Thank you for taking an interest in the various military and defense parts, aerospace parts, and other items that we offer. You have reached the RFQ page for part number 4087201, a United Technologies Corporation item with the NSN 2840014487539 that is listed alongside the description “Disk Turbine Aircraft Gas Turbin.” If you are interested in part number 4087201 and wish to learn more about your purchasing options, be sure to submit the form below at your earliest convenience while supplying us with important information concerning your needs and restrictions alike. Once we have a chance to receive and review your completed form, a member of our staff will reach out to you in 15 minutes or less to present a tailored solution for your comparisons.
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To ensure that shopping with us is as simple as possible, we make it easy to identify and procure exact items by listing parts alongside all applicable designations and information. For example, part number 4087201 is specifically listed with the NSN 2840-01-448-7539, and this code can be used to determine that it falls under FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components. Additionally, while tracing back to United Technologies Corporation, this NSN part was specifically produced under CAGE Code 77445. With our services and dedication to simple procurement in mind, get started with us today!
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-448-7539 Item PartTypeName: DISK,TURBINE,AIRCRAFT GAS TURBIN | 2840 | 014487539 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| I | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 4085001 | 1 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABMZ | Diameter | 36.696 INCHES MINIMUM AND 36.736 INCHES MAXIMUM |
| FEAT | Special Features | T.O. 2J-F100-54, FIG 99, IND 42; USE ONLY ON P/NS 4084517-700 AND 4083015-701; LOCATED NEAR THE REAR COMPRESSOR DRIVE TURBINE ROTOR AND STATOR ASSY |
| ABHP | Overall Length | 1.809 INCHES MINIMUM AND 1.811 INCHES MAXIMUM |
| CZBJ | Engine Section Location | TURBINE |
| MRC | Decoded Requirement | Clear Text Reply |
| MDCL | Material Document And Classification | PWA1106 MFR REF SINGLE MATERIAL RESPONSE OVERALL |
| MATT | Material | NICKEL ALLOY OVERALL |
| AGAV | End Item Identification | F100-PW-229 AIRCRAFT GAS TURBINE ENGINE |
| CZCJ | Stage Number | 1 |
| APGF | Design Type | AXIAL COMPRESSOR |
| CRTL | Criticality Code Justification | APGF AND CZBJ AND ABMZ AND ABHP AND FEAT |
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