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BOLT, TEE HEAD - AMS5662, CHAMFERED, .2500-28 UNJF-3A (STRESS RUPTURE RESISTANT)
- Aerospace Standard
- AS3410C
- Revised
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English
Rationale
IN TABLE 1, CORRECT L DIM FOR AS3410-41, IN TABLE 1, CANCEL PART NUMBER AS3410-60 (DUPLICATION OF AS3410-59), FIGURE 1 REDRAWN, Y14.5M FORMATS UPDATED, ADD EDGE DISTANCE EXCEPTION FOR HEAD MARKING, ADD AS3062 FOR THREAD RUNOUT, REVISE LEAD THREAD CHAMFER PER AS1132, UPDATE FPI AND SURFACE TEXTURE REFERENCES, ADD NEW NOTE FOR DISPOSITION OF EXISTING INVENTORY, GENERAL EDITORIAL UPDATES THROUGHOUT.
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Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| TABLE 1 | PART NUMBERS, DIMENSIONS, AND APPROX. MASS |
Issuing Committee
E-25 General Standards for Aerospace and Propulsion Systems
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.
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