3120-01-524-5541
Find complete technical information, availability, and procurement data for: 3120-01-524-5541
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A single or multistage item designed to draw air into the front of an engine, gas turbine, aircraft. The air is pushed to the compressor, aircraft gas turbine engine and around the outside of the engine. It consists of a case (3) and vane assembly, fan, aircraft gas turbine engine and a rotor, fan, aircraft gas turbine engine.
0.9950 inches minimum and 1.0000 inches maximum overall length, 0.8600 inches minimum and 0.8700 inches maximum flange outside diameter, 0.6261 inches minimum and 0.6266 inches maximum body outside diameter, 0.4840 inches minimum and 0.4910 inches maximum body inside diameter, f-22 aircraft end item identification
Product Characteristics
Below you’ll find the complete technical specifications and performance data for this part, including material details and compliance information.
- Overall Length
- 0.9950 inches minimum and 1.0000 inches maximum
- Body Outside Diameter
- 0.6261 inches minimum and 0.6266 inches maximum
- Body Inside Diameter
- 0.4840 inches minimum and 0.4910 inches maximum
- Flange Outside Diameter
- 0.8600 inches minimum and 0.8700 inches maximum
- End Item Identification
- f-22 aircraft
- Flange Width
- 0.0600 inches minimum and 0.0650 inches maximum
- Corner Shape
- square all corners
- Part Name Assigned By Controlling Agency
- bushing,flanged,undersize bore (for clamped installation)
- Material
- steel comp xm-12 overall
- Surface Treatment
- passivate overall
- Style Designator
- solid, external flange one end
Related Parts
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| Part Number | Name |
|---|---|
| BACB28AP08-016 | Sleeve Bushing |
FAQs
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Does the NSN 3120-01-524-5541 have a Schedule B code assigned?
Does NSN 3120-01-524-5541 require demilitarization?
Does NSN 3120-01-524-5541 contain precious materials?
Does NSN 3120-01-524-5541 contain hazardous materials?
When the NSN 3120-01-524-5541 was assigned to the Federal Catalog?
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Pricing
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