/1
  • 【Reaffirmed Date】(R 2018)
  • 【Language】English
  • 【Status】Active
  • 【Organization】SAE
  • 【Document #】SAE ARP5293

  • Safety Considerations for Lasers Projected in the Navigable Airspace

  • 【Date】2005/6/1
  • 【Reaffirmed Date】(R 2010)
  • 【Language】English
  • 【Status】Active
  • 【Organization】SAE
  • 【Document #】SAE AIR5642

  • The Effect of Installation Power Losses on the Overall Performance of a Helicopter

  • 【Date】2005/6/1
  • 【Language】English
  • 【Status】Active
  • 【Organization】SAE
  • 【Document #】SAE AS85049/133

  • CONNECTOR ACCESSORIES, FIBER OPTIC BACKSHELL, 90°, SELF-LOCKING CATEGORY 3B FOR MIL-DTL-38999 SERIES III & SAE AS5590/1 CONNECTORS

  • 【Date】2005/5/1
  • 【Reaffirmed Date】(R 2016)
  • 【Language】English
  • 【Status】Active
  • 【Organization】SAE
  • 【Document #】SAE AS85049/131

  • CONNECTOR ACCESSORIES, FIBER OPTIC BACKSHELL, STRAIGHT, SELF-LOCKING CATEGORY 3B FOR MIL-DTL-38999 SERIES III & SAE AS5590/1 CONNECTORS

  • 【Date】2005/5/1
  • 【Reaffirmed Date】(R 2016)
  • 【Language】English
  • 【Status】Active
  • 【Organization】SAE
  • 【Document #】SAE ARP5600

  • Disposition of Damaged Wheels Involved in Accidents/Incidents

  • 【Date】2005/5/1
  • 【Reaffirmed Date】(R 2015)
  • 【Language】English
  • 【Status】Active
  • 【Organization】SAE
  • 【Document #】SAE AS5202A

  • PORT OR FITTING END, INTERNAL STRAIGHT THREAD, DESIGN STANDARD - Best Copy Available

  • 【Date】2005/5/1
  • 【Reaffirmed Date】(R 2013)
  • 【Language】English
  • 【Status】Active
  • 【Organization】SAE
  • 【Document #】SAE J2051

  • Qualifications for Four-Way Subbase Mounted Air Valves for Automotive Manufacturing Applications

  • 【Date】2005/5/1
  • 【Language】English
  • 【Status】Active
  • 【Organization】SAE
  • 【Document #】SAE AMS4203C

  • Aluminum Alloy, Plate 6.2Zn - 1.8Cu - 2.4Mg - 0.13Zr (7010-T7351) Solution Heat Treated, Stress Relieved, and Precipitation Heat Treated - UNS A97010

  • 【Date】2005/4/1
  • 【Reaffirmed Date】(R 2017)
  • 【Language】English
  • 【Status】Active