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- 【Organization】SAE
- 【Document #】SAE J1953
Brake-Stroke Indicator Design Guideline for Cam or Disc Air-Brake Actuators
- 【Date】2018/5/1
- 【Language】English
- 【Status】Active
- 【Organization】SAE
- 【Document #】SAE ARP5794A
Centrifugal Aircraft Fuel Pump Requirements, Design and Testing, Aerospace Standard
- 【Date】2018/5/1
- 【Language】English
- 【Status】Active
- 【Organization】SAE
- 【Document #】SAE AS39029/5E
CONTACTS, ELECTRICAL CONNECTOR, SOCKET, CRIMP REMOVABLE (FOR MIL-DTL-26482 SERIES 2, AS81703 SERIES 3, MIL-DTL-83723 SERIES I AND III, MIL-DTL-83733 CONNECTORS, MIL-DTL-12883/40, AND /41 RELAY SOCKETS)
- 【Date】2018/5/1
- 【Language】English
- 【Status】Active
- 【Organization】SAE
- 【Document #】SAE ARP6025
Duty Cycle Considerations for Electrohydrostatic Actuators
- 【Date】2018/5/1
- 【Language】English
- 【Status】Active
- 【Organization】SAE
- 【Document #】SAE ARP6538
Dynamic Modeling of Aerospace Systems (DyMAS)
- 【Date】2018/5/1
- 【Language】English
- 【Status】Active
- 【Organization】SAE
- 【Document #】SAE AS3505C
INSERT - THIN WALL, LONG, SELF-LOCKING, 1025 °F, SILVER PLATED ON INTERNAL SURFACES ONLY, UNS N07718, UNJ THREAD
- 【Date】2018/5/1
- 【Language】English
- 【Status】Active
- 【Organization】SAE
- 【Document #】SAE AMS5402D
Nickel Alloy, Corrosion and Heat-Resistant, Investment Castings 62Ni - 21.5Cr - 9.0Mo - 3.6Cb (Nb) As Cast - UNS N26010
- 【Date】2018/5/1
- 【Language】English
- 【Status】Active
- 【Organization】SAE
- 【Document #】SAE AS9356C
NUT, PLAIN, HEXAGON, UNS S66286
- 【Date】2018/5/1
- 【Language】English
- 【Status】Active
- 【Organization】SAE
- 【Document #】SAE AMS2431D
Peening Media General Requirements
- 【Date】2018/5/1
- 【Language】English
- 【Status】Active
- 【Organization】SAE
- 【Document #】SAE AS6810
Requirements for Accreditation Bodies when Accrediting Test Laboratories Performing Detection of Suspect/Counterfeit in Accordance with AS6171 General Requirements and the Associated Test Method
- 【Date】2018/5/1
- 【Language】English
- 【Status】Active