BOLT, TEE HEAD - AMS 5662, CHAMFERED, .250-28UNJF-3A (STRESS RUPTURE RESISTANT)
- Aerospace Standard
|Aerospace Standard||Stud, Locked In - Ring, Straight, Installation and Removal Of|
|Aerospace Standard||RIVET - TUBULAR, COUNTERSUNK, CORROSION AND HEAT RESISTANT NICKEL ALLOY (UNS N06600)|
|Aerospace Standard||BOLT, TEE HEAD – CHAMFERED, AMS5708 (UNS N07001), 165 KSI MIN UTS, .1900-32UNJF-3A|
Data Sets - Support Documents
The SAE E-25 General Standards for Aerospace & Propulsion Systems committee addresses aerospace propulsion systems and components. These systems and components include bolts, screws, nuts, washers, studs, rivets, pins, covers, O-rings, brackets, plugs and associated procurement requirements, as well as solid film lubricants and design specifications for screw threads and fastener assembly requirements.