Thank you for taking interest in United Technologies Corporation part number 4082748, which is listed with the NSN 2840-01-448-7033 and a product description of “Seal Air Aircraft Gas Turbine En.” In order to receive procurement options on this particular listing, we ask that you fill out and submit the form provided below with as much information as you can concerning your needs. By supplying our staff with key details on your desired quantity, pricing target, and expedited fulfillment timeframe, we can respond with a quote that has been specifically tailored to your unique specifications. We also ask that you make us aware of any restrictions that you may have as soon as possible, such as if you have a time constraint or are seeking unlisted items.
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Alongside part number 4082748, you are encouraged to continue exploring our collection curated catalogs to find additional items that can accompany this Seal Air Aircraft Gas Turbine En part with the NSN 2840-01-448-7033. For example, you can browse other United Technologies Corporation components that were produced under CAGE Code 77445 or listings that belong to FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components with ease on our website, with search tools provided for quick location. Furthermore, our staff is just a call or email away from assisting you with any inquiries or requests, so be sure to get started on the quotation process for part number 4082748 and other desired offerings on Aerospace Spare.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-448-7033 Item PartTypeName: SEAL,AIR,AIRCRAFT GAS TURBINE EN | 2840 | 014487033 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| 7 | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 4082748-01 | 5 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| MRC | Decoded Requirement | Clear Text Reply |
| ABHP | Overall Length | 0.154 INCHES MINIMUM AND 0.166 INCHES MAXIMUM |
| CZBJ | Engine Section Location | COMBUSTION CHAMBER |
| ABMZ | Diameter | 19.626 INCHES MINIMUM AND 19.630 INCHES MAXIMUM |
| APGF | Design Type | AXIAL COMPRESSOR |
| CXCY | Part Name Assigned By Controlling Agency | ORIGINAL NAME BRUSHSEAL,INNER |
| CRTL | Criticality Code Justification | ABHP AND ABMZ AND ABMK AND CZBJ AND FEAT |
| AGAV | End Item Identification | F100-PW-229 AIRCRAFT GAS TURBINE ENGINE |
| FEAT | Special Features | T.O. 2J-F100-54, FIG 86, IND 19G; SEAL CONTAINS BRUSH WIRE PACK THAT HAS 2250-2650 WIRES PER CIRCUMFERENTIAL INCH; USE ONLY ON P/NS 4083194, 4083560 AND 4083565; LOCATED NEAR THE REAR COMPRESSOR DRIVE TURBINE ROTOR AND STATOR ASSY, TURBINE STATOR SUPPORT |
| CZCJ | Stage Number | 1 |
| MDCL | Material Document And Classification | AMS5599 ASSN STD 1ST MATERIAL RESPONSE OVERALL OR AMS5666 ASSN STD 2ND MATERIAL RESPONSE OVERALL |
| MATT | Material | NICKEL ALLOY OVERALL |
| ABMK | Overall Width | 0.258 INCHES MINIMUM AND 0.268 INCHES MAXIMUM |
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