SAE
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- 【Organization】SAE
- 【Document #】SAE AS1974
Clamps, Support, Comparative Fatigue Strengths, Test Method
- 【Date】2003/4/1
- 【Reaffirmed Date】(R 2013)
- 【Language】English
- 【Status】Active
- 【Organization】SAE
- 【Document #】SAE ARP5015A
Ground Equipment - 400 Hertz Ground Power Performance Requirements
- 【Date】2003/4/1
- 【Reaffirmed Date】(R 2011)
- 【Language】English
- 【Status】Active
- 【Organization】SAE
- 【Document #】SAE PT-94
Homogeneous Charge of Compression Ignition (HCCI) Engines: Key Research and Development Issues
- 【Date】2003/3/20
- 【Language】English
- 【Status】Active
- 【Organization】SAE
- 【Document #】SAE ARP1409C
(R) Aircraft On Board Weight and Balance System Requirements
- 【Date】2003/3/1
- 【Reaffirmed Date】(R 2018)
- 【Language】English
- 【Status】Active
- 【Organization】SAE
- 【Document #】SAE AMS4233C
Aluminum Alloy, Welding Wire 4.5Cu - 0.70Ag - 0.30Mn - 0.25Mg - 0.25Ti (201) - UNS A02010
- 【Date】2003/3/1
- 【Reaffirmed Date】(R 2014)
- 【Language】English
- 【Status】Active
- 【Organization】SAE
- 【Document #】SAE AMS2801B
Heat Treatment of Titanium Alloy Parts
- 【Date】2003/3/1
- 【Reaffirmed Date】(R 2014)
- 【Language】English
- 【Status】Active
- 【Organization】SAE
- 【Document #】SAE ARP5364
Human Factor Considerations in the Design of Multifunction Display Systems for Civil Aircraft
- 【Date】2003/3/1
- 【Language】English
- 【Status】Active
- 【Organization】SAE
- 【Document #】SAE AIR825/5A
Liquid Oxygen Systems
- 【Date】2003/3/1
- 【Reaffirmed Date】(R 2018)
- 【Language】English
- 【Status】Active
- 【Organization】SAE
- 【Document #】SAE AS172321 THRU AS172370A
NUT, SPANNER, AERONAUTICAL, UNS G41400
- 【Date】2003/3/1
- 【Reaffirmed Date】(R 2012)
- 【Language】English
- 【Status】Active
- 【Organization】SAE
- 【Document #】SAE AIR825/12A
Oxygen System Integration and Performance Precautions
- 【Date】2003/3/1
- 【Reaffirmed Date】(R 2018)
- 【Language】English
- 【Status】Active