SAE
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- 【Organization】SAE
- 【Document #】SAE AMS3960A
(R) Advanced Composites Prepreg - Nominal 250 °F Cure - Carbon Fiber and Epoxy Resin, Unidirectional Tape
- 【Date】2015/8/1
- 【Language】English
- 【Status】Active
- 【Organization】SAE
- 【Document #】SAE AMS3915A
(R) Advanced Composites Prepreg – Nominal 250 °F Cure – Glass Fiber and Epoxy Resin, 7781 Weave Fabric
- 【Date】2015/8/1
- 【Language】English
- 【Status】Active
- 【Organization】SAE
- 【Document #】SAE ARP1532B
(R) Aircraft Oxygen System Lines, Fabrication, Test, and Installation
- 【Date】2015/8/1
- 【Language】English
- 【Status】Active
- 【Organization】SAE
- 【Document #】SAE ARP5818A
(R) Aircraft Refueling Vehicle Design and Performance Requirements
- 【Date】2015/8/1
- 【Language】English
- 【Status】Active
- 【Organization】SAE
- 【Document #】SAE MAP749C
(R) Aircraft Turbine Engine Fuel System Component Endurance Test Procedure (Room Temperature Contaminated Fuel)
- 【Date】2015/8/1
- 【Language】English
- 【Status】Active
- 【Organization】SAE
- 【Document #】SAE AS3114A
(R) BOLT, MACHINE - HEXAGON HEAD, DRILLED 6 HOLES, PD SHANK, CRES AMS5731, .190-32 UNJF-3A
- 【Date】2015/8/1
- 【Language】English
- 【Status】Active
- 【Organization】SAE
- 【Document #】SAE AS3115A
(R) BOLT, MACHINE - HEXAGON HEAD, DRILLED 6 HOLES, PD SHANK, CRES AMS5731, .250-28 UNJF-3A
- 【Date】2015/8/1
- 【Language】English
- 【Status】Active
- 【Organization】SAE
- 【Document #】SAE AS9958A
(R) BOLT, MACHINE, HEXAGON HEAD, DRILLED, 6 HOLE, PD SHANK, STEEL AMS6322, CADMIUM PLATED, .250-28 UNJF-3A
- 【Date】2015/8/1
- 【Language】English
- 【Status】Active
- 【Organization】SAE
- 【Document #】SAE AS9400B
(R) BOLT, TEE HEAD - CADMIUM PLATED, STEEL, UNS G87400, 125 KSI MIN, CHAMFERED, .3750-24 UNJF-3A
- 【Date】2015/8/1
- 【Language】English
- 【Status】Active
- 【Organization】SAE
- 【Document #】SAE AS9401B
(R) BOLT, TEE HEAD - CADMIUM PLATED, STEEL, UNS G87400, 125 KSI MIN, CHAMFERED, .4375-20 UNJF-3A
- 【Date】2015/8/1
- 【Language】English
- 【Status】Active