3040-01-095-2312
Find complete technical information, availability, and procurement data for: 3040-01-095-2312
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An item specifically designed to position and/or restrain the movement of one or more blade, or blade set, turbine, aircraft gas turbine engine. It may be the full 360 degrees required for one turbine stage or a segment thereof.
circular grooved and externally threaded second end style, 0.1980 inches minimum and 0.2060 inches maximum second end groove diameter, plain first end style, 0.0700 inches minimum and 0.1100 inches maximum second end groove width, not identical end similarity
Product Characteristics
Below you’ll find the complete technical specifications and performance data for this part, including material details and compliance information.
- First End Style
- plain
- End Similarity
- not identical
- Second End Style
- circular grooved and externally threaded
- Second End Groove Width
- 0.0700 inches minimum and 0.1100 inches maximum
- Second End Groove Diameter
- 0.1980 inches minimum and 0.2060 inches maximum
- Overall Length
- 5.590 inches minimum and 5.610 inches maximum
- First End Diameter
- 0.3110 inches minimum and 0.3120 inches maximum
- Second End Distance From End To Groove
- 0.370 inches nominal
- Second End Diameter
- 0.3720 inches minimum and 0.3730 inches maximum
- Second End External Thread Length
- 0.370 inches nominal
- Step Quantity
- 4
- Largest Step Diameter
- 0.372 inches minimum and 0.373 inches maximum
- Material
- steel comp 416
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 |
|---|---|
| 12292463 | Shouldered Shaft |
FAQs
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When the NSN 3040-01-095-2312 was assigned to the Federal Catalog?
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