3120-01-504-2805
Find complete technical information, availability, and procurement data for: 3120-01-504-2805
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A high strength, 160,000 pounds per square inch (1100 megapascals) minimum tensile strength externally threaded fastener designed for use in applications involving great shear stress. The head is designed to accommodate an external wrench or driver. The head is not designed to be held or driven with an inserted driver, nor is it designed for rotation by the thumb and fingers. The unthreaded portion is of specific grip length, plated or unplated, and is machined to a tolerance of one thousandth (0.001) of an inch (0.025 mm) or less of a specific diameter for items one inch (25 mm) or less in diameter. Items over one inch (25 mm) in diameter shall have a tolerance of fifteen ten thousandths (0.0015) of an inch (0.038 mm) or less. The nominal major diameter of the threads shall be at least one thousandth (0.001) of an inch (0.025 mm) below the minimum shank diameter, but not below the minimum major diameter for applicable class of fit, as shown in the screw thread standards, fed std h28 and/or other nationally recognized standards. A locking feature may be incorporated in the design of the head or threads. See bolt, machine and bolt, clevis.
c-17a aircraft end item identification, 1.4270 inches minimum and 1.4570 inches maximum flange outside diameter, 0.2758 inches minimum and 0.2858 inches maximum overall length, 1.0638 inches minimum and 1.0648 inches maximum body outside diameter, 0.8590 inches minimum and 0.8640 inches maximum body inside diameter
Product Characteristics
Below you’ll find the complete technical specifications and performance data for this part, including material details and compliance information.
- Overall Length
- 0.2758 inches minimum and 0.2858 inches maximum
- Body Outside Diameter
- 1.0638 inches minimum and 1.0648 inches maximum
- Body Inside Diameter
- 0.8590 inches minimum and 0.8640 inches maximum
- Flange Outside Diameter
- 1.4270 inches minimum and 1.4570 inches maximum
- End Item Identification
- c-17a aircraft
- Flange Width
- 0.0610 inches minimum and 0.0620 inches maximum
- Part Name Assigned By Controlling Agency
- bushing,sleeve-press fit,flanged
- Material
- copper alloy 630 overall
- Style Designator
- solid, external flange one end
Related Parts
This NSN group includes multiple components designed to meet specific performance and operational standards. Each listing provides detailed specs, functionality data, and replacement compatibility information:
| Part Number | Name |
|---|---|
| 4D0035N14B018 | Sleeve Bushing |
FAQs
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