5305-01-586-4895
Find complete technical information, availability, and procurement data for: 5305-01-586-4895
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An item of various configuration that is an integral member of the airframe structure. It is specifically designed for the purpose of maintaining, positioning, joining, and strengthening the aircraft structure. It may include holes for mounting purposes or to form an assembly.
3a thread class, 0.746 inches minimum and 0.776 inches maximum fastener length, pan head style, right-hand thread direction, 0.323 inches nominal thread length
Product Characteristics
Below you’ll find the complete technical specifications and performance data for this part, including material details and compliance information.
- Thread Class
- 3a
- Thread Direction
- right-hand
- Thread Length
- 0.323 inches nominal
- Fastener Length
- 0.746 inches minimum and 0.776 inches maximum
- Head Style
- pan
- Head Diameter
- 0.357 inches minimum and 0.373 inches maximum
- Head Height
- 0.122 inches minimum and 0.133 inches maximum
- Grip Diameter
- 0.188 inches minimum and 0.189 inches maximum
- Internal Drive Style
- offset cruciform (torque set)
- Nominal Thread Diameter
- 0.190 inches
- Grip Length
- 0.428 inches minimum and 0.448 inches maximum
- Thread Quantity Per Inch
- 32
- Part Name Assigned By Controlling Agency
- bolt pan head close tolerance short thread cruciform recess titanium alloy 6al-4v self locking and non locking
- Material
- titanium alloy uns r56400 overall
- Surface Treatment
- aluminum overall
- Thread Series Designator
- unjf
Related Parts
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| Part Number | Name |
|---|---|
| NAS7903A7 | Close Tolerance Screw |
FAQs
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When the NSN 5305-01-586-4895 was assigned to the Federal Catalog?
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