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BOLT, MACHINE - HEXAGON HEAD, PD SHANK, AMS 5662, .250-28UNJF-3A (STRESS RUPTURE RESISTANT)
- Aerospace Standard
- AS3414
- Reaffirmed
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Rationale
THIS DOCUMENT HAS BEEN REAFFIRMED TO COMPLY WITH THE SAE 5-YEAR REVIEW POLICY.
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FOR PART NUMBERS AS3414-04 THRU AS3414-18
IN TOL NOTES SHALL BE CHANGED TO
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MATERIAL: CORROSION AND HEAT RESISTANT NICKEL ALLOY AMS 5662.
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MANUFACTURING SPECIFICATION: AMS 7467 EXCEPT ROLL THREAD AND COLD WORK FILLET RADIUS AFTER PRECIPITATION HARDENING.
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FLUORESCENT PENETRANT INSPECTION PER AMS 2645.
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SURFACE TEXTURE: SYMBOLS PER ANSI Y14.36-1978; REQUIREMENTS PER ANSI B46.1-1978. UNLESS OTHERWISE SPECIFIED, SURFACES TO BE 125 MICROINCHES Ra. EXCEPT UPSET HEAD TO BE 250 MICROINCHES Ra.
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BREAK SHARP EDGES .003-.015 UNLESS OTHERWISE SPECIFIED.
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DIMENSIONS IN INCHES.
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DIMENSIONS AND TOLERANCING ANSI Y14.5M-1982.
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DO NOT USE UNASSIGNED PART NUMBERS.
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Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 |
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.
Reference
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