SAE
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- 【Organization】SAE
- 【Document #】SAE AS18802
Fuel and Oil Lines, Aircraft, Installation of
- 【Date】1998/1/1
- 【Reaffirmed Date】(R 2013)
- 【Language】English
- 【Status】Active
- 【Organization】SAE
- 【Document #】SAE AS4201A
PORT – RING LOCKED FLUID CONNECTION TYPE, 8000 PSI DESIGN STANDARD
- 【Date】1998/1/1
- 【Reaffirmed Date】(R 2015)
- 【Language】English
- 【Status】Active
- 【Organization】SAE
- 【Document #】SAE J2316
Wheel Nut Seat System Test Procedures and Performance Requirements for Passenger Cars and Light Trucks
- 【Date】1998/1/1
- 【Reaffirmed Date】(R 2012)
- 【Language】English
- 【Status】Active
- 【Organization】SAE
- 【Document #】SAE AIR1326A
Aircraft Fuel System Vapor-Liquid Ratio Parameter
- 【Date】1997/12/1
- 【Reaffirmed Date】(R 2014)
- 【Language】English
- 【Status】Active
- 【Organization】SAE
- 【Document #】SAE ARP1665A
Definition of Pressure Surge Test and Measurement Methods for Receiver Aircraft
- 【Date】1997/12/1
- 【Reaffirmed Date】(R 2007)
- 【Language】English
- 【Status】Active
- 【Organization】SAE
- 【Document #】SAE ARP1892B
Electrical Connectors for Use in Battery Powered Ground Support Equipment
- 【Date】1997/12/1
- 【Reaffirmed Date】(R 2015)
- 【Language】English
- 【Status】Active
- 【Organization】SAE
- 【Document #】SAE ARP699E
High Temperature Pneumatic Duct Systems for Aircraft
- 【Date】1997/12/1
- 【Reaffirmed Date】(R 2015)
- 【Language】English
- 【Status】Active
- 【Organization】SAE
- 【Document #】SAE AS5133
Nut, Floating, Attached Retention Element (A.R.E.) - Hole Dimensions and Installation Requirements
- 【Date】1997/12/1
- 【Reaffirmed Date】(R 2018)
- 【Language】English
- 【Status】Active
- 【Organization】SAE
- 【Document #】SAE AS3067B
NUT, SELF-LOCKING, DOUBLE HEXAGON, REDUCED ENVELOPE, AS7251
- 【Date】1997/12/1
- 【Reaffirmed Date】(R 2012)
- 【Language】English
- 【Status】Active
- 【Organization】SAE
- 【Document #】SAE AS1225A
Oxygen System Fill/Check Valve
- 【Date】1997/12/1
- 【Reaffirmed Date】(R 2017)
- 【Language】English
- 【Status】Active