5306-01-654-2575
Find complete technical information, availability, and procurement data for: 5306-01-654-2575
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An item of various cross-sectional shapes which may be of solid or hollow construction. It is specifically designed for attachment to a lever(s) and/or control(s) to actuate various remote mechanisms. It is one of the following: (1) a one-piece item with or without eyes and/or holes in each end which may have bushings or bearings pressed in the eyes; (2) a one-piece item with both ends processed for terminations, excluding threaded end(s); (3) a two-piece construction type item consisting of a body with both ends processed for terminations and a single end attachment; or (4) a three-piece construction type item consisting of a body and two end attachments. Excludes:internal combustion engine type piston connecting rods; drag link, steering; link, anchor, brake shoe; tie rod, steering; and turnbuckle. For cylindrical shaped externally threaded items without end attachments, see rod, threaded end and stud (as modified).
hexagon head style, right-hand thread direction, 3a thread class, 6.1200 inches nominal fastener length, 0.3700 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
- 0.3700 inches nominal
- Fastener Length
- 6.1200 inches nominal
- Head Style
- hexagon
- Head Height
- 0.1250 inches minimum and 0.1400 inches maximum
- Width Between Flats
- 0.4290 inches minimum and 0.4390 inches maximum
- End Item Identification
- f-35 aircraft
- Nominal Thread Diameter
- 0.2500 inches
- Thread Quantity Per Inch
- 28
- Minimum Tensile Strength
- 160000 pounds per square inch
- Part Name Assigned By Controlling Agency
- bolt, tension, hex head, close tolerance, a286 cres, short thread, reduced major thread diameter, self locking and non-locking, 160 ksi ftu
- Material
- titanium alloy uns r56400 overall
- Material Document And Classification
- ams 5662 assn std single material response or ams 5962 assn std single material response overall
- Thread Series Designator
- unjf
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|---|---|
| NAS6304U92D | Shear Bolt |
FAQs
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